WO2016075272A1 - Micro-scale energy directors for ultrasonic welding - Google Patents

Micro-scale energy directors for ultrasonic welding Download PDF

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Publication number
WO2016075272A1
WO2016075272A1 PCT/EP2015/076518 EP2015076518W WO2016075272A1 WO 2016075272 A1 WO2016075272 A1 WO 2016075272A1 EP 2015076518 W EP2015076518 W EP 2015076518W WO 2016075272 A1 WO2016075272 A1 WO 2016075272A1
Authority
WO
WIPO (PCT)
Prior art keywords
microscale
tool
master
replication
lateral
Prior art date
Application number
PCT/EP2015/076518
Other languages
French (fr)
Inventor
Carl Esben POULSEN
Anders Wolff
Nis Korsgaard ANDERSEN
Kasper KISTRUP
Rafael Taboryski
Original Assignee
Danmarks Tekniske Universitet
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Danmarks Tekniske Universitet filed Critical Danmarks Tekniske Universitet
Publication of WO2016075272A1 publication Critical patent/WO2016075272A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0053Moulding articles characterised by the shape of the surface, e.g. ribs, high polish
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/10Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating making use of vibrations, e.g. ultrasonic welding
    • B23K20/103Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating making use of vibrations, e.g. ultrasonic welding using a roller
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/10Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating making use of vibrations, e.g. ultrasonic welding
    • B23K20/106Features related to sonotrodes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/0006Working by laser beam, e.g. welding, cutting or boring taking account of the properties of the material involved
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/062Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam
    • B23K26/0622Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam by shaping pulses
    • B23K26/0624Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam by shaping pulses using ultrashort pulses, i.e. pulses of 1ns or less
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/352Working by laser beam, e.g. welding, cutting or boring for surface treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/352Working by laser beam, e.g. welding, cutting or boring for surface treatment
    • B23K26/3568Modifying rugosity
    • B23K26/3584Increasing rugosity, e.g. roughening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/26Moulds
    • B29C45/37Mould cavity walls, i.e. the inner surface forming the mould cavity, e.g. linings
    • B29C45/372Mould cavity walls, i.e. the inner surface forming the mould cavity, e.g. linings provided with means for marking or patterning, e.g. numbering articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/022Mechanical pre-treatments, e.g. reshaping
    • B29C66/0222Mechanical pre-treatments, e.g. reshaping without removal of material, e.g. cleaning by air blowing or using brushes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/302Particular design of joint configurations the area to be joined comprising melt initiators
    • B29C66/3022Particular design of joint configurations the area to be joined comprising melt initiators said melt initiators being integral with at least one of the parts to be joined
    • B29C66/30221Particular design of joint configurations the area to be joined comprising melt initiators said melt initiators being integral with at least one of the parts to be joined said melt initiators being point-like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/534Joining single elements to open ends of tubular or hollow articles or to the ends of bars
    • B29C66/5346Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
    • B29C66/53461Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/20Tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/08Non-ferrous metals or alloys
    • B23K2103/10Aluminium or alloys thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/72Heating or cooling
    • B29C45/73Heating or cooling of the mould
    • B29C2045/7356Heating or cooling of the mould the temperature of the mould being near or higher than the melting temperature or glass transition temperature of the moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/72Heating or cooling
    • B29C45/73Heating or cooling of the mould
    • B29C2045/7393Heating or cooling of the mould alternately heating and cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C59/00Surface shaping of articles, e.g. embossing; Apparatus therefor
    • B29C59/02Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing
    • B29C59/022Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing characterised by the disposition or the configuration, e.g. dimensions, of the embossments or the shaping tools therefor
    • B29C2059/023Microembossing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C59/00Surface shaping of articles, e.g. embossing; Apparatus therefor
    • B29C59/02Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing
    • B29C59/026Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing of layered or coated substantially flat surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7316Surface properties
    • B29C66/73161Roughness or rugosity
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/92Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools
    • B29C66/929Measuring or controlling the joining process by measuring or controlling the pressure, the force, the mechanical power or the displacement of the joining tools characterized by specific pressure, force, mechanical power or displacement values or ranges
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0093Other properties hydrophobic

Definitions

  • the present invention relates in one aspect to a replication tool and a method of providing the replication tool.
  • the present invention relates to a method of producing a part by replication, the part having a flange portion for use in the formation of an ultrasonic welding joint.
  • the invention relates to a method of joining two parts by ultrasonic welding.
  • Ultrasonic welding is a technique for joining thermoplastics parts by applying high- frequency ultrasonic acoustic vibrations across the joint surfaces while pressing the parts together.
  • the acoustic vibrations are absorbed by the thermoplastic material, which melts locally, thereby forming a welded seam.
  • at least one of the flanges of the joint comprises pointed or knife edge type protrusions, so-called energy directors that concentrate the ultrasonic energy to the location where the weld is to be formed.
  • Energy directors commonly known from industrial processes have several disadvantages, in particular when high precision welds with high weld strength are to be formed.
  • microfluidic chips such as used for medical diagnosis or environmental testing.
  • a base chip with a system of microfluidic channels and components is formed e.g. as a replicated part in an injection moulding, compression moulding or hot embossing process.
  • the base chip is then covered by a counter-part, which may equally comprise microfluidic channels and components, but may as well be a simple lid.
  • the two parts are joined to form a fluid tight seal.
  • Such joints may be formed e.g. by gluing, thermal bonding, or vapour bonding, but attempts have also been made to use ultrasonic bonding for joining such parts.
  • ultrasonic bonding may overcome some of the challenges encountered with other bonding techniques, e.g. when packaging hazardous materials or sensitive reagents, where the other bonding techniques, due to the process parameters involved, are outright in- compatible with the product.
  • the uncontrolled deformation of the energy directors during the ultrasonic welding process typically results in the occurrence of so-called flashes that may penetrate into the microfluidic channels, or may lead to uncontrolled cross-sectional dimensions of the microfluidic channels and components. Therefore, there is a need for a reliable and cost-effective process for forming an ultrasonic joint overcoming at least some of the above-mentioned disadvantages, or at least to provide an alternative to known methods. Furthermore, there is a need for suitable tooling for use in the above method of forming an ultrasonic joint. Furthermore, there is a need for a process for providing such suitable tooling.
  • a first aspect of the invention relates to a method of providing a replication tool, the method comprising providing a forming tool having a tool surface adapted to define a general shape of a part to be formed; modifying at least portions of the tool surface by a pulsed laser treatment to obtain a microscale structured master surface with a lateral master pattern and a vertical master profile; wherein the pulsed laser treatment is adapted to generate microscale phase explosions on the tool surface, thereby forming the microscale structured master surface as a lateral arrangement of microscale crater-shaped depressions.
  • the crater-shaped depressions obtained by the microscale phase explosions are irregular in shape and polydisperse, i.e. varying in size with a spread about a most prominent size.
  • the size may e.g. be characterized by the area covered by the depression as seen in a vertical projection on a lateral plane.
  • the microscale structuring of the tool surface is provided by the localized application of laser pulses directly to selected portions of the tool surface.
  • This post-treatment of the tool surface by means of localized laser treatment has the advantage that the replication tool with the shape defining tool surface may be designed and produced using existing techniques and equipment for tool making, thereby contributing to a relatively simple and cost effective implementation of the surface modification in an existing fabrication process.
  • the localized pulsed laser treatment is adapted to melt and evaporate material at the tool surface to generate microscale phase explosions, thereby producing a randomised surface structure of polydisperse microscale features.
  • the microscale surface features are depressions, which are typically crater shaped with steeply sloped side walls.
  • the process of provoking mi- croscale phase explosions by locally applying laser energy to the tool surface so as to form the crater-shaped depressions is stochastic in nature, wherein upon appropriate exposure the microscale surface features are densely packed and may even partially overlap, thereby forming a microscale lateral pattern with a microscale po- rous appearance.
  • the localized application of laser power may be scanning a laser spot along a predetermined scanning path at a pre-determined scan speed over the tool surface.
  • the path may follow a single scan along the path over the tool surface, a repetitive scanning along the same linear path, or a combination of both.
  • the path is adapted to cover the selected portions of the tool surface.
  • the path may e.g. be straight, curved, meandering, segmented or a combination thereof and some sections of the path may overlap other sections of the path in order to achieve an even exposure of the selected portions of the tool surface with laser energy.
  • the pulsed laser radiation has to be of a wave length and pulse characteristics that is absorbed by the tool surface in order to be able to locally melt and evaporate material from the tool surface so as to produce microscale phase explosions creating the crater-shaped depressions.
  • the laser radiation may be from a picosecond-laser source with a wavelength in the near infrared, such as 1064 nm, but other wavelength ranges, e.g. in the visible part of the electromagnetic spectrum, and pulse characteristics that are suitable for locally heating the tool surface to generate microscale phase-explosions may be conceived, too.
  • the finish of the targeted portions of the tool surface is controlled by adapting the exposure of these tool surface portions with the pulsed laser radiation.
  • the exposure of the tool surface is controllable e.g.
  • the laser power/spot intensity by adjusting the laser power/spot intensity and/or by varying the scan speed, wherein exposure of a given surface portion increases with increasing laser power, but decreases with increasing scan speed.
  • the finish of the targeted portions of the tool in turn determines the finish of the replicated part in the corresponding regions on the surface of the part via the replication process. Furthermore, multiple exposures of the same surface portions, e.g. by repetitive and/or overlapping scan- ning of the laser spot over these surface portions, results in an exposure that is increased correspondingly.
  • the lateral pattern of the microscale structured master surface has an area density of microscale master features of at least 5000/mm 2 .
  • a rea- sonably densely packed lateral distribution of microscale features on the master surface is achieved, thereby allowing for producing parts with a replicated microscale surface texture that is useful for forming high precision, fluid tight ultrasonic joints with improved bond strength.
  • the lateral pattern of the microscale structured master surface has an area density of microscale master features of at least 8000/mm 2 , or even of at least 10000/mm 2 .
  • an upper limit for the area density resulting from the microscale of the surface structuring exists, which is discussed in detail further below.
  • a further aspect of the invention relates to a method of producing a first part having a flange portion for use in the formation of an ultrasonic welding joint with a cooperating second part, the method comprising the steps of providing a replication tool with a microscale structured master surface by a method according to the above-mentioned embodiment; and using the replication tool to form the first part by the replication process, wherein the formed first part has the general shape as defined by the tool surface, and wherein the formed first part comprises a microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions on at least the flange portion of the first part.
  • the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 5000/mm 2 . As mentioned above, this allows for forming high precision, fluid tight ultrasonic joints with im- proved bond strength.
  • the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 8000/mm 2 , or even of at least 10000/mm 2 .
  • this allows for forming high precision, fluid tight ultrasonic joints with particularly improved bond strength.
  • An upper limit for the area density resulting from the microscale of the cone-like protrusions forming the surface texture exists, which is discussed in detail further below.
  • the method is useful for forming the first part from a replication material replicating the microscale structured master surface onto the first part to form a surface region with a lateral arrangement of polydisperse microscale energy directors shaped as polydisperse microscale protrusions on the first part.
  • a lateral replica pattern is defined by the lateral master pattern, and a vertical replica profile has finite peak-to- peak amplitude to form a three-dimensional texture. Since the lateral replica pattern is defined by the lateral master pattern, it is equally irregular as seen in a projection onto a lateral plane, and the microscale protrusions are polydisperse.
  • the method is for producing the first part by a fast replication process using the replication tool, such as required by a commercially viable production of the item in large numbers.
  • the laser treatment of the tool surface results in a porous surface appearance produced by a randomised lateral arrangement of, preferably densely packed, microscale depressions, which are typically shaped as relatively deep, steep-walled craters with a more or less pointed bottom.
  • the sloped sidewalls facilitate an easy de-moulding of the replicated item in the step of releasing the item from the tool surface.
  • a replication process may be considered fast, for example, if the replication period from contacting the tool surface with the molten replication material to releasing the formed part is short, such as well below ten minutes, such as less than five minutes, such as less than 3 minutes, such as less than one minute, such as less than 30 seconds, or even less than 10 seconds.
  • the suggested thermally controlled replication process using a thermoplastic replication material can be performed fast as compared to for example replication processes using thermosetting replication materials, or chemically setting replication materials.
  • the method is also useful for the production of first parts having a flange portion with microscale energy directors thereon by other replication techniques, such as the mentioned slower methods using thermosetting or chemically setting replication materials, or for replication techniques like compression moulding and hot em- bossing.
  • microscale refers to dimensions of about 1 ⁇ to 1000 ⁇ that are generally measured in microns (micrometres), typically in the range of about 1 ⁇ to 100 ⁇ .
  • nanoscale refers to dimensions of about 1 nm to 1000 nm that are generally measured in nanometres, typically in the range of about 1 nm to 100 nm.
  • the microscale structure of the master surface and, accordingly, the microscale texture of the replica surface have a three-dimensional topography of microscale elements arranged next to each other and may be decomposed in a lateral pattern and a vertical profile.
  • the term "lateral pattern” refers to the arrangement in lateral directions of the (3D) microscale elements making up the microscale structure/texture, as seen in vertical projection on to a lateral plane.
  • the term “vertical profile” refers to the variation of the location of the surface in a direction perpendicu- lar to the lateral directions.
  • a surface structuring/texturing When a surface structuring/texturing is applied to an object having a general shape, such as a tool surface or an item, the surface structuring/texturing can be seen as a vertical variation of the surface, which is added to the general shape of the tool sur- face/item. Accordingly, on an object with a microscale structured/textured surface, an average surface that flattens out any vertical variations of the surface by averaging on a lateral scale larger than that of the microscale structuring/texturing essentially follows the general shape of the object.
  • the general shape of the object is thus defined independent of any nano- or microscale surface roughness / finish / structur- ing.
  • lateral directions are parallel / tangential to a surface defining the general shape of the object on a scale larger than the scale of the lateral pattern. Accordingly, the vertical direction at a given point on the surface of the object is the surface normal to the general shape in that point. In each given point, the vertical direction is perpendicular to the corresponding lateral directions.
  • the general shape of the replicated part is defined by the general shape of the tool surface.
  • the replication process is for accurately replicating the general shape of the part as defined by the tool surface.
  • the surface of the replicated part is functional- ised by applying a surface finish with a microscale texture at least on selected regions of the surface of the part.
  • the particular functionalization is to make a flange portion of the replicated part susceptible to concentrate ultrasonic energy so as to act as a distributed energy director when forming an ultrasonic joint with a cooperating flange portion of a counterpart.
  • the area of contact is reduced to point contacts where the tops of the protrusions meet the surface of the counterpart when the first flange portion is brought in contact with the cooper- ating second flange portion.
  • the protrusions are sacrificial; Upon formation of the joint, the protrusions are flattened out by the ultrasonic energy dissipated and the pressure applied.
  • the material of the energy directors spreads in lateral directions, but is easily absorbed on the spot also on a microscale, due to the lateral interspaces between the protrusions. Thereby, the quality and precision of the ultrasonic joint is improved, and the formation of undesirable "flashes", i.e. the spreading of material into regions adjacent to the ultrasonic joint, is avoided.
  • An important advantage of the present method is that the laser treatment of the tool surface is only limited by the requirement of an optical access to the surface to be modified.
  • a microscale structured master surface may be applied to virtually any surface topology, including very narrow and deep trenches or holes, as long as a laser beam can be guided to the tool surface to be modified.
  • This allows for an improved freedom for designing the ultrasonic joint and accordingly for designing the replicated parts to be assembled.
  • the microscale protrusions may be distributed over the entire flange portion of the replicated parts or only to selected regions thereof.
  • the flange portion may be arbitrarily shaped as seen in the lateral direction, e.g. the flange portion may easily be adapted to cover larger surfaces.
  • the microscale energy directors may even be arranged on curved and/or oblique surfaces following a more complex general shape of the replicated part, thereby adding to the above-mentioned improved freedom of design.
  • the method comprises the steps of (a) providing a replication tool having a tool surface adapted to define a general shape of the first part, wherein the tool surface comprises a microscale structured master surface obtained by localized pulsed laser treatment of the tool surface to generate mi- croscale phase explosions, said microscale structured master surface having a lateral master pattern and a vertical master profile; (b) contacting the tool surface with a replication material in the melt phase, wherein the tool surface is maintained at a process temperature below a melt temperature of the replication material, thereby (c) cooling the replication material to a stabilized shape with a microscale textured replica surface, wherein the lateral master pattern defines a corresponding lateral replica pattern of the microscale textured replica surface and wherein the amplitude of a vertical profile of the microscale textured replica surface is in the microscale, and (d) releasing the shaped item from the tool surface.
  • a replication process where the tool surface is maintained at a more or less constant temperature below the melt temperature throughout the production process is sometimes referred to as an "isothermal" type process. Isothermal processes may be performed at high throughput.
  • the truthfulness of the replication of the vertical profile of the microscale master structure is uncritical as long as the peak-to-peak amplitude of the vertical profile of the micro-texture on the replica surface is sufficient, and further preferably the lateral pattern is faithfully transferred.
  • the mi- croscale structured master surface is prior to contact with the replication material heated to an injection temperature above the melting temperature of the replication material, but immediately upon injection of the replication material rapidly cooled to a temperature below the melting temperature of the replication material, at which the first part is finally released from the mould.
  • the replication process is one of injection moulding, hot embossing, compression moulding, and extrusion coating.
  • the microscale textured replica surface has a peak-to-peak amplitude of at least 0.5 ⁇ , or at least 1 ⁇ and up to 5 ⁇ , or up to ⁇ ⁇ , or even up to 30 ⁇ .
  • the exact 3D-shape of each of the microscale features on the tool surface and their exact arrangement with respect to each other is not critical. Also, the exact details of the individual microscale elements and of their arrangement making up the micro-texture on the surface of the replicated item are uncritical for achieving a concentration effect by the microscale energy directors.
  • the fast replica- tion process thus yields proper items as long as the general shape is faithfully obtained reliably, the microscale lateral pattern is reliably reproduced in each reproduction process, and the peak-to-peak amplitude of the vertical profile of the replica surface is adapted to provide point contacts between the tops of the protrusions on the first part and the cooperating flange portion of the second part.
  • Reduced ampli- tude gives less "flashes", but requires corresponding precision in the flatness/fit of the cooperating first and second flange portions.
  • Relatively small amplitudes of the vertical profile of the texture of the replica surface may already achieve a sufficient concentration of ultrasonic energy into point contacts, such as amplitudes of at least 100nm, alternatively at least 200nm, alternatively at least 500nm, and preferably in the microscale, such as ⁇ ⁇ - ⁇ ⁇ , such as 1 ⁇ -30 ⁇ , preferably in the range ⁇ ⁇ - ⁇ ⁇ .
  • the fidelity of replication of the vertical pro- file tends to be affected by standard parameters of processes for fast replication in thermoplastic materials, such as tool temperature, replication period, and temperature and/or pressure of the thermoplastic replication material in the melt phase. This is owing to the ability of the thermoplastic replication material to fill the depressions of the relatively deep steep-walled master structure before solidifying, which may be controlled by these parameters. Thereby, the fidelity of replication may be controlled. For example, fidelity of microstructure replication may be reduced by reducing the temperature at which the tool surface is maintained.
  • the melt When the replication material contacts the tool surface at the lower the melt is cooled more rapidly, thereby increasing the viscosity of the melt and impeding the filling of the microscale depressions/crevices/craters/pores of the master structure on the tool surface by the melt before it solidifies.
  • a reduced fidelity is reflected by a reduced amplitude of the replicated profile as compared to the master profile: the replication is more shallow than the master.
  • the fidelity of replication of the vertical profile may thus be characterised e.g.
  • the method by comparing the peak-to-peak amplitudes of the vertical profiles of the replicated microscale texture and the microscale master structure to each other, wherein for a low fidelity replication the amplitude of the replicated profile as compared to the master profile is lower than for a higher fidelity replication.
  • the low-fidelity replicated microscale textures exhibit a rounded top. Since the energy concentration is uncritical as to the exact shape and arrangement of the individual microscale features, another advantage of the method is that it facilitates a relatively simple and cost effective implementation of the surface functionalization in an existing fabrication process by merely modifying the tool surface of a replication tool in a post-treatment step.
  • the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 5000/mm 2 , at least 8000/mm 2 , or at least 10000/mm 2 .
  • the protrusions are densely packed to provide a good mechanical strength of the joint.
  • a densely packed lateral arrangement of the protrusions also ensures good fluid sealing properties of the ultrasonic joint, e.g. when forming hermetically sealed chambers or channels.
  • the part may be made entirely from replication material with a shape defined by the tool surface, or the replication material may be applied to/carried by a substrate material, e.g. in an additive moulding step or a coating step.
  • the replication process used for producing the part is injection moulding.
  • Injection moulding is a cyclic replication process with a fast cycle time, i.e. using this embodiment a large number of separate items with a microscale textured replica surface may be produced at high throughput.
  • the inner surface of the injection mould is the tool surface defining the general shape of the part. At least portions of the tool surface have a finish with a microscale structuring generated by localised treatment with a pulsed laser source.
  • the thermoplastic replication material is heated to above the melt transition temperature and in the melt phase injected into the closed mould, which is kept at a temperature between the glass transition temperature and the melt transition tempera- ture of the replication material. When the molten replication material contacts the cooled tool surface it solidifies, whereby it is shaped and textured, before the item is released from the mould.
  • a surprising insight is that the replica surface produced in a fast injection moulding process using the replication tool presented herein exhibits a microscale textured replica surface which is well suited for forming a reliable ultrasonic welding joint also if the vertical profile of the microscale texture on the replica surface is a low fidelity replication of the corresponding profile of the microscale structure on the master surface.
  • Precise and strong ultrasonic welding joints may be reliably obtained as long as the lateral pattern is faithfully transferred and the peak-to-peak amplitude of the vertical profile of the micro-texture on the replica surface is in the microscale, or at least has an amplitude that is sufficient for forming point contacts that are distributed over the respective flange portions.
  • the replication process is extrusion coating.
  • Extrusion coating is a process for roll-to-roll processing, i.e. using this embodiment the part may be produced in a continuous process as a layered web with a microscale textured replica surface.
  • a substrate web may be passed between a nib roll and a cooling roll, in a conventional manner, wherein the rotary surface of the cooling roll is the tool surface defining the general shape of the item.
  • the tool surface has a finish with a microscale structuring gener- ated by treatment with a pulsed laser source.
  • a thermoplastic replication material is heated to above the melting temperature and in the melt phase supplied between the substrate web and the cooling roll, which is kept at a temperature below the melting temperature of the replication material. When the molten replication material contacts the cooled tool surface it solidifies, whereby it is shaped and textured, be- fore the item is released from the replication tool.
  • a replication period from contacting the tool surface with the molten replication material to releasing the shaped item is less than 3 minutes, such as less than one minute, such as less than 30 seconds, or even less than 10 seconds.
  • the replication time may be less than one minute, i.e. a few tens of seconds, such as about 30 seconds.
  • an extrusion coating process is even faster with replication times of less than 10 seconds.
  • the vertical replica profile predominantly has rounded tops with a radius of curvature in the microscale.
  • the replication process may be controlled to influence the fidelity of replication to provide a vertical replica profile that predominantly has rounded tops with a radius of curvature in the microscale.
  • a low fidelity replication may be achieved in a fast replication process with short replication periods.
  • a process goal/constraint of a faithful replication of the vertical profile of the master structure may entail long settling or curing times incompatible with a fast replication process.
  • the radius of curvature of the rounded tops is of the same order as the lateral distance between adjacent structures/features of the lateral pattern, such as predominantly above 1 ⁇ , above 5 ⁇ , or even above 10 ⁇ , and predominantly less than 300 ⁇ , less than ⁇ ⁇ or even less than 50 ⁇ .
  • the vertical amplitude of the replica profile is about equal or less than the lateral distance between adjacent microscale features.
  • a method for producing a part with microscale energy directors on flange portions thereof comprises preparing a replication tool using the above- mentioned method, and repeatedly performing the method of producing an item with a microscale textured replica surface by a replication process according to any one of the above-mentioned embodiments. Large numbers of items exhibiting enhanced hydrophobicity or super-hydrophobicity may thus be produced cheaply.
  • the invention relates to a part with a microscale textured replica surface produced by replication according to any of the above- mentioned methods.
  • a method of joining a first part and a second part by ultrasonic welding comprises the steps of producing the first part with microscale energy directors in the form of microscale cone-like protrusions on a flange portion thereof by the method according to any one of the above-mentioned embodiments; producing a second part having a cooperating flange portion; - bringing the microscale cone-like protrusions on the flange portion of the first part in contact with the cooperating flange portion of the second part; and applying ultrasonic energy and pressure, thereby flattening out the cone-like protrusions, to form an ultrasonic welding joint between the first and second parts.
  • the ultrasonic energy is applied across the flange portions while applying a compression force pressing the two cooperating flanges together.
  • the invention provides areas of microscale energy directors distributed over flange portions where the work pieces are to be welded together.
  • a master of the micro-scale energy directors is produced by at least partially covering corresponding flange portions of the work piece negative in a forming tool with a micro-scale roughening, and subsequently replicating the microscale roughening into the flange portions of the work pieces in a forming step. It has turned out that the above described pulsed laser treatment of the tool surface gives an adequate microscale roughening that may be replicated onto the part to form micro-scale energy directors.
  • a proper scale of the depressions is obtained.
  • a welding joint portion may even be defined on the forming tool in a post processing process, e.g. on an existing forming tool, independent of the process of preparing the forming tool / tool surface.
  • the welding joint portion may be produced in the same replicating step as the part itself.
  • the master surface has a microscale structuring with a lateral master patterning and a vertical master profile. Accordingly, the replicated part has a microscale texture with lateral replica patterning and a vertical replica profile.
  • the first part comprises a flexible web carrying the microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions on at least a flange portion thereof.
  • the first part may be useful for assemblies comprising a functional- ized flexible web integrated therein, or for packaging purposes, or when using the flexible web as a cover for a closed container in food packaging, in medical packaging, in analytic devices, or similar applications.
  • a further aspect of the invention relates to a replication tool for producing a part with a microscale textured replica surface by replication, the replication tool comprising a tool surface defining a general shape of the part, the tool surface comprising at least on portions thereof a microscale structured master surface having a lateral master pattern and a vertical master profile, wherein said microscale structured master surface has been provided by localized pulsed laser treatment adapted to generate microscale phase explosions.
  • the vertical master profile has a peak-to- peak amplitude of at least 0.5 ⁇
  • the lateral master pattern has an area density of microscale master features of at least 5000/mm 2 .
  • the replication tool for the replication process in question e.g. a mould for injection moulding or a roller for extrusion coating
  • the microscale surface structuring is applied as a post treatment of the tool surface by means of a pulsed laser directly scanned over the tool surface.
  • a suitable pulsed laser may be, but is not limited to, an industrial picosecond-laser operating in the near infrared, such as at 1064nm.
  • the exposure of the surface to the pulsed laser radiation is adapted to generate microscale phase explosions.
  • microscale structured master surface has a lateral master pattern and a vertical master profile as described above.
  • the post-treatment applied here does not require the precise micro-milling of a specific pre-determined shape of the master structure, such as a regular array of micro- cones, the post-treatment may be applied using cheaper equipment. Furthermore, this post-treatment adapted to generate a microscale porous surface from mi- croscale phase explosions is faster to apply than e.g. micro-milling of microscale features. Furthermore, as also mentioned above, the microscale phase explosions generate microscale crater-shaped depressions with sloped sidewalls that are well suited for fast replication processes, such as injection moulding and extrusion coating. Amongst others, the crater shape with sloped sidewalls facilitates easy releas- ing of the shaped items from the tool surface at the end of the moulding process (de-moulding).
  • the tool surface is made of a metal, such as aluminium or steel.
  • the tool surface has to be suited for the fast replication processes for which the method is intended.
  • the tool surface comprising the microscale master structure can be directly produced on a mould surface for contacting the replication material and/or on an inlay attached to the inside of a mould. It is understood that the tool surface may be broken up in sub-surfaces that form part of the mould as is customary in tool design for fast replication processes, such as injection moulding or extrusion coating.
  • commonly used metals that are also suitable for the present invention include, but are not limited to, aluminium alloys of the types 2017, 1050 or 5754, or tool steel, such as "Sandvik Corona C60", orvar 2343 or similar.
  • the microscale structured master surface is a lateral arrangement of polydisperse microscale master features.
  • polydisperse refers to microscale features having varying transverse dimensions as seen in a vertical projection.
  • the polydisperse dimen- sions are characterized by a statistical distribution having a centre value and a spread.
  • the transverse dimensions may be specified as transverse linear dimensions characteristic of the lumen defined by the crater-shaped depression. Given the irregular nature of a polydisperse arrangement, transverse dimensions can also be defined in combination by specifying an area covered by the crater-shaped depres- sion. An equivalent linear dimension characterizing a given crater-shaped depression may then be defined as the diameter of a circle with the same area.
  • microscale master features on the master surface are preferably densely packed, with neighbouring crater shaped depressions only being separated from each other by a ridge having a width that is comparable to or preferably less than the transverse linear dimension characterizing the crater-shaped depression.
  • the microscale master features are crater-shaped depressions.
  • the crater-shaped depressions appear more or less circular as seen in a vertical projection.
  • the crater- shape implies an outwardly sloped sidewall providing a positive release angle facilitates de-moulding of the shaped item.
  • the vertical profile of the microscale structured master surface has a peak-to-peak amplitude of at least ⁇ , ⁇ or at least 1 m and below 30 ⁇ , below 20 m, or preferably below 10 ⁇ .
  • the lateral pattern of the microscale structured master surface has an area density of microscale master fea- tures of at least 5000/mm 2 , at least 8000/mm 2 , or at least 10000/mm 2 .
  • the replication tool is particularly useful for producing parts comprising a microscale textured surface with a reasonably densely packed lateral distribution of microscale features.
  • high precision, fluid tight ultrasonic joints with improved bond strength are achieved.
  • the process according to the present invention will not exceed an inherent upper limit for the area density of the microscale lateral structuring.
  • Such an inherent limit is due to the fact that the microscale features produced by the microscale phase explosions according to the present invention require a minimum footprint in order to be resolved.
  • the present invention produces polydisperse features with a distribution that may include submicron elements, their average (most prominent) lateral dimensions are in the microscale.
  • Increasing the area density of the microscale features results in an increasing proba- bility for the occurrence of overlap between adjacent microscale features.
  • the microscale features are overlapping to such an extent that they appear merged and effectively have a much larger lateral extension than a targeted feature size of individual, unmerged microscale features.
  • a critical area density such merged features increasingly dominate the actual fea- ture size produced on the replication tool.
  • the merged features are then counted as a single feature with a larger lateral dimension or foot print.
  • This effect is best seen in a graph showing the area density of mi- croscale features, e.g. counted in a given surface portion by means of image analysis, as a function of the laser energy exposure applied to that surface portion.
  • a graph shows the area density of mi- croscale features, e.g. counted in a given surface portion by means of image analysis, as a function of the laser energy exposure applied to that surface portion.
  • a graph is shown in Fig.19.
  • the data shown has been ob- tained by an analysis of the microscale structuring applied to more than 70 replication tool blanks (tool grade aluminium as specified elsewhere in this application) using the method according to the invention.
  • the ordinate shows the exposure dose expressed in terms of the number of repetitions divided by the scan speed; the coordinate shows the area density of holes detected by an image analysis performed on micrographs of the processed surface; and the marker size indicates the size of the detected feature determined by the same image analysis algorithm.
  • the individual microscale features are resolved and all have essentially the same size.
  • the initial regime covers a low density regime up to about 5000/mm 2 where the distribution of the microscale features may be consid- ered as sparse.
  • an intermediate exposure regime above about 5000/mm 2 the microscale features may be considered as more and more densely packed, reaching a critical density of about 12000/mm 2 , where overlap of adjacent microscale features begins to become significant.
  • the critical density is the maximum achievable density for a given system, which in the example of Fig.19 is about 12000/mm 2 .
  • Other material systems and laser processing set-ups may have a different maximum achievable area density, such as about 100000/mm 2 , or about 50000/mm 2 , or 20000/mm 2 , or about 15000/mm 2 .
  • An inherent limit to the maximum achievable area density is given by the requirement of microscale dimensions of the lateral structuring as achieved by the present invention. Increasing the exposure beyond the criti- cal value then only results in merging of the microscale features and in a deterioration of the desired patterning.
  • the mi- croscale features are adequately dimensioned in their lateral extend, yet are packed sufficiently dense so as to achieve a significant wetting behaviour enhancement.
  • An adequate range may be determined by an exposure experiment as outlined in Fig.19, wherein preferably the area density is at least 60%, at least 70%, at least 80%, or at least 90% of the maximum achievable area density of microscale features.
  • the wetting behaviour enhancement of the replicated item also deteriorates more and more.
  • the microscale master features have an aspect ratio of a vertical dimension to a lateral dimension of at least 1 :2, or about 1 :1 , wherein the vertical dimension is the peak-to-peak amplitude and the lateral dimension is the square root of the average footprint area per microscale master feature, which for a given microscale structured surface area is cal- culated as the inverse of the area density of microscale master features per area, i.e. the area of the given surface in lateral projection divided by the count of microscale features in that area.
  • the above-mentioned replication tool and methods are adapted such that the lateral arrangement of microscale protrusions in addition to the flange portions includes further portions on the surface of the first part.
  • the further portions on the surface of the first part may be functionalised by applying a microscale textured replica surface to these further portions in the replication process.
  • the replication tool is adapted by applying the above-mentioned laser treatment to generate microscale phase explosions also to further portions on the tool surface, in addition to flange portions.
  • the parameters of the laser treatment may be kept the same or set differently for different portions of the tool surface to generate different microscale structured master surface portions depending on the purpose of the respective portions of the mi- croscale textured replica surface to be produced therefrom.
  • microscale texturing of the replicated flange portions is to act as energy directors, whereas the purpose of the microscale texturing of the replicated further portions may be another functionalization.
  • a microscale textured replica surface produced according to any of the herein disclosed methods also exhibits enhanced wetting properties.
  • the microscale textured replica surface may exhibit enhanced hydrophobicity or even superhydrophobicity, provided that the surface material is hydrophobic.
  • a microscale textured replica surface produced according to any of the herein disclosed methods may also exhibit enhanced hydrophilicity, provided that the surface material is hydrophilic.
  • wetting properties refers to the interracial interactions in a system comprised of three states of matter, a solid, a liquid, and a gas, and can be quantified by a contact angle.
  • the line connecting all three interfaces e.g. solid-liquid, solid-gas, liquid-solid, is denoted the three phase-contact line.
  • the contact angle is defined as the angle between the tangents of the liquid-gas and the liquid-solid interphases perpendicular to the three-phase line at any intersection of the two tangents on the three phase line.
  • the wetting properties between a solid and a liquid in a three phase system are considered enhanced with respect to the wetting properties of a flat surface if the apparent macroscopic contact angle is altered by the structure on the surface, wherein the wetting properties of a system with a solid-liquid contact angle smaller than 90° (philic behaviour) is considered enhanced if this contact angle is reduced by the modification (philic enhancement).
  • the wetting properties of a system with a solid-liquid contact angle greater than 90° is considered enhanced if this contact angle is increased by the modification (phobic enhancement).
  • the laser treatment of the tool surface may be the same for all portions, since the microscale texturing may simultaneously act as microscale energy directors and provide enhanced wetting properties as compared to a flat unstructured surface of the surface material.
  • the laser treatment of the tool surface may be varied for different portions thereof.
  • the laser treatment of flange portions may be optimised for the purpose of forming energy directors for use in the formation of an ultrasonic joint, whereas the laser treatment of further portions of the tool surface may be optimised for producing enhanced wettability on the further portions of the replicated part.
  • the further portions of the microscale textured replica surface on a formed item are adapted to exhibit enhanced hydrophobicity, or even super-hydrophobicity.
  • the replica material is hydrophobic or the microscale textured replica surface is covered with a hydrophobic layer.
  • the further portions of the microscale textured replica surface on a formed item are adapted to exhibit enhanced hydro- philicity, or even super-hydrophilicity.
  • the replica material is hydrophilic or the microscale textured replica surface is covered with a hydrophilic layer.
  • microscale texturing of the replicated first part produced by replication from a microscale structured master surface on a replication tool may thus serve multiple purposes. This may e.g. be useful in providing a packaging having a functionalised surface, such as a superhydrophobic surface, and at the same time allowing for a formation of a precise and reliable ultrasonic joint with a high degree of design freedom.
  • a dual use of the microscale texturing applied to flange portions and further portions may be useful in microfluidics, when forming sealed channels and/or reservoirs that may thus be provided with inner surfaces with an enhanced wettability, such as enhanced hydrophobicity or enhanced hydro- philicity as explained above.
  • a material is referred to as hydrophobic, if a flat surface thereof is characterized by a water contact angle of above 90 degrees, such as above 95 degrees, such as about or above 100 degrees. Accordingly, a material is referred to as hydrophilic, if a flat surface thereof is characterized by a water contact angle of below 90 degrees, such as below 85 degrees, such as about or below 80 degrees.
  • a flat surface of the hydrophilic plastics material acryloni- trile butadiene styrene (ABS) may have a water contact angle of about 81 degrees.
  • FIG. 1 a-c SEM micrographs of a microscale structured master surface at different magnifications
  • FIG. 2a-c SEM micrographs of a microscale textured replica surface at different magnifications
  • FIG. 3 a SEM micrograph of another microscale structured master surface
  • FIG. 4 a SEM micrograph of the microscale textured surface of an injection moulded item (polypropylene) using an isotherm process
  • FIG. 5 a SEM micrograph of the microscale textured surface of an injection moulded item (polypropylene) using a variotherm process
  • FIG. 6 schematically, the surface modification of a tool surface by pulsed laser treatment to generate microscale phase explosions
  • FIG. 7 schematically, an injection moulding process according to one embodiment of the invention
  • FIG. 8 schematically, an extrusion coating process according to a further embodiment of the invention
  • FIG. 9 schematically an ultrasonic welding process according to one embod- iment of the invention.
  • FIG. 10 schematically an assembly formed using an ultrasonic welding process as shown in Fig.9, FIGS.1 1-14 four graphs plotting hole size and hole density on a microscale structured master surface for different parameter settings of the pulsed laser treatment of the tool surface, and in FIGS.15-18 four graphs plotting hole density on a number of microscale structured master surfaces against the scan speed used during the pulsed laser treatment of the respective tool surfaces;
  • Fig. 19 a graph plotting hole density on a number of microscale structured master surfaces against the exposure in terms of repetitions divided by scan speed used during the pulsed laser treatment of the respective tool surfaces;
  • suitable materials are materials commonly used as inlays or mould materials in e.g. injection moulding or extrusion coating processes. These materials of the tool surface suited to be modified by pulsed laser treatment to generate mi- croscale phase explosions include Aluminium alloys, such as so-called 1050 aluminium, 5754 aluminium, or 2017 aluminium, as well as tool steel, such as Sandvik corona C60 and orvar 2343.
  • Figs.1 a-c show micrographs taken by scanning electron microscopy (SEM) of an aluminium tool surface, more particular a tool surface made of 2017 aluminium, which has been modified by pulsed laser treatment using a picosecond laser with a maximum power output of 50 W operating at a pulse frequency of 200 kHz and at a wavelength of 1064 nm.
  • the surface was scanned repetitively at a given power setting in per cent of the maximum power output and with a given speed.
  • the laser beam was incident on the tool surface in a vertical direction, wherein the laser was slightly defocused by shifting the focal point by 1 ,3mm in a vertical direction with respect to the tool surface to be modified.
  • a line scan of the laser produced a modified trace width of about 10 ⁇ ⁇ 5 ⁇ .
  • a broader trace as the one shown in Fig.1 a and 1 b was obtained by a meander line scan with adjacent legs of the meander shifted in a direction perpendicular to the scanning direction. Thereby an arbitrary area can be covered by a microscale surface structure.
  • the laser treatment results in an ablation of some of the tool surface material.
  • the parameters of the pulsed laser treatment are, however, adjusted such that the bottom of the trace exhibits a lateral arrangement of polydisperse microscale master features, see e.g. Fig.1 b.
  • the microscale master features obtained by this pulsed laser treatment are crater-shaped depressions.
  • the crater-shaped depressions at the bottom of the trace are a consequence of the localized pulsed laser treatment generating microscale phase explosions.
  • Fig. 3 shows a SEM micrograph of tool surface made of tool steel, more particular Sandvik corona C60 tool steel, which has been modified by pulsed laser treatment using the same picosecond laser with a maximum power output of 50 W operating at a pulse frequency of 200 kHz and at a wavelength of 1064 nm.
  • the surface was scanned repetitively at a given power setting in per cent of the maximum power output and with a given speed.
  • the laser beam was incident on the tool surface in a vertical direction, wherein the laser was slightly defocused.
  • the localized pulsed laser treatment generates microscale phase explosions resulting in a lateral arrangement of polydisperse microscale master features, wherein the microscale master features are crater-shaped depressions.
  • Figs. 2a-c show an example of a microscale textured replica surface on a mould insert for injection moulding, as observed in a scanning electron microscope at different magnifications, wherein the width of the image corresponds to 1.2mm in Fig.2a, 0.23mm in Fig.2b, and 0.03mm in Fig.2c.
  • the mould insert for injection moulding was designed and fabricated in 2017 aluminium alloy (Metal Centret, Denmark) by micro milling using conventional techniques to provide a tool surface defining the general shape of the part to be fabricated.
  • microscale structured master surface on the tool surface, a 1064nm, 200kHz, 50W (max power) picosecond laser (FUEGO, Time Bandwidth) mounted in a microSTRUCT vario (3D- Micromac AG) was used to generate microscale phase explosions on the tool surface, thereby producing a densely packed lateral arrangement of microscale crater- shaped depressions.
  • the area intended for structuring was irradiated by the laser in parallel lines separated by 20 ⁇ . In the example shown in Figs.2a-c, this pattern was repeated 20 times, and the laser power was set to 25% of the max power.
  • Fo- cus was offset by +1 .3 mm above the surface.
  • the microscale structured master surface produced in this example consisted of 10 lines (200 ⁇ wide) and was 305.5 mm long.
  • the part with the microscale textured replica surface thereon was replicated from this replication tool with the microscale structured master surface on its tool surface using a Victory 80/45 Tech injection moulder (Engel, Schwertberg, Austria).
  • the polymer substrate used for injection moulding was cyclic olefin copolymer (COC) TOPAS grade 5013L-10 (TOPAS Advanced Polymers, Dusseldorf, Germany) with a glass transition temperature (Tg) of 135 C.
  • Injection temperature of the polymer was 270 C and the mould temperature was kept stable at 120 C.
  • the injection moulding was performed in isothermal mode.
  • microscale sur- face texturing is depicted in Figs.2a-c.
  • the microscale textured replica surface on this first part is adapted to act as microscale energy directors for forming an ultrasonic welding joint with a cooperating second part.
  • Further examples for the microscale textured replica surface on replicated parts are given in Figs.4 and 5.
  • the laser structured aluminium insert was installed in a Victory 80/45 Tech injection moulder (Engel).
  • the respective surfaces have been characterised with respect to the shape of the microscale features on the microscale textured surface of the replicated item, see Fig.4 and Fig.5.
  • the isothermal process results in a surface texture with rounded tops, see Fig.4, and the variothermal process results in a surface texture with a hairy appearance ("pulled polypropylene"), see Fig.5.
  • Both surfaces faithfully replicate the lateral pattern of the master, but only provide a low fidelity replication of the vertical profile of the master. Nevertheless, both processes result in a fast replication of parts with microscale energy directors on flange portions thereof.
  • the isothermal process is preferable for high throughput or high volume production, because the isothermal moulding process is not time limited by any process step(s) involving temperature adjustments of mould and/or mould inserts, whereas the variotherm moulding process is partially time limited by one or more process step(s) involving temperature adjustments of mould and/or mould inserts.
  • Fig.7 shows schematically an injection moulding process for producing a replicated part 4.
  • the process uses a mould having mould parts 1 a and 6, wherein mould part 6 has an insert 1 b.
  • Tool surfaces 2a, 2b, 7 define a general shape of the replicated item 4.
  • Tool surfaces 2a, 2b are provided with microscale structured master surfaces 3a, 3b, 3c, 3d, which are replicated on the item 4 as microscale textures 5a, 5b, 5c, 5d respectively.
  • Fig. 8 shows schematically an extrusion coating process for coating a substrate web S, with a coating 14.
  • the process uses a roll 1 1 , 1 1 a with a tool surface 12, 12a defining a general shape of the coating.
  • the tool surface comprises microscale structured master surfaces 13, 13a, which are replicated as microscale surface texture 15 on the coating 14.
  • a microscale structured master surface 13 may be applied directly to the tool surface 12 of the roll 1 1 and/or a microscale structured master surface 13a may be applied to the tool surface 12a of a replication tool insert 1 1 a for attachment to the roll 1 1.
  • Fig.6 shows schematically the configuration of the set-up for localized pulsed laser treatment of a tool surface 2 on a replication tool 1 to generate a microscale structured master surface 3 by scanning a pulsed laser beam 99 over the tool surface.
  • the example illustrates different ways of identifying suitable laser processing parameters for modifying a given tool surface to obtain a microscale structured master surface.
  • Aluminium 2017 (available from “Metalcenteret” Glostrup, Denmark) was surface structured using a 1064nm, 200kHz, 50W picosecond laser (FUEGO, Time Bandwidth) mounted in a microSTRUCT vario (3D-Micromac AG).
  • FUEGO Time Bandwidth
  • 3D-Micromac AG microSTRUCT vario
  • the average dimension and standard deviation of the hole sizes may be adjusted by varying parameters such as laser power in percent of maximum power output, scanning speed, number of cross repetitions and z offset of the focus plane.
  • parameters such as laser power in percent of maximum power output, scanning speed, number of cross repetitions and z offset of the focus plane.
  • the optimal parameter settings for achieving a desired hole size population and hole density in the alloy in question one may map the parameter space of the laser settings. When replicated in polymer, the hole size population and hole density will determine the surface structure and roughness and hence the final wetting properties of the polymer piece.
  • the parameter space was for the
  • Scan Speed in mm/s from 150 to 1950 (both included), in increments of 100; and from 600 to 4200 (both included), in increments of 200;
  • the parameter coordinate with the highest (scan speed / cross repetition) value, and hence lowest process time is preferred.
  • the high intensity (slow speed) results in few but large holes
  • Fig. 13 shows that for the numerical value of the ratio of repetitions over scan speed (in mm/s) equal to 0.01 a more densely packed and uniform hole formation is achieved.
  • Figs.15-18 show four graphs plotting hole density against the scan speed used during the pulsed laser treatment of the respective tool surfaces. At speeds ⁇ 1250 mm/s, the hole density is consistent regardless of other parameters than speed, and it is concluded that writing speed is the main determining factor in this regime. At speeds ⁇ 1250 mm/s, the hole density varies with the number of cross repetitions. This is true, even when the product (power X repetitions) is kept constant, (see Fig. 16). Marker size represents cross repetitions in Fig.15 and (cross repetitions X power) in Fig.16.
  • the coefficient of variance (CV) of hole size is observed to be stable in the regime where (speed ⁇ 1250 mm/s), see Fig.17, and accordingly for the standard deviation (STD), see Fig.18.
  • Marker size represents hole size CV in Fig.17 and hole size STD in Fig.18.
  • the laser focus parameter space may be mapped to identify applicable laser settings.
  • Fig. 9 shows schematically a process for forming an ultrasonic welding joint between a first part 40 and a cooperating second part 50.
  • the first part 40 is a replicated part produced using a microscale structured replication tool in a method as described before.
  • the first part 40 has a general shape as defined by the tool surface of the replication tool.
  • the general shape includes flange portions 41 , 42 carrying microscale textured replica surfaces 43, 44 with a lateral arrangement of microscale protrusions, and a recessed portion 45.
  • the second part 50 has cooperating flange portions 51 , 52 facing towards the flange portions 41 , 42 of the first part and are aligned with these flange portions 41 , 42 of the first part.
  • the first and second parts 40, 50 are brought in contact with each other such that the tops of the microscale protrusions on the first flange portions 41 , 42 form point contacts with the corresponding second flange portions 51 , 52.
  • the parts are clamped in an ultrasonic tool 60, here schematically represented by an ultrasonic horn.
  • the ultrasonic tool 60 is adapted for applying ultrasonic energy while applying a uniaxial pressure in the direction of arrow 61 across the contact interface.
  • the ultrasonic energy is dissipated in the contact region, thereby melting the material with an axial pressure applied across the interface to form a welding joint.
  • FIG. 10 shows schematically the assembly 90 formed by welding the first part 40 and the second part 50 together, thereby forming a cavity 95 defined by the recess portion 45 of the first part 40 and the second part 50.
  • the second part 50 forms a lid, which is sealed fluid tight to the first part 40 by the ultrasonic welding joints 92, 94.
  • the following is an example of a welding joint formed between a polymer part and a sheet of cyclic olefin copolymer (COC).
  • Ultrasonic welding of the polymer part to a 152 ⁇ thick COC sheet was done using a Telsonic-USP4700 ultrasonic welder (Telsonic, Herstad+Piper, Denmark).
  • the chip welding was conducted by depositing 45 J at 90% amplitude, 20 kHz and with a normal force on the piece of 600 N.
  • the normal force could generally be estimated from area (x y cross section) as 10 MN/m2:
  • the amount of energy required can be estimated from the volume of the energy directors.
  • microscale structured energy directors for ultrasonic welding of microfluidic systems with a lateral arrangement of microscale features, which in this example are referred to as micropillars.
  • the micropillar EDs are produced by replicating microscale crater-shaped depressions in a mold to obtain cone like protrusion (CLP) structures on the surface of the replicated part.
  • CLP cone like protrusion
  • the microscale crater-shaped depressions are introduced on an injection mould surface using a pico-second laser and may therefore be added to any mould surface acces- sible to a pico-second laser beam.
  • the replication tool For device fabrication based on replication techniques (e.g. hot embossing and injection moulding), the replication tool has the inverse structure and the ED structures thus have to be realized as depressions in the bottom of the cavity structure used to define the channel wall.
  • ED structures can be realized, e.g., by micro milling, which is a rapid mould tool fabrication process, though the size of the milling tool limits the ED dimensions that can be realized. Milling tools are made as small as 10- 50 ⁇ , yet it is often not feasible to make EDs on high-aspect ratio wall structures by milling, since the drill aspect ratio is often limited to 1 :3, and the micro mills are short and mounted on large shanks.
  • micropillar EDs are used for ultrasonic welding (UW) of microfluidic systems.
  • the EDs are formed by introducing cone-like protrusion structures as a back-end processing of replication moulds using a picosecond laser.
  • the micropillar EDs have the substantial advantage over traditional EDs that they can be defined on any surface accessible to a high energy pico-second laser beam.
  • the micropillar EDs can be introduced in designated areas on the tool, and the width of these areas can be chosen independently from the heights of the EDs contrary to traditional EDs, where larger widths are accompanied by higher structures.
  • the CLPs are formed stochastically within the designated area exposed to the laser treatment, so only laser treatment of the general ED layout/shape is required, not an individual laser shaping of each of the individual CLPs.
  • the technology is demonstrated for an aluminium mould.
  • the CLP formation is verified for tool steel as used for high-throughput industrial moulds.
  • CLP-EDs are compared to micromilled EDs with respect to (1 ) welding strength, (2) structural deformation of a freestanding high-aspect structure, and (3) formation of particles during welding. No significant particle formation was induced by the process in the example. Chip fabrication
  • Injection moulding was carried out using a custom-made moulding tool comprising a 50 mm diameter disk cavity with 12 luer inlets.
  • the tool could be combined with mould inserts with structures machined in aluminium 2017 (al2017).
  • AI2017 was preferred for mould making in this example, due to its ease of machining.
  • the injection moulding was carried out on a Victory 80/45 Tech hydraulic injection moulding machine (Engel, Schwertberg, Austria) using COC grade 5013L-10 (TOPAS Advanced Polymers GmbH, Frankfurt-Hochst, Germany) with injection and mould temperatures of 270 °C and 120 °C, respectively. Injection pressure was 1766 bar.
  • Fabricated chips were bonded to a 500 ⁇ thick foil of COC grade 5013S-04 (TOPAS Advanced Polymers GmbH) by ultrasonic welding.
  • UW was performed at ambient temperature using a Telsonic-USP4700 ultrasonic welder (Telsonic, Erlan- gen, Germany), depositing 25 J with 75% vibrational amplitude, a trigger force of 400 N and 0.5 bar welding pressure.
  • the vibrational amplitudes at the sample surface were approximately 44 ⁇ .
  • the bonding strength was assessed using the razor-blade test based on fracture propagation developed by Maszara et al., J. Appl. Phys. 64 (1988) p.4943, and employed by Matteucci et al., Microelectron. Eng. 1 1 1 (2013) p.294, to assess the bonding strength of thermal bonding in similar chips.
  • two mould inserts with a milled 5.15x42.5x0.25 mm 3 cavity were fabricated by micro milling.
  • the first insert further featured a 40.5 mm long conventional ED made by conventional milling and the second insert featured a laser micromachined ED with CLPs on an area of 40.5x0.2 mm 2 .
  • the injection moulded structures were bonded to a COC foil as described above.
  • FIGs 20a and 20b show scanning electron microscopy (SEM) images of the CLPs written in the al2017 mould. It is noteworthy that although the laser scanning is conducted in bundles of parallel lines, the formed CLPs are stochastically formed within the laser ablated area. This may be ascribed to the fact that the microphase explosions causing the CLPs are caused by a combination of metal impurities (alloy) picking up the energy, the pulsing nature of the laser beam and non-uniformity of the laser fluence distribution.
  • the CLPs have a typical height and spacing of 10 ⁇ and 10 ⁇ , respectively. On average, the CLP area protrudes 47 ⁇ from the plane of the tool (Fig. 23g).
  • Fig. 20c shows a SEM image of a COC replica of the mould.
  • the replicated structures are observed to have rounded tops due to imperfect filling during replication.
  • Fig. 20d shows tool steel Orvar2343 ablated to produce CLPs similar to those demonstrated in al2017.
  • FIGs 23a and 23b show SEM images of the CLP-EDs in the al2017 mould for fabrication of the high-aspect ratio microfluidic system. The images clearly show the feasibility of writing CLP-ED structures at the bottom of the trenches in the mould. Note that the separation and joining of bundles of laser lines do not alter the pattern and formation of CLPs. Thus, CLP-EDs can be formed in any pattern or geometry.
  • Corresponding SEM images of the injection moulded COC replica (Figs. 23c,d) clearly show that micropillar structures are well reproduced on the top of the high- aspect ratio wall.
  • Figures 23e and 23f show optical micrographs of the same structures pre and post UW.
  • the final micropillar CLP-EDs of the polymer chip are opaque (Fig. 23e). However, like conventional butt joint EDs, the joints are transparent post welding (Fig. 23f). It is noteworthy that no signs of trapped or com- pressed air are observed in structures surrounded by CLP-EDs, such as the pocket in the corner of the structure (Fig. 23e) where little or no gap is observed post UW in Fig. 23f. This indicates that the micropillar structure facilitates the escape of air during UW. SEM images Figs.23g and 23h highlight the position of CLP-ED polymer pre and post welding. Note the solidified polymer from the welding process in Fig.23h without any significant formation of "bonding flashes". This shows the high precision achieved with the bonding method of the invention.
  • Bonding strengths in terms of the surface energy, ⁇ (gamma), calculated from razor- blade tests are listed in Table 1 .
  • thermo- plastics is largest for structures bonded using ultrasonic welding. No significant difference is observed between conventional EDs and micropillar EDs.
  • Fig.21 shows a schematic drawing of the high aspect ratio chip with an outer channel 101 , and an inner channel 102 separated by walls 103. Cross sections (l-l, ll-ll, Ill-Ill) for confocal imaging are indicated. A bundle of 20 laser patterning lines 104 were added on the walls 103. Note that the 20 lines 104 are separated into two bundles of 10 lines each (104a, 104b) at the corners, to keep a constant edge distance of 180 ⁇ . First, it was verified that the microfluidic channels were leak-tight when filled with an aqueous solution containing fruit dye. Further, pressure testing with gas applied to the outer channel while leaving the inner channel at ambient pressure showed that the devices (three tested) could sustain pressure up to at least 9.5 bar (maximum pressure available in the test).
  • Fig.22 shows confocal imaging data (thick lines) of the free-standing wall structures of the device along the cross sections 1-3 (cf. Fig. 21 ).
  • the data of the three sections taken along the length of the parallel channel section (l-l, ll-ll, Ill-Ill) are over- laid on each other and fully coincide.
  • the confocal imaging data are further overlaid with the corresponding CAD file used for the mould fabrication. From the confocal images, it is derived that the channel height of the welded structure matches that of the design (2000 ⁇ ) with a tolerance of ⁇ 4.2 ⁇ . This value is smaller than the confocal image voxel height and we conclude that any height difference is below our detection limit.
  • This data further supports the particularly high precision of the bonding method according to the present invention.
  • the present example shows ultrasonic welding of microfluidic systems based on micropillar EDs according to one embodiment of the invention.
  • the mi- cropillar EDs are produced by replication of CLPs in aluminium, formed using a picosecond laser, and can be added to any mould surface accessible to a high power pico-second laser.
  • the example demonstrated the technology by injection moulding microfluidic devices featuring high-aspect ratio structures and shown that ultrasonic welding of the devices is possible with no detectable channel deformation.
  • the per- formance of the CLP-EDs was characterised showing that bonding strength is similar to conventional EDs, with no particle formation. The bonded devices could withstand 9.5 bar of hydraulic pressure without fracturing.
  • the laser processing method has further been demonstrated to work in high endurance tool steel used for making high performance injection moulding tools. Furthermore, the method of the invention supports a modification rate of 200 seconds/cm 2 and post processing capabilities on full three-dimensional mould surface shapes, as long as these are optically accessible.

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Abstract

The invention relates to a replication tool (1) for producing a part (4) with a microscale textured replica surface (5a, 5b, 5c, 5d). The replication tool (1) comprises a tool surface (2a, 2b) defining a general shape of the item (4). The tool surface (2a, 2b) comprises a microscale structured master surface (3a, 3b, 3c, 3d) having a lateral master pattern and a vertical master profile. The microscale structured master surface (3a, 3b, 3c, 3d) has been provided by localized pulsed laser treatment to generate microscale phase explosions. A method for producing a part (4) with microscale energy directors on flange portions thereof uses the replication tool (1) to form an item (4) with a general shape as defined by the tool surface (2a, 2b). The formed item (4) comprises a microscale textured replica surface (5a, 5b, 5c, 5d) with a lateral arrangement of polydisperse microscale protrusions. The microscale protrusions may be provided on a flange portion of a first part (40) and are configured to act as energy directors when forming an ultrasonic joint with a cooperating flange portion of a second part (50).

Description

MICRO-SCALE ENERGY DIRECTORS FOR ULTRASONIC WELDING
The present invention relates in one aspect to a replication tool and a method of providing the replication tool. In a further aspect, the present invention relates to a method of producing a part by replication, the part having a flange portion for use in the formation of an ultrasonic welding joint. In yet a further aspect, the invention relates to a method of joining two parts by ultrasonic welding.
BACKGROUND OF THE INVENTION
Ultrasonic welding is a technique for joining thermoplastics parts by applying high- frequency ultrasonic acoustic vibrations across the joint surfaces while pressing the parts together. The acoustic vibrations are absorbed by the thermoplastic material, which melts locally, thereby forming a welded seam. In a typical ultrasonic welding process, at least one of the flanges of the joint comprises pointed or knife edge type protrusions, so-called energy directors that concentrate the ultrasonic energy to the location where the weld is to be formed. Energy directors commonly known from industrial processes have several disadvantages, in particular when high precision welds with high weld strength are to be formed. Examples of such applications, where high precision to form a fluid tight weld seam is essential, are microfluidic chips, such as used for medical diagnosis or environmental testing. In such applica- tions, often a base chip with a system of microfluidic channels and components is formed e.g. as a replicated part in an injection moulding, compression moulding or hot embossing process. The base chip is then covered by a counter-part, which may equally comprise microfluidic channels and components, but may as well be a simple lid. The two parts are joined to form a fluid tight seal. Such joints may be formed e.g. by gluing, thermal bonding, or vapour bonding, but attempts have also been made to use ultrasonic bonding for joining such parts. In particular, ultrasonic bonding may overcome some of the challenges encountered with other bonding techniques, e.g. when packaging hazardous materials or sensitive reagents, where the other bonding techniques, due to the process parameters involved, are outright in- compatible with the product. However, the uncontrolled deformation of the energy directors during the ultrasonic welding process typically results in the occurrence of so-called flashes that may penetrate into the microfluidic channels, or may lead to uncontrolled cross-sectional dimensions of the microfluidic channels and components. Therefore, there is a need for a reliable and cost-effective process for forming an ultrasonic joint overcoming at least some of the above-mentioned disadvantages, or at least to provide an alternative to known methods. Furthermore, there is a need for suitable tooling for use in the above method of forming an ultrasonic joint. Furthermore, there is a need for a process for providing such suitable tooling.
SUMMARY OF THE INVENTION
A first aspect of the invention relates to a method of providing a replication tool, the method comprising providing a forming tool having a tool surface adapted to define a general shape of a part to be formed; modifying at least portions of the tool surface by a pulsed laser treatment to obtain a microscale structured master surface with a lateral master pattern and a vertical master profile; wherein the pulsed laser treatment is adapted to generate microscale phase explosions on the tool surface, thereby forming the microscale structured master surface as a lateral arrangement of microscale crater-shaped depressions. The crater-shaped depressions obtained by the microscale phase explosions are irregular in shape and polydisperse, i.e. varying in size with a spread about a most prominent size. The size may e.g. be characterized by the area covered by the depression as seen in a vertical projection on a lateral plane.
The microscale structuring of the tool surface is provided by the localized application of laser pulses directly to selected portions of the tool surface. This post-treatment of the tool surface by means of localized laser treatment has the advantage that the replication tool with the shape defining tool surface may be designed and produced using existing techniques and equipment for tool making, thereby contributing to a relatively simple and cost effective implementation of the surface modification in an existing fabrication process. At the targeted portion of the tool surface, the localized pulsed laser treatment is adapted to melt and evaporate material at the tool surface to generate microscale phase explosions, thereby producing a randomised surface structure of polydisperse microscale features. The microscale surface features are depressions, which are typically crater shaped with steeply sloped side walls. The process of provoking mi- croscale phase explosions by locally applying laser energy to the tool surface so as to form the crater-shaped depressions is stochastic in nature, wherein upon appropriate exposure the microscale surface features are densely packed and may even partially overlap, thereby forming a microscale lateral pattern with a microscale po- rous appearance. The localized application of laser power may be scanning a laser spot along a predetermined scanning path at a pre-determined scan speed over the tool surface. The path may follow a single scan along the path over the tool surface, a repetitive scanning along the same linear path, or a combination of both. The path is adapted to cover the selected portions of the tool surface. The path may e.g. be straight, curved, meandering, segmented or a combination thereof and some sections of the path may overlap other sections of the path in order to achieve an even exposure of the selected portions of the tool surface with laser energy.
The pulsed laser radiation has to be of a wave length and pulse characteristics that is absorbed by the tool surface in order to be able to locally melt and evaporate material from the tool surface so as to produce microscale phase explosions creating the crater-shaped depressions. For example, the laser radiation may be from a picosecond-laser source with a wavelength in the near infrared, such as 1064 nm, but other wavelength ranges, e.g. in the visible part of the electromagnetic spectrum, and pulse characteristics that are suitable for locally heating the tool surface to generate microscale phase-explosions may be conceived, too. The finish of the targeted portions of the tool surface is controlled by adapting the exposure of these tool surface portions with the pulsed laser radiation. The exposure of the tool surface is controllable e.g. by adjusting the laser power/spot intensity and/or by varying the scan speed, wherein exposure of a given surface portion increases with increasing laser power, but decreases with increasing scan speed. The finish of the targeted portions of the tool in turn determines the finish of the replicated part in the corresponding regions on the surface of the part via the replication process. Furthermore, multiple exposures of the same surface portions, e.g. by repetitive and/or overlapping scan- ning of the laser spot over these surface portions, results in an exposure that is increased correspondingly.
Preferably, the lateral pattern of the microscale structured master surface has an area density of microscale master features of at least 5000/mm2. Thereby, a rea- sonably densely packed lateral distribution of microscale features on the master surface is achieved, thereby allowing for producing parts with a replicated microscale surface texture that is useful for forming high precision, fluid tight ultrasonic joints with improved bond strength.
Further preferably, the lateral pattern of the microscale structured master surface has an area density of microscale master features of at least 8000/mm2, or even of at least 10000/mm2. Thereby, a densely packed lateral distribution of microscale features on the master surface is achieved, thereby allowing for forming high preci- sion, fluid tight ultrasonic joints with particularly improved bond strength. It should be noted that an upper limit for the area density resulting from the microscale of the surface structuring exists, which is discussed in detail further below.
A further aspect of the invention relates to a method of producing a first part having a flange portion for use in the formation of an ultrasonic welding joint with a cooperating second part, the method comprising the steps of providing a replication tool with a microscale structured master surface by a method according to the above-mentioned embodiment; and using the replication tool to form the first part by the replication process, wherein the formed first part has the general shape as defined by the tool surface, and wherein the formed first part comprises a microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions on at least the flange portion of the first part.
Preferably, the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 5000/mm2. As mentioned above, this allows for forming high precision, fluid tight ultrasonic joints with im- proved bond strength.
Further preferably, the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 8000/mm2, or even of at least 10000/mm2. As also mentioned above, this allows for forming high precision, fluid tight ultrasonic joints with particularly improved bond strength. An upper limit for the area density resulting from the microscale of the cone-like protrusions forming the surface texture exists, which is discussed in detail further below. The method is useful for forming the first part from a replication material replicating the microscale structured master surface onto the first part to form a surface region with a lateral arrangement of polydisperse microscale energy directors shaped as polydisperse microscale protrusions on the first part. A lateral replica pattern is defined by the lateral master pattern, and a vertical replica profile has finite peak-to- peak amplitude to form a three-dimensional texture. Since the lateral replica pattern is defined by the lateral master pattern, it is equally irregular as seen in a projection onto a lateral plane, and the microscale protrusions are polydisperse. The method is for producing the first part by a fast replication process using the replication tool, such as required by a commercially viable production of the item in large numbers.
As mentioned above, the laser treatment of the tool surface results in a porous surface appearance produced by a randomised lateral arrangement of, preferably densely packed, microscale depressions, which are typically shaped as relatively deep, steep-walled craters with a more or less pointed bottom. The sloped sidewalls facilitate an easy de-moulding of the replicated item in the step of releasing the item from the tool surface.
Since the method is useful for the production of first parts by a fast replication process, it allows for a low-cost and/or mass production of the first part with a first flange portion that is prepared for ultrasonic bonding with a cooperating second flange portion on a second part by providing the first flange portion with microscale energy directors. A replication process may be considered fast, for example, if the replication period from contacting the tool surface with the molten replication material to releasing the formed part is short, such as well below ten minutes, such as less than five minutes, such as less than 3 minutes, such as less than one minute, such as less than 30 seconds, or even less than 10 seconds. In particular, the suggested thermally controlled replication process using a thermoplastic replication material can be performed fast as compared to for example replication processes using thermosetting replication materials, or chemically setting replication materials. How- ever, the method is also useful for the production of first parts having a flange portion with microscale energy directors thereon by other replication techniques, such as the mentioned slower methods using thermosetting or chemically setting replication materials, or for replication techniques like compression moulding and hot em- bossing.
The term microscale refers to dimensions of about 1 μηη to 1000 μηη that are generally measured in microns (micrometres), typically in the range of about 1 μηη to 100 μηη. Accordingly, the term nanoscale refers to dimensions of about 1 nm to 1000 nm that are generally measured in nanometres, typically in the range of about 1 nm to 100 nm.
The microscale structure of the master surface and, accordingly, the microscale texture of the replica surface have a three-dimensional topography of microscale elements arranged next to each other and may be decomposed in a lateral pattern and a vertical profile. The term "lateral pattern" refers to the arrangement in lateral directions of the (3D) microscale elements making up the microscale structure/texture, as seen in vertical projection on to a lateral plane. The term "vertical profile" refers to the variation of the location of the surface in a direction perpendicu- lar to the lateral directions.
When a surface structuring/texturing is applied to an object having a general shape, such as a tool surface or an item, the surface structuring/texturing can be seen as a vertical variation of the surface, which is added to the general shape of the tool sur- face/item. Accordingly, on an object with a microscale structured/textured surface, an average surface that flattens out any vertical variations of the surface by averaging on a lateral scale larger than that of the microscale structuring/texturing essentially follows the general shape of the object. The general shape of the object is thus defined independent of any nano- or microscale surface roughness / finish / structur- ing. At a given point on the surface of the object, lateral directions are parallel / tangential to a surface defining the general shape of the object on a scale larger than the scale of the lateral pattern. Accordingly, the vertical direction at a given point on the surface of the object is the surface normal to the general shape in that point. In each given point, the vertical direction is perpendicular to the corresponding lateral directions.
The general shape of the replicated part is defined by the general shape of the tool surface. The replication process is for accurately replicating the general shape of the part as defined by the tool surface. The surface of the replicated part is functional- ised by applying a surface finish with a microscale texture at least on selected regions of the surface of the part. The particular functionalization is to make a flange portion of the replicated part susceptible to concentrate ultrasonic energy so as to act as a distributed energy director when forming an ultrasonic joint with a cooperating flange portion of a counterpart. To concentrate the ultrasonic energy applied across the interface between the first and second flange portions, the area of contact is reduced to point contacts where the tops of the protrusions meet the surface of the counterpart when the first flange portion is brought in contact with the cooper- ating second flange portion.
The protrusions are sacrificial; Upon formation of the joint, the protrusions are flattened out by the ultrasonic energy dissipated and the pressure applied. The material of the energy directors spreads in lateral directions, but is easily absorbed on the spot also on a microscale, due to the lateral interspaces between the protrusions. Thereby, the quality and precision of the ultrasonic joint is improved, and the formation of undesirable "flashes", i.e. the spreading of material into regions adjacent to the ultrasonic joint, is avoided. An important advantage of the present method is that the laser treatment of the tool surface is only limited by the requirement of an optical access to the surface to be modified. Consequently, a microscale structured master surface may be applied to virtually any surface topology, including very narrow and deep trenches or holes, as long as a laser beam can be guided to the tool surface to be modified. This allows for an improved freedom for designing the ultrasonic joint and accordingly for designing the replicated parts to be assembled. Furthermore, at the choice of the designer, the microscale protrusions may be distributed over the entire flange portion of the replicated parts or only to selected regions thereof. Also, the flange portion may be arbitrarily shaped as seen in the lateral direction, e.g. the flange portion may easily be adapted to cover larger surfaces. The microscale energy directors may even be arranged on curved and/or oblique surfaces following a more complex general shape of the replicated part, thereby adding to the above-mentioned improved freedom of design.
According to some embodiments, the method comprises the steps of (a) providing a replication tool having a tool surface adapted to define a general shape of the first part, wherein the tool surface comprises a microscale structured master surface obtained by localized pulsed laser treatment of the tool surface to generate mi- croscale phase explosions, said microscale structured master surface having a lateral master pattern and a vertical master profile; (b) contacting the tool surface with a replication material in the melt phase, wherein the tool surface is maintained at a process temperature below a melt temperature of the replication material, thereby (c) cooling the replication material to a stabilized shape with a microscale textured replica surface, wherein the lateral master pattern defines a corresponding lateral replica pattern of the microscale textured replica surface and wherein the amplitude of a vertical profile of the microscale textured replica surface is in the microscale, and (d) releasing the shaped item from the tool surface. A replication process, where the tool surface is maintained at a more or less constant temperature below the melt temperature throughout the production process is sometimes referred to as an "isothermal" type process. Isothermal processes may be performed at high throughput. As also mentioned above, the truthfulness of the replication of the vertical profile of the microscale master structure is uncritical as long as the peak-to-peak amplitude of the vertical profile of the micro-texture on the replica surface is sufficient, and further preferably the lateral pattern is faithfully transferred.
Alternatively, e.g. in a so-called variothermal injection moulding process, the mi- croscale structured master surface is prior to contact with the replication material heated to an injection temperature above the melting temperature of the replication material, but immediately upon injection of the replication material rapidly cooled to a temperature below the melting temperature of the replication material, at which the first part is finally released from the mould. Further according to some embodiment the replication process is one of injection moulding, hot embossing, compression moulding, and extrusion coating. Further according to one embodiment of the method, the microscale textured replica surface has a peak-to-peak amplitude of at least 0.5μηι, or at least 1 μηι and up to 5μηι, or up to Ι Ομηη, or even up to 30μηι. A minimum vertical profile required to form a 3D textured surface suited for forming point contacts between cooperating first and second flange portions. To achieve a concentration of the ultrasonic energy to point contacts, the exact 3D-shape of each of the microscale features on the tool surface and their exact arrangement with respect to each other is not critical. Also, the exact details of the individual microscale elements and of their arrangement making up the micro-texture on the surface of the replicated item are uncritical for achieving a concentration effect by the microscale energy directors. The fast replica- tion process thus yields proper items as long as the general shape is faithfully obtained reliably, the microscale lateral pattern is reliably reproduced in each reproduction process, and the peak-to-peak amplitude of the vertical profile of the replica surface is adapted to provide point contacts between the tops of the protrusions on the first part and the cooperating flange portion of the second part. Reduced ampli- tude gives less "flashes", but requires corresponding precision in the flatness/fit of the cooperating first and second flange portions. Relatively small amplitudes of the vertical profile of the texture of the replica surface may already achieve a sufficient concentration of ultrasonic energy into point contacts, such as amplitudes of at least 100nm, alternatively at least 200nm, alternatively at least 500nm, and preferably in the microscale, such as Ι μηΊ-Ι ΟΟμηΊ, such as 1 μηΊ-30μΓη, preferably in the range Ι μηΊ-Ι ΟμηΊ. For ensuring a good production yield it is therefore sufficient to control the lateral scale of the texture which is well controlled by the lateral scale of the pattern of the master surface - and ensuring that the amplitude of the profile of the texture on the replica surface exceeds the local flatness of the cooperating flange sur- face so as to reliably form distributed point contacts between the top of the protrusions and the surface of the counterpart. A further important insight therefore relates to the nature of the fast replication process. Here, it is exploited that the lateral pattern of the microscale master structure on the tool surface is inherently reproduced with high fidelity on the replicated item. The fidelity of replication of the vertical pro- file on the other hand tends to be affected by standard parameters of processes for fast replication in thermoplastic materials, such as tool temperature, replication period, and temperature and/or pressure of the thermoplastic replication material in the melt phase. This is owing to the ability of the thermoplastic replication material to fill the depressions of the relatively deep steep-walled master structure before solidifying, which may be controlled by these parameters. Thereby, the fidelity of replication may be controlled. For example, fidelity of microstructure replication may be reduced by reducing the temperature at which the tool surface is maintained. When the replication material contacts the tool surface at the lower the melt is cooled more rapidly, thereby increasing the viscosity of the melt and impeding the filling of the microscale depressions/crevices/craters/pores of the master structure on the tool surface by the melt before it solidifies. A reduced fidelity is reflected by a reduced amplitude of the replicated profile as compared to the master profile: the replication is more shallow than the master. The fidelity of replication of the vertical profile may thus be characterised e.g. by comparing the peak-to-peak amplitudes of the vertical profiles of the replicated microscale texture and the microscale master structure to each other, wherein for a low fidelity replication the amplitude of the replicated profile as compared to the master profile is lower than for a higher fidelity replication. Typically, the low-fidelity replicated microscale textures exhibit a rounded top. Since the energy concentration is uncritical as to the exact shape and arrangement of the individual microscale features, another advantage of the method is that it facilitates a relatively simple and cost effective implementation of the surface functionalization in an existing fabrication process by merely modifying the tool surface of a replication tool in a post-treatment step.
Further according to one embodiment of the method, the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 5000/mm2, at least 8000/mm2, or at least 10000/mm2. Preferably, the protrusions are densely packed to provide a good mechanical strength of the joint. Furthermore, a densely packed lateral arrangement of the protrusions also ensures good fluid sealing properties of the ultrasonic joint, e.g. when forming hermetically sealed chambers or channels. Note that the part may be made entirely from replication material with a shape defined by the tool surface, or the replication material may be applied to/carried by a substrate material, e.g. in an additive moulding step or a coating step. Further according to one embodiment of the method, the replication process used for producing the part is injection moulding. Injection moulding is a cyclic replication process with a fast cycle time, i.e. using this embodiment a large number of separate items with a microscale textured replica surface may be produced at high throughput. The inner surface of the injection mould is the tool surface defining the general shape of the part. At least portions of the tool surface have a finish with a microscale structuring generated by localised treatment with a pulsed laser source. The thermoplastic replication material is heated to above the melt transition temperature and in the melt phase injected into the closed mould, which is kept at a temperature between the glass transition temperature and the melt transition tempera- ture of the replication material. When the molten replication material contacts the cooled tool surface it solidifies, whereby it is shaped and textured, before the item is released from the mould.
A surprising insight is that the replica surface produced in a fast injection moulding process using the replication tool presented herein exhibits a microscale textured replica surface which is well suited for forming a reliable ultrasonic welding joint also if the vertical profile of the microscale texture on the replica surface is a low fidelity replication of the corresponding profile of the microscale structure on the master surface. Precise and strong ultrasonic welding joints may be reliably obtained as long as the lateral pattern is faithfully transferred and the peak-to-peak amplitude of the vertical profile of the micro-texture on the replica surface is in the microscale, or at least has an amplitude that is sufficient for forming point contacts that are distributed over the respective flange portions. Thereby, a robust low-cost mass- production process for parts is achieved, which are suited for being joined to other parts by ultrasonic welding, and even form a fluid tight seal.
In another particularly advantageous embodiment of the method, the replication process is extrusion coating. Extrusion coating is a process for roll-to-roll processing, i.e. using this embodiment the part may be produced in a continuous process as a layered web with a microscale textured replica surface. To that end, a substrate web may be passed between a nib roll and a cooling roll, in a conventional manner, wherein the rotary surface of the cooling roll is the tool surface defining the general shape of the item. The tool surface has a finish with a microscale structuring gener- ated by treatment with a pulsed laser source. A thermoplastic replication material is heated to above the melting temperature and in the melt phase supplied between the substrate web and the cooling roll, which is kept at a temperature below the melting temperature of the replication material. When the molten replication material contacts the cooled tool surface it solidifies, whereby it is shaped and textured, be- fore the item is released from the replication tool.
Further according to one embodiment of the method for producing a part with microscale energy directors on flange portions thereof, a replication period from contacting the tool surface with the molten replication material to releasing the shaped item is less than 3 minutes, such as less than one minute, such as less than 30 seconds, or even less than 10 seconds. Typically, in an injection moulding process, the replication time may be less than one minute, i.e. a few tens of seconds, such as about 30 seconds. Typically, an extrusion coating process is even faster with replication times of less than 10 seconds.
Further according to one embodiment of the method for producing a part with microscale energy directors on flange portions thereof, the vertical replica profile predominantly has rounded tops with a radius of curvature in the microscale. As described above, the replication process may be controlled to influence the fidelity of replication to provide a vertical replica profile that predominantly has rounded tops with a radius of curvature in the microscale. A low fidelity replication may be achieved in a fast replication process with short replication periods. A process goal/constraint of a faithful replication of the vertical profile of the master structure, on the other hand may entail long settling or curing times incompatible with a fast replication process.
Advantageously, the radius of curvature of the rounded tops is of the same order as the lateral distance between adjacent structures/features of the lateral pattern, such as predominantly above 1 μηι, above 5μηι, or even above 10μηι, and predominantly less than 300 μηη, less than Ι ΟΟμηι or even less than 50μηι. Further advantageously, the vertical amplitude of the replica profile is about equal or less than the lateral distance between adjacent microscale features. In a further aspect, a method for producing a part with microscale energy directors on flange portions thereof comprises preparing a replication tool using the above- mentioned method, and repeatedly performing the method of producing an item with a microscale textured replica surface by a replication process according to any one of the above-mentioned embodiments. Large numbers of items exhibiting enhanced hydrophobicity or super-hydrophobicity may thus be produced cheaply.
According to a further aspect, the invention relates to a part with a microscale textured replica surface produced by replication according to any of the above- mentioned methods.
According to a further aspect, a method of joining a first part and a second part by ultrasonic welding, comprises the steps of producing the first part with microscale energy directors in the form of microscale cone-like protrusions on a flange portion thereof by the method according to any one of the above-mentioned embodiments; producing a second part having a cooperating flange portion; - bringing the microscale cone-like protrusions on the flange portion of the first part in contact with the cooperating flange portion of the second part; and applying ultrasonic energy and pressure, thereby flattening out the cone-like protrusions, to form an ultrasonic welding joint between the first and second parts.
The ultrasonic energy is applied across the flange portions while applying a compression force pressing the two cooperating flanges together. In contrast to energy directors commonly used for forming ultrasonic joints, the invention provides areas of microscale energy directors distributed over flange portions where the work pieces are to be welded together. According to the present invention, a master of the micro-scale energy directors is produced by at least partially covering corresponding flange portions of the work piece negative in a forming tool with a micro-scale roughening, and subsequently replicating the microscale roughening into the flange portions of the work pieces in a forming step. It has turned out that the above described pulsed laser treatment of the tool surface gives an adequate microscale roughening that may be replicated onto the part to form micro-scale energy directors. In particular, by tuning the laser treatment to generate "microscale phase ex- plosions" when applied to tool surfaces, such as forming steel surfaces or aluminium tool surfaces/inserts), a proper scale of the depressions is obtained. By using laser processing of the tool surface a welding joint portion may even be defined on the forming tool in a post processing process, e.g. on an existing forming tool, independent of the process of preparing the forming tool / tool surface. By applying the micro-scale roughening to the tool, the welding joint portion may be produced in the same replicating step as the part itself. The master surface has a microscale structuring with a lateral master patterning and a vertical master profile. Accordingly, the replicated part has a microscale texture with lateral replica patterning and a vertical replica profile.
Further according to some embodiments of the method of joining first and second parts, at least one of the first part and the second part is made of a thermoplastics material. Further according to some embodiments of the method, the first part comprises a flexible web carrying the microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions on at least a flange portion thereof. For example, such embodiments may be useful for assemblies comprising a functional- ized flexible web integrated therein, or for packaging purposes, or when using the flexible web as a cover for a closed container in food packaging, in medical packaging, in analytic devices, or similar applications.
A further aspect of the invention relates to a replication tool for producing a part with a microscale textured replica surface by replication, the replication tool comprising a tool surface defining a general shape of the part, the tool surface comprising at least on portions thereof a microscale structured master surface having a lateral master pattern and a vertical master profile, wherein said microscale structured master surface has been provided by localized pulsed laser treatment adapted to generate microscale phase explosions. Preferably, the vertical master profile has a peak-to- peak amplitude of at least 0.5μηι, and the lateral master pattern has an area density of microscale master features of at least 5000/mm2.
The replication tool for the replication process in question, e.g. a mould for injection moulding or a roller for extrusion coating, has a tool surface defining the general shape of the part to be formed and may be provided in a conventional manner and using conventional tooling materials as known in the art, such as tool steel or 2017 aluminium. The microscale surface structuring is applied as a post treatment of the tool surface by means of a pulsed laser directly scanned over the tool surface. A suitable pulsed laser may be, but is not limited to, an industrial picosecond-laser operating in the near infrared, such as at 1064nm. The exposure of the surface to the pulsed laser radiation is adapted to generate microscale phase explosions. This includes localised melting of tool material on the tool surface, evaporating molten tool material, and ejecting molten and evaporated material in microscale eruptions from the melt surface, thereby forming a densely packed arrangement of microscale crater-shaped depressions. The localized pulsed laser treatment is adapted to produce a micro-porous structure, wherein the micro-porous structure is formed by a densely packed arrangement of crater-shaped microscale depressions with outwardly sloped side walls. The obtained microscale structured master surface has a lateral master pattern and a vertical master profile as described above. Since the post-treatment applied here does not require the precise micro-milling of a specific pre-determined shape of the master structure, such as a regular array of micro- cones, the post-treatment may be applied using cheaper equipment. Furthermore, this post-treatment adapted to generate a microscale porous surface from mi- croscale phase explosions is faster to apply than e.g. micro-milling of microscale features. Furthermore, as also mentioned above, the microscale phase explosions generate microscale crater-shaped depressions with sloped sidewalls that are well suited for fast replication processes, such as injection moulding and extrusion coating. Amongst others, the crater shape with sloped sidewalls facilitates easy releas- ing of the shaped items from the tool surface at the end of the moulding process (de-moulding).
Further according to one embodiment of the replication tool, the tool surface is made of a metal, such as aluminium or steel. The tool surface has to be suited for the fast replication processes for which the method is intended. The tool surface comprising the microscale master structure can be directly produced on a mould surface for contacting the replication material and/or on an inlay attached to the inside of a mould. It is understood that the tool surface may be broken up in sub-surfaces that form part of the mould as is customary in tool design for fast replication processes, such as injection moulding or extrusion coating. Examples of commonly used metals that are also suitable for the present invention include, but are not limited to, aluminium alloys of the types 2017, 1050 or 5754, or tool steel, such as "Sandvik Corona C60", orvar 2343 or similar.
Further according to one embodiment of the replication tool, the microscale structured master surface is a lateral arrangement of polydisperse microscale master features. The term polydisperse refers to microscale features having varying transverse dimensions as seen in a vertical projection. Typically, the polydisperse dimen- sions are characterized by a statistical distribution having a centre value and a spread. The transverse dimensions may be specified as transverse linear dimensions characteristic of the lumen defined by the crater-shaped depression. Given the irregular nature of a polydisperse arrangement, transverse dimensions can also be defined in combination by specifying an area covered by the crater-shaped depres- sion. An equivalent linear dimension characterizing a given crater-shaped depression may then be defined as the diameter of a circle with the same area. The microscale master features on the master surface are preferably densely packed, with neighbouring crater shaped depressions only being separated from each other by a ridge having a width that is comparable to or preferably less than the transverse linear dimension characterizing the crater-shaped depression.
Further according to some embodiments of the replication tool the microscale master features are crater-shaped depressions. Typically the crater-shaped depressions appear more or less circular as seen in a vertical projection. Furthermore, the crater- shape implies an outwardly sloped sidewall providing a positive release angle facilitates de-moulding of the shaped item.
Further according to one embodiment of the replication tool, the vertical profile of the microscale structured master surface has a peak-to-peak amplitude of at least Ο,δμιτι or at least 1 m and below 30μιτι, below 20 m, or preferably below 10μιη.
Further according to one embodiment of the replication tool, the lateral pattern of the microscale structured master surface has an area density of microscale master fea- tures of at least 5000/mm2, at least 8000/mm2, or at least 10000/mm2. Thereby, the replication tool is particularly useful for producing parts comprising a microscale textured surface with a reasonably densely packed lateral distribution of microscale features. When using a part with such a densely packed microscale texture in flange portions for forming ultrasonic joints, high precision, fluid tight ultrasonic joints with improved bond strength are achieved.
It should be noted, however, that the process according to the present invention will not exceed an inherent upper limit for the area density of the microscale lateral structuring. Such an inherent limit is due to the fact that the microscale features produced by the microscale phase explosions according to the present invention require a minimum footprint in order to be resolved. While the present invention produces polydisperse features with a distribution that may include submicron elements, their average (most prominent) lateral dimensions are in the microscale. Increasing the area density of the microscale features results in an increasing proba- bility for the occurrence of overlap between adjacent microscale features. Above a critical overlap, the microscale features are overlapping to such an extent that they appear merged and effectively have a much larger lateral extension than a targeted feature size of individual, unmerged microscale features. As a consequence, above a critical area density such merged features increasingly dominate the actual fea- ture size produced on the replication tool.
In a characterization of the microscale surface structure of the master surface, e.g. by commonly known image analysis techniques applied to micrographs thereof, the merged features are then counted as a single feature with a larger lateral dimension or foot print. This effect is best seen in a graph showing the area density of mi- croscale features, e.g. counted in a given surface portion by means of image analysis, as a function of the laser energy exposure applied to that surface portion. By way of example, such a graph is shown in Fig.19. The data shown has been ob- tained by an analysis of the microscale structuring applied to more than 70 replication tool blanks (tool grade aluminium as specified elsewhere in this application) using the method according to the invention. The ordinate shows the exposure dose expressed in terms of the number of repetitions divided by the scan speed; the coordinate shows the area density of holes detected by an image analysis performed on micrographs of the processed surface; and the marker size indicates the size of the detected feature determined by the same image analysis algorithm. In an initial regime at low exposure, the individual microscale features are resolved and all have essentially the same size. The initial regime covers a low density regime up to about 5000/mm2 where the distribution of the microscale features may be consid- ered as sparse. In an intermediate exposure regime above about 5000/mm2, the microscale features may be considered as more and more densely packed, reaching a critical density of about 12000/mm2, where overlap of adjacent microscale features begins to become significant. The critical density is the maximum achievable density for a given system, which in the example of Fig.19 is about 12000/mm2. Other material systems and laser processing set-ups may have a different maximum achievable area density, such as about 100000/mm2, or about 50000/mm2, or 20000/mm2, or about 15000/mm2. An inherent limit to the maximum achievable area density is given by the requirement of microscale dimensions of the lateral structuring as achieved by the present invention. Increasing the exposure beyond the criti- cal value then only results in merging of the microscale features and in a deterioration of the desired patterning. In the example of Fig.19, a significant decrease of the area density of microscale features to below 5000/mm2, accompanied by a corresponding increase of the average feature size is observed. When the microscale structure of the replication tool master surface is transferred onto a replicated item to form a microscale surface texture for the enhancement of a wetting behaviour, a sparse distribution of microscale features may prove insufficient to provide a significant wetting behaviour enhancement - if any at all. In a preferred exposure regime around the maximum achievable area density of about 100000/mm2, or about 50000/mm2, or 20000/mm2, or about 15000/mm2, or about 12000/mm2, the mi- croscale features are adequately dimensioned in their lateral extend, yet are packed sufficiently dense so as to achieve a significant wetting behaviour enhancement. An adequate range may be determined by an exposure experiment as outlined in Fig.19, wherein preferably the area density is at least 60%, at least 70%, at least 80%, or at least 90% of the maximum achievable area density of microscale features. Above a critical exposure, in the regime where merging becomes more and more dominant, the wetting behaviour enhancement of the replicated item also deteriorates more and more. Further according to one embodiment of the replication tool, the microscale master features have an aspect ratio of a vertical dimension to a lateral dimension of at least 1 :2, or about 1 :1 , wherein the vertical dimension is the peak-to-peak amplitude and the lateral dimension is the square root of the average footprint area per microscale master feature, which for a given microscale structured surface area is cal- culated as the inverse of the area density of microscale master features per area, i.e. the area of the given surface in lateral projection divided by the count of microscale features in that area.
Advantageously according to a further aspect of the invention, the above-mentioned replication tool and methods are adapted such that the lateral arrangement of microscale protrusions in addition to the flange portions includes further portions on the surface of the first part. Thereby the further portions on the surface of the first part may be functionalised by applying a microscale textured replica surface to these further portions in the replication process. The replication tool is adapted by applying the above-mentioned laser treatment to generate microscale phase explosions also to further portions on the tool surface, in addition to flange portions. The parameters of the laser treatment may be kept the same or set differently for different portions of the tool surface to generate different microscale structured master surface portions depending on the purpose of the respective portions of the mi- croscale textured replica surface to be produced therefrom. The purpose for the microscale texturing of the replicated flange portions is to act as energy directors, whereas the purpose of the microscale texturing of the replicated further portions may be another functionalization. In particular, a microscale textured replica surface produced according to any of the herein disclosed methods also exhibits enhanced wetting properties. For example, the microscale textured replica surface may exhibit enhanced hydrophobicity or even superhydrophobicity, provided that the surface material is hydrophobic. Alternatively, a microscale textured replica surface produced according to any of the herein disclosed methods may also exhibit enhanced hydrophilicity, provided that the surface material is hydrophilic.
The term "wetting properties" refers to the interracial interactions in a system comprised of three states of matter, a solid, a liquid, and a gas, and can be quantified by a contact angle. The line connecting all three interfaces, e.g. solid-liquid, solid-gas, liquid-solid, is denoted the three phase-contact line. The contact angle is defined as the angle between the tangents of the liquid-gas and the liquid-solid interphases perpendicular to the three-phase line at any intersection of the two tangents on the three phase line. The wetting properties between a solid and a liquid in a three phase system are considered enhanced with respect to the wetting properties of a flat surface if the apparent macroscopic contact angle is altered by the structure on the surface, wherein the wetting properties of a system with a solid-liquid contact angle smaller than 90° (philic behaviour) is considered enhanced if this contact angle is reduced by the modification (philic enhancement). Likewise, the wetting properties of a system with a solid-liquid contact angle greater than 90° (phobic behav- iour) is considered enhanced if this contact angle is increased by the modification (phobic enhancement).
In some embodiments, the laser treatment of the tool surface may be the same for all portions, since the microscale texturing may simultaneously act as microscale energy directors and provide enhanced wetting properties as compared to a flat unstructured surface of the surface material. Alternatively in some embodiments, the laser treatment of the tool surface may be varied for different portions thereof. For example, the laser treatment of flange portions may be optimised for the purpose of forming energy directors for use in the formation of an ultrasonic joint, whereas the laser treatment of further portions of the tool surface may be optimised for producing enhanced wettability on the further portions of the replicated part.
Advantageously according to some embodiments, the further portions of the microscale textured replica surface on a formed item are adapted to exhibit enhanced hydrophobicity, or even super-hydrophobicity. Further advantageously the replica material is hydrophobic or the microscale textured replica surface is covered with a hydrophobic layer. Alternatively according to some embodiments, the further portions of the microscale textured replica surface on a formed item are adapted to exhibit enhanced hydro- philicity, or even super-hydrophilicity. Further advantageously the replica material is hydrophilic or the microscale textured replica surface is covered with a hydrophilic layer.
The microscale texturing of the replicated first part produced by replication from a microscale structured master surface on a replication tool may thus serve multiple purposes. This may e.g. be useful in providing a packaging having a functionalised surface, such as a superhydrophobic surface, and at the same time allowing for a formation of a precise and reliable ultrasonic joint with a high degree of design freedom. In a further example, such a dual use of the microscale texturing applied to flange portions and further portions may be useful in microfluidics, when forming sealed channels and/or reservoirs that may thus be provided with inner surfaces with an enhanced wettability, such as enhanced hydrophobicity or enhanced hydro- philicity as explained above.
In the context of this application, a material is referred to as hydrophobic, if a flat surface thereof is characterized by a water contact angle of above 90 degrees, such as above 95 degrees, such as about or above 100 degrees. Accordingly, a material is referred to as hydrophilic, if a flat surface thereof is characterized by a water contact angle of below 90 degrees, such as below 85 degrees, such as about or below 80 degrees. For example, a flat surface of the hydrophilic plastics material acryloni- trile butadiene styrene (ABS) may have a water contact angle of about 81 degrees. BRIEF DESCRIPTION OF THE DRAWINGS
Preferred embodiments of the invention will be described in more detail in connection with the appended drawings, which show in FIG. 1 a-c SEM micrographs of a microscale structured master surface at different magnifications,
FIG. 2a-c SEM micrographs of a microscale textured replica surface at different magnifications,
FIG. 3 a SEM micrograph of another microscale structured master surface,
FIG. 4 a SEM micrograph of the microscale textured surface of an injection moulded item (polypropylene) using an isotherm process,
FIG. 5 a SEM micrograph of the microscale textured surface of an injection moulded item (polypropylene) using a variotherm process, FIG. 6 schematically, the surface modification of a tool surface by pulsed laser treatment to generate microscale phase explosions,
FIG. 7 schematically, an injection moulding process according to one embodiment of the invention,
FIG. 8 schematically, an extrusion coating process according to a further embodiment of the invention,
FIG. 9 schematically an ultrasonic welding process according to one embod- iment of the invention,
FIG. 10 schematically an assembly formed using an ultrasonic welding process as shown in Fig.9, FIGS.1 1-14 four graphs plotting hole size and hole density on a microscale structured master surface for different parameter settings of the pulsed laser treatment of the tool surface, and in FIGS.15-18 four graphs plotting hole density on a number of microscale structured master surfaces against the scan speed used during the pulsed laser treatment of the respective tool surfaces; Fig. 19 a graph plotting hole density on a number of microscale structured master surfaces against the exposure in terms of repetitions divided by scan speed used during the pulsed laser treatment of the respective tool surfaces; Figs. 20a-d SEM micrographs of
(a) cone like protrusions in an al2017 mould at a 30° view angle,
(b) cone like protrusions in an al2017 mould at a 0° view angle,
(c) replication of the al2017 mould in cyclic olefin copolymer, and
(d) an orvar2343 steel surface modified using the presented technolo- gy as seen at an 0° view angle;
Schematic drawing of a high aspect ratio chip;
Actual dimensional data obtained by confocal microscopy on the chip of Fig.22, overlaid with the nominal dimensional data as obtained from the corresponding CAD-design;
Figs. 23a-d - (a-d) SEM micrographs of
(a), (c) a laser modified mould on indicated length scales, (b), (d) the corresponding injection moulded piece seen at 30° tilt,
- (e-f) optical micrographs of
(e) unbonded microscale structured energy directors, and
(f) an ultrasonic welding seam using the energy directors,
- (g-h) cross-sectional SEM micrographs of
(g) a chip prior to ultrasonic bonding, and
(h) an ultrasonic weld formed using the present technique. DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS Replication Tool
Examples of suitable materials are materials commonly used as inlays or mould materials in e.g. injection moulding or extrusion coating processes. These materials of the tool surface suited to be modified by pulsed laser treatment to generate mi- croscale phase explosions include Aluminium alloys, such as so-called 1050 aluminium, 5754 aluminium, or 2017 aluminium, as well as tool steel, such as Sandvik corona C60 and orvar 2343.
Figs.1 a-c show micrographs taken by scanning electron microscopy (SEM) of an aluminium tool surface, more particular a tool surface made of 2017 aluminium, which has been modified by pulsed laser treatment using a picosecond laser with a maximum power output of 50 W operating at a pulse frequency of 200 kHz and at a wavelength of 1064 nm. The surface was scanned repetitively at a given power setting in per cent of the maximum power output and with a given speed. The laser beam was incident on the tool surface in a vertical direction, wherein the laser was slightly defocused by shifting the focal point by 1 ,3mm in a vertical direction with respect to the tool surface to be modified. While the apparent spot size was about 50μηη on the surface, a line scan of the laser produced a modified trace width of about 10μηη ± 5μηη. A broader trace as the one shown in Fig.1 a and 1 b was obtained by a meander line scan with adjacent legs of the meander shifted in a direction perpendicular to the scanning direction. Thereby an arbitrary area can be covered by a microscale surface structure. As best seen in Fig. 1 a, the laser treatment results in an ablation of some of the tool surface material. The parameters of the pulsed laser treatment are, however, adjusted such that the bottom of the trace exhibits a lateral arrangement of polydisperse microscale master features, see e.g. Fig.1 b. The microscale master features obtained by this pulsed laser treatment are crater-shaped depressions. The crater-shaped depressions at the bottom of the trace are a consequence of the localized pulsed laser treatment generating microscale phase explosions.
Fig. 3 shows a SEM micrograph of tool surface made of tool steel, more particular Sandvik corona C60 tool steel, which has been modified by pulsed laser treatment using the same picosecond laser with a maximum power output of 50 W operating at a pulse frequency of 200 kHz and at a wavelength of 1064 nm. Again, the surface was scanned repetitively at a given power setting in per cent of the maximum power output and with a given speed. The laser beam was incident on the tool surface in a vertical direction, wherein the laser was slightly defocused. Also here, the localized pulsed laser treatment generates microscale phase explosions resulting in a lateral arrangement of polydisperse microscale master features, wherein the microscale master features are crater-shaped depressions. Replicated Item
Figs. 2a-c show an example of a microscale textured replica surface on a mould insert for injection moulding, as observed in a scanning electron microscope at different magnifications, wherein the width of the image corresponds to 1.2mm in Fig.2a, 0.23mm in Fig.2b, and 0.03mm in Fig.2c. The mould insert for injection moulding was designed and fabricated in 2017 aluminium alloy (Metal Centret, Denmark) by micro milling using conventional techniques to provide a tool surface defining the general shape of the part to be fabricated. To create the microscale structured master surface on the tool surface, a 1064nm, 200kHz, 50W (max power) picosecond laser (FUEGO, Time Bandwidth) mounted in a microSTRUCT vario (3D- Micromac AG) was used to generate microscale phase explosions on the tool surface, thereby producing a densely packed lateral arrangement of microscale crater- shaped depressions. The area intended for structuring was irradiated by the laser in parallel lines separated by 20 μηη. In the example shown in Figs.2a-c, this pattern was repeated 20 times, and the laser power was set to 25% of the max power. Fo- cus was offset by +1 .3 mm above the surface. The microscale structured master surface produced in this example consisted of 10 lines (200 μηη wide) and was 305.5 mm long. The part with the microscale textured replica surface thereon was replicated from this replication tool with the microscale structured master surface on its tool surface using a Victory 80/45 Tech injection moulder (Engel, Schwertberg, Austria). The polymer substrate used for injection moulding was cyclic olefin copolymer (COC) TOPAS grade 5013L-10 (TOPAS Advanced Polymers, Dusseldorf, Germany) with a glass transition temperature (Tg) of 135 C. Injection temperature of the polymer was 270 C and the mould temperature was kept stable at 120 C. The injection moulding was performed in isothermal mode. The resulting microscale sur- face texturing is depicted in Figs.2a-c. The microscale textured replica surface on this first part is adapted to act as microscale energy directors for forming an ultrasonic welding joint with a cooperating second part. Further examples for the microscale textured replica surface on replicated parts are given in Figs.4 and 5. To produce these replica surfaces, the laser structured aluminium insert was installed in a Victory 80/45 Tech injection moulder (Engel). The polymer substrate used for injection moulding polypropylene HD120MO (Borealis) with a Heat Deflection Temperature (0.45 N/mm2) of 88 °C. Injection temperature of the polymer was 255 °C with an injection pressure of 1200 bar. Both variotherm and isotherm injection moulding processes were tested.
Parameters specific for isotherm injection moulding:
• Temperature of microscale structured aluminium insert face = 80 °C. (constant) · Temperature of "backside" mould = 60 °C. (constant)
Parameters specific for variotherm injection moulding:
• Temperature of structured aluminium insert face = 120 °C. (injection)
• Temperature of "backside" mould = 100 °C. (injection)
· Active cooling was applied immediately after polymer injection for the duration of the holding time (60 seconds) followed by and additional cooling time (60 seconds). This resulted in a final mould temperature of 40-50 degrees.
The respective surfaces have been characterised with respect to the shape of the microscale features on the microscale textured surface of the replicated item, see Fig.4 and Fig.5. The isothermal process results in a surface texture with rounded tops, see Fig.4, and the variothermal process results in a surface texture with a hairy appearance ("pulled polypropylene"), see Fig.5. Both surfaces faithfully replicate the lateral pattern of the master, but only provide a low fidelity replication of the vertical profile of the master. Nevertheless, both processes result in a fast replication of parts with microscale energy directors on flange portions thereof. The isothermal process is preferable for high throughput or high volume production, because the isothermal moulding process is not time limited by any process step(s) involving temperature adjustments of mould and/or mould inserts, whereas the variotherm moulding process is partially time limited by one or more process step(s) involving temperature adjustments of mould and/or mould inserts.
Replication Process
Fig.7 shows schematically an injection moulding process for producing a replicated part 4. The process uses a mould having mould parts 1 a and 6, wherein mould part 6 has an insert 1 b. Tool surfaces 2a, 2b, 7 define a general shape of the replicated item 4. Tool surfaces 2a, 2b are provided with microscale structured master surfaces 3a, 3b, 3c, 3d, which are replicated on the item 4 as microscale textures 5a, 5b, 5c, 5d respectively.
Fig. 8 shows schematically an extrusion coating process for coating a substrate web S, with a coating 14. The process uses a roll 1 1 , 1 1 a with a tool surface 12, 12a defining a general shape of the coating. The tool surface comprises microscale structured master surfaces 13, 13a, which are replicated as microscale surface texture 15 on the coating 14. A microscale structured master surface 13 may be applied directly to the tool surface 12 of the roll 1 1 and/or a microscale structured master surface 13a may be applied to the tool surface 12a of a replication tool insert 1 1 a for attachment to the roll 1 1.
Localized Pulsed Laser Treatment Generating Microscale Phase Explosions
Fig.6 shows schematically the configuration of the set-up for localized pulsed laser treatment of a tool surface 2 on a replication tool 1 to generate a microscale structured master surface 3 by scanning a pulsed laser beam 99 over the tool surface.
EXAMPLE
The example illustrates different ways of identifying suitable laser processing parameters for modifying a given tool surface to obtain a microscale structured master surface.
Aluminium 2017 (available from "Metalcenteret" Glostrup, Denmark) was surface structured using a 1064nm, 200kHz, 50W picosecond laser (FUEGO, Time Bandwidth) mounted in a microSTRUCT vario (3D-Micromac AG). To perform the surface structuring, the area intended for structuring was irradiated by the laser in parallel lines separated by 20 μηι. Every second layer was perpendicular to the previous, and so one set of perpendicular planes of lines is referred to as one "cross repetition". The laser power was set to 25% and 10 repetitions was conducted with focus offset +1 .3 mm above the surface.
As illustrated in 1 1-18, the average dimension and standard deviation of the hole sizes may be adjusted by varying parameters such as laser power in percent of maximum power output, scanning speed, number of cross repetitions and z offset of the focus plane. To identify the optimal parameter settings for achieving a desired hole size population and hole density in the alloy in question, one may map the parameter space of the laser settings. When replicated in polymer, the hole size population and hole density will determine the surface structure and roughness and hence the final wetting properties of the polymer piece. In the example below, the parameter space was for the
- Laser power in percent of the maximum power of 50W: from 10 to 100 (both included), in increments of 5;
Scan Speed in mm/s: from 150 to 1950 (both included), in increments of 100; and from 600 to 4200 (both included), in increments of 200;
Number of cross repetitions: from 3 to 39 (both included), in increments of 2;
It may be noted that similar surface characteristics may be achieved using different parameter combinations. However, to minimise time consumption for the laser process, the parameter coordinate with the highest (scan speed / cross repetition) value, and hence lowest process time, is preferred.
A recommended method to reduce the number of parameters and experiments is by locking parameter pairs in a fixed ratio, such as keeping (laser power / scan speed) constant, see Fig.1 1 and Fig.12, where the numerical value of the ratio of (laser power (in percent of the max power of 50W) divided by the scan speed (in mm/s) is kept constant at 25E-5 (= 0,00025) or 50E-5 (= 0,0005) and allows for identification of the desired modification characteristics: both figures show peaks in hole density X. Likewise, the numerical value of the ratio of the number of repetitions divided by the scan speed (in mm/s) can be kept constant, see Fig.13 and Fig.14, where this ratio is kept constant at 1 E-2 (= 0.01 ) or 2E-2 (= 0.02) and allows for identifying de- sired modification characteristics. As can be seen in Fig. 14, the high intensity (slow speed) results in few but large holes, whereas Fig. 13 shows that for the numerical value of the ratio of repetitions over scan speed (in mm/s) equal to 0.01 a more densely packed and uniform hole formation is achieved.
Figs.15-18 show four graphs plotting hole density against the scan speed used during the pulsed laser treatment of the respective tool surfaces. At speeds < 1250 mm/s, the hole density is consistent regardless of other parameters than speed, and it is concluded that writing speed is the main determining factor in this regime. At speeds≥ 1250 mm/s, the hole density varies with the number of cross repetitions. This is true, even when the product (power X repetitions) is kept constant, (see Fig. 16). Marker size represents cross repetitions in Fig.15 and (cross repetitions X power) in Fig.16. Regardless of the parameter settings used to achieve a desired hole density, the coefficient of variance (CV) of hole size is observed to be stable in the regime where (speed≥ 1250 mm/s), see Fig.17, and accordingly for the standard deviation (STD), see Fig.18. Marker size represents hole size CV in Fig.17 and hole size STD in Fig.18. Similarly, the laser focus parameter space may be mapped to identify applicable laser settings. Ultrasonic Welding
Fig. 9 shows schematically a process for forming an ultrasonic welding joint between a first part 40 and a cooperating second part 50. The first part 40 is a replicated part produced using a microscale structured replication tool in a method as described before. The first part 40 has a general shape as defined by the tool surface of the replication tool. The general shape includes flange portions 41 , 42 carrying microscale textured replica surfaces 43, 44 with a lateral arrangement of microscale protrusions, and a recessed portion 45. The second part 50 has cooperating flange portions 51 , 52 facing towards the flange portions 41 , 42 of the first part and are aligned with these flange portions 41 , 42 of the first part. For welding, the first and second parts 40, 50 are brought in contact with each other such that the tops of the microscale protrusions on the first flange portions 41 , 42 form point contacts with the corresponding second flange portions 51 , 52. The parts are clamped in an ultrasonic tool 60, here schematically represented by an ultrasonic horn. The ultrasonic tool 60 is adapted for applying ultrasonic energy while applying a uniaxial pressure in the direction of arrow 61 across the contact interface. The ultrasonic energy is dissipated in the contact region, thereby melting the material with an axial pressure applied across the interface to form a welding joint. Fig. 10 shows schematically the assembly 90 formed by welding the first part 40 and the second part 50 together, thereby forming a cavity 95 defined by the recess portion 45 of the first part 40 and the second part 50. The second part 50 forms a lid, which is sealed fluid tight to the first part 40 by the ultrasonic welding joints 92, 94. The following is an example of a welding joint formed between a polymer part and a sheet of cyclic olefin copolymer (COC).
EXAMPLE
Ultrasonic welding of the polymer part to a 152 μηη thick COC sheet (TOPAS grade 5013S-04, TOPAS Advanced Polymers) was done using a Telsonic-USP4700 ultrasonic welder (Telsonic, Herstad+Piper, Denmark). The chip welding was conducted by depositing 45 J at 90% amplitude, 20 kHz and with a normal force on the piece of 600 N. The normal force could generally be estimated from area (x y cross section) as 10 MN/m2:
area=(305.51 e-3*200e-6)m2 =(6.1 102e-05)m2
6.1 102e-05 m2 * 10 MN/m2 = 61 1 N.
In a similar fashion, the amount of energy required can be estimated from the volume of the energy directors.
EXAMPLE
Referring to Figs.20-23 in the following, a detailed example is given, which shows the high precision and improved strength of fluid tight ultrasonic bonds as achieved by the invention.
The example concerns the use of microscale structured energy directors (ED) for ultrasonic welding of microfluidic systems with a lateral arrangement of microscale features, which in this example are referred to as micropillars. The micropillar EDs are produced by replicating microscale crater-shaped depressions in a mold to obtain cone like protrusion (CLP) structures on the surface of the replicated part. The microscale crater-shaped depressions are introduced on an injection mould surface using a pico-second laser and may therefore be added to any mould surface acces- sible to a pico-second laser beam. The technology is demonstrated on an injection moulded microfluidic device featuring high-aspect ratio (w χ h = 2000 μηη χ 550 μηη), free standing channel walls, where bonding is achieved with no detectable channel deformation. Bonding strength is similar to conventional EDs and the fabricated sys- tern can withstand pressures of over 9.5 bar.
For device fabrication based on replication techniques (e.g. hot embossing and injection moulding), the replication tool has the inverse structure and the ED structures thus have to be realized as depressions in the bottom of the cavity structure used to define the channel wall. ED structures can be realized, e.g., by micro milling, which is a rapid mould tool fabrication process, though the size of the milling tool limits the ED dimensions that can be realized. Milling tools are made as small as 10- 50 μηη, yet it is often not feasible to make EDs on high-aspect ratio wall structures by milling, since the drill aspect ratio is often limited to 1 :3, and the micro mills are short and mounted on large shanks.
In this example, micropillar EDs are used for ultrasonic welding (UW) of microfluidic systems. The EDs are formed by introducing cone-like protrusion structures as a back-end processing of replication moulds using a picosecond laser. The micropillar EDs have the substantial advantage over traditional EDs that they can be defined on any surface accessible to a high energy pico-second laser beam. Moreover, the micropillar EDs can be introduced in designated areas on the tool, and the width of these areas can be chosen independently from the heights of the EDs contrary to traditional EDs, where larger widths are accompanied by higher structures. The CLPs are formed stochastically within the designated area exposed to the laser treatment, so only laser treatment of the general ED layout/shape is required, not an individual laser shaping of each of the individual CLPs. In the example, the technology is demonstrated for an aluminium mould. In addition thereto the CLP formation is verified for tool steel as used for high-throughput industrial moulds. To character- ise the performance of the micropillar EDs, CLP-EDs are compared to micromilled EDs with respect to (1 ) welding strength, (2) structural deformation of a freestanding high-aspect structure, and (3) formation of particles during welding. No significant particle formation was induced by the process in the example. Chip fabrication
Injection moulding was carried out using a custom-made moulding tool comprising a 50 mm diameter disk cavity with 12 luer inlets. The tool could be combined with mould inserts with structures machined in aluminium 2017 (al2017). Prior to injection moulding, two types of ED structures were introduced: (1 ) Traditional EDs introduced by micro milling using a 60° helical engraving tool (#7025, DIXI Polytool, Le Locle, Switzerland). An apex depth of 100 μηη was used (width=1 15 μηη). (2) Micro- structured CLP-EDs written using a FUEGO 1064 nm, 50 W picosecond laser (Time Bandwidth, 3D-Micromac AG, Chemnitz, Germany) mounted in a microSTRUCT vario (3D-Micromac AG). CLPs were introduced by scanning the designated areas with parallel lines (10 μηη spacing), repeated 20 times at 50% power and 1000 mm/s with the focus plane 1 .3 mm above the surface. The writing time was 200 seconds/cm2. To verify that CLPs can be produced in an equivalent manner also in other industrially relevant mould materials, writing of CLPs in high performance tool steel Orvar2343 (MetalCentret, Glostrup, Denmark) was also demonstrated. AI2017 was preferred for mould making in this example, due to its ease of machining. The injection moulding was carried out on a Victory 80/45 Tech hydraulic injection moulding machine (Engel, Schwertberg, Austria) using COC grade 5013L-10 (TOPAS Advanced Polymers GmbH, Frankfurt-Hochst, Germany) with injection and mould temperatures of 270 °C and 120 °C, respectively. Injection pressure was 1766 bar.
Fabricated chips were bonded to a 500 μηη thick foil of COC grade 5013S-04 (TOPAS Advanced Polymers GmbH) by ultrasonic welding. UW was performed at ambient temperature using a Telsonic-USP4700 ultrasonic welder (Telsonic, Erlan- gen, Germany), depositing 25 J with 75% vibrational amplitude, a trigger force of 400 N and 0.5 bar welding pressure. With the fitted 2x booster and sonotrode, the vibrational amplitudes at the sample surface were approximately 44 μηη.
Bonding strength
The bonding strength was assessed using the razor-blade test based on fracture propagation developed by Maszara et al., J. Appl. Phys. 64 (1988) p.4943, and employed by Matteucci et al., Microelectron. Eng. 1 1 1 (2013) p.294, to assess the bonding strength of thermal bonding in similar chips. To perform the test, two mould inserts with a milled 5.15x42.5x0.25 mm3 cavity were fabricated by micro milling. In this cavity, the first insert further featured a 40.5 mm long conventional ED made by conventional milling and the second insert featured a laser micromachined ED with CLPs on an area of 40.5x0.2 mm2. The injection moulded structures were bonded to a COC foil as described above.
CLP and ED structures
Figures 20a and 20b show scanning electron microscopy (SEM) images of the CLPs written in the al2017 mould. It is noteworthy that although the laser scanning is conducted in bundles of parallel lines, the formed CLPs are stochastically formed within the laser ablated area. This may be ascribed to the fact that the microphase explosions causing the CLPs are caused by a combination of metal impurities (alloy) picking up the energy, the pulsing nature of the laser beam and non-uniformity of the laser fluence distribution. The CLPs have a typical height and spacing of 10 μηη and 10 μηη, respectively. On average, the CLP area protrudes 47 μηη from the plane of the tool (Fig. 23g). Note that the CLPs are locally convex depressions in the mould that hence facilitate easy demoulding during replication. Fig. 20c shows a SEM image of a COC replica of the mould. The replicated structures are observed to have rounded tops due to imperfect filling during replication. We found that operating at conditions yielding higher fidelity replication resulted in more difficult demoulding due to stronger adhesion between the mould and its replica. This rounding did not affect the performance of the EDs. Fig. 20d shows tool steel Orvar2343 ablated to produce CLPs similar to those demonstrated in al2017.
Figures 23a and 23b show SEM images of the CLP-EDs in the al2017 mould for fabrication of the high-aspect ratio microfluidic system. The images clearly show the feasibility of writing CLP-ED structures at the bottom of the trenches in the mould. Note that the separation and joining of bundles of laser lines do not alter the pattern and formation of CLPs. Thus, CLP-EDs can be formed in any pattern or geometry. Corresponding SEM images of the injection moulded COC replica (Figs. 23c,d) clearly show that micropillar structures are well reproduced on the top of the high- aspect ratio wall. Figures 23e and 23f show optical micrographs of the same structures pre and post UW. Due to the structure of the CLPs, the final micropillar CLP-EDs of the polymer chip are opaque (Fig. 23e). However, like conventional butt joint EDs, the joints are transparent post welding (Fig. 23f). It is noteworthy that no signs of trapped or com- pressed air are observed in structures surrounded by CLP-EDs, such as the pocket in the corner of the structure (Fig. 23e) where little or no gap is observed post UW in Fig. 23f. This indicates that the micropillar structure facilitates the escape of air during UW. SEM images Figs.23g and 23h highlight the position of CLP-ED polymer pre and post welding. Note the solidified polymer from the welding process in Fig.23h without any significant formation of "bonding flashes". This shows the high precision achieved with the bonding method of the invention.
Bonding strength
Bonding strengths in terms of the surface energy, γ (gamma), calculated from razor- blade tests are listed in Table 1 .
Table 1
Bonding method Material γ [Mm2]
UW, conventional EDs COC Topas 5013L-10 100+30
UW, CLP-EDs COC Topas 5013L-10 122±23
From the results given in Table 1 it appears that the bonding strength for thermo- plastics is largest for structures bonded using ultrasonic welding. No significant difference is observed between conventional EDs and micropillar EDs.
High-aspect ratio microfluidic system
The performance of CLP-ED structures were tested in the described high-aspect ratio microfluidic system. Fig.21 shows a schematic drawing of the high aspect ratio chip with an outer channel 101 , and an inner channel 102 separated by walls 103. Cross sections (l-l, ll-ll, Ill-Ill) for confocal imaging are indicated. A bundle of 20 laser patterning lines 104 were added on the walls 103. Note that the 20 lines 104 are separated into two bundles of 10 lines each (104a, 104b) at the corners, to keep a constant edge distance of 180μηι. First, it was verified that the microfluidic channels were leak-tight when filled with an aqueous solution containing fruit dye. Further, pressure testing with gas applied to the outer channel while leaving the inner channel at ambient pressure showed that the devices (three tested) could sustain pressure up to at least 9.5 bar (maximum pressure available in the test).
Fig.22 shows confocal imaging data (thick lines) of the free-standing wall structures of the device along the cross sections 1-3 (cf. Fig. 21 ). The data of the three sections taken along the length of the parallel channel section (l-l, ll-ll, Ill-Ill) are over- laid on each other and fully coincide. The confocal imaging data are further overlaid with the corresponding CAD file used for the mould fabrication. From the confocal images, it is derived that the channel height of the welded structure matches that of the design (2000 μηη) with a tolerance of ±4.2 μηη. This value is smaller than the confocal image voxel height and we conclude that any height difference is below our detection limit. This data further supports the particularly high precision of the bonding method according to the present invention.
In conclusion, the present example shows ultrasonic welding of microfluidic systems based on micropillar EDs according to one embodiment of the invention. The mi- cropillar EDs are produced by replication of CLPs in aluminium, formed using a picosecond laser, and can be added to any mould surface accessible to a high power pico-second laser. The example demonstrated the technology by injection moulding microfluidic devices featuring high-aspect ratio structures and shown that ultrasonic welding of the devices is possible with no detectable channel deformation. The per- formance of the CLP-EDs was characterised showing that bonding strength is similar to conventional EDs, with no particle formation. The bonded devices could withstand 9.5 bar of hydraulic pressure without fracturing. The laser processing method has further been demonstrated to work in high endurance tool steel used for making high performance injection moulding tools. Furthermore, the method of the invention supports a modification rate of 200 seconds/cm2 and post processing capabilities on full three-dimensional mould surface shapes, as long as these are optically accessible.

Claims

1. Method of producing a first part having a flange portion for use in the formation of an ultrasonic welding joint with a cooperating second part, the method comprising the steps of
providing a forming tool having a tool surface adapted to define a general shape of a part to be formed;
modifying at least portions of the tool surface by a pulsed laser treatment to obtain a replication tool with a microscale structured master surface with a lateral master pattern and a vertical master profile; wherein the pulsed laser treatment is adapted to generate microscale phase explosions on the tool surface, thereby forming the microscale structured master surface as a lateral arrangement of microscale crater-shaped depressions; and
using the replication tool to form the first part by the replication process, wherein the formed first part has the general shape defined by the tool surface, and wherein the formed first part comprises a microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions produced by the microscale structured master surface on at least the flange portion of the first part, wherein the lateral pattern of the microscale textured replica surface has an area density of microscale cone-like protrusions of at least 5000/mm2.
Method according to claim 1 , wherein the replication process is one of injection moulding, hot embossing, compression moulding, and extrusion coating.
Method according to claim 1 or claim 2, wherein the microscale textured replica surface has a peak-to-peak amplitude of at least 0.5μηι, or at least 1 μηη and up to 5μηι, or up to Ι Ομηη, or even up to 30μηι. 4. Method according to any of the preceding claims, wherein the lateral pattern of the microscale textured replica surface has an area density of microscale conelike protrusions of at least 8000/mm2, or at least 10000/mm2.
5. Method of joining a first part and a second part by ultrasonic welding, the method comprising the steps of producing the first part with microscale energy directors on a flange portion thereof by the method according to any one of claims 1-4; producing a second part having a cooperating flange portion; bringing the microscale cone-like protrusions on the flange portion of the first part in contact with the cooperating flange portion of the second part; and applying ultrasonic energy and pressure, thereby flattening out the cone-like protrusions, to form an ultrasonic welding joint between the first and second parts.
Method according to claim 5, wherein at least one of the first part and the second part is made of a thermoplastics material.
Method according to claim 5 or claim 6, wherein the first part comprises a flexible web carrying the microscale textured replica surface with a lateral arrangement of microscale cone-like protrusions on at least a flange portion thereof.
8. Replication tool for producing a part with a microscale textured replica surface by replication, the replication tool comprising a tool surface defining a general shape of the part, the tool surface comprising a microscale structured master surface having a lateral master pattern and a vertical master profile, wherein said microscale structured master surface has been provided by localized pulsed laser treatment adapted to generate microscale phase explosions, wherein the vertical master profile has a peak-to-peak amplitude of at least 0,5μηι, and wherein the lateral master pattern has an area density of microscale master features of at least 5000/mm2.
9. Replication tool according to claim 8, wherein the tool surface is made of a metal, such as alloys of aluminium or steel.
10. Replication tool according to claim 8 or claim 9, wherein the microscale structured master surface is a lateral arrangement of polydisperse microscale master features.
1 1. Replication tool according to any one of claims 8-10, wherein the microscale master features are crater-shaped depressions.
12. Replication tool according to any one of claims 8-1 1 , wherein the vertical master profile has a peak-to-peak amplitude of at least Ο.δμηη, preferably at least 1 μηη, or at least 2μηη.
13. Replication tool according to any one of claims 8-12, wherein the vertical master profile has a peak-to-peak amplitude below 30μηι, below 20μηι, or preferably below 10μηη.
4. Replication tool according to any one of claims 8-13, wherein the lateral master pattern has an area density of microscale master features of at least 8000/mm2, or at least 10000/mm2.
5. Replication tool according to any one of claims 8-14, wherein the microscale master features have an aspect ratio of a vertical dimension to a lateral dimension of at least 1 :2, or about 1 :1 , wherein the vertical dimension is the peak-to- peak amplitude and the lateral dimension is the square root of the average footprint area per microscale master feature.
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