CN107639844A - The manufacture method and relevant apparatus features of the part of appliance of motor vehicles - Google Patents

The manufacture method and relevant apparatus features of the part of appliance of motor vehicles Download PDF

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Publication number
CN107639844A
CN107639844A CN201710590822.3A CN201710590822A CN107639844A CN 107639844 A CN107639844 A CN 107639844A CN 201710590822 A CN201710590822 A CN 201710590822A CN 107639844 A CN107639844 A CN 107639844A
Authority
CN
China
Prior art keywords
top layer
cylinder
retaining element
composite panel
face
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN201710590822.3A
Other languages
Chinese (zh)
Inventor
史蒂夫·热内斯
瓦莱丽·马塞尔
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Adler Pelzer France Grand Est SAS
Original Assignee
Faurecia Automotive Industrie SAS
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 Faurecia Automotive Industrie SAS filed Critical Faurecia Automotive Industrie SAS
Publication of CN107639844A publication Critical patent/CN107639844A/en
Pending legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
    • B29C65/0672—Spin welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
    • B29C65/069—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding the welding tool cooperating with specially formed features of at least one of the parts to be joined, e.g. cooperating with holes or ribs of at least one of the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/60—Riveting or staking
    • B29C65/601—Riveting or staking using extra riveting elements, i.e. the rivets being non-integral with the parts to be joined
    • B29C65/603—Riveting or staking using extra riveting elements, i.e. the rivets being non-integral with the parts to be joined the rivets being pushed in blind holes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint 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
    • B29C66/112—Single lapped joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
    • B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined
    • B29C66/30325—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined
    • B29C66/30326—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined in the form of porosity
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General 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
    • B29C66/51—Joining 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
    • B29C66/53—Joining single elements to tubular articles, hollow articles or bars
    • B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/72—General 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 structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/72—General 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 structure of the material of the parts to be joined
    • B29C66/725—General 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 structure of the material of the parts to be joined being hollow-walled or honeycombs
    • B29C66/7252—General 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 structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled
    • B29C66/72525—General 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 structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled comprising honeycomb cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/73—General 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
    • B29C66/739—General 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
    • B29C66/7392—General 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832—Reciprocating joining or pressing tools
    • B29C66/8322—Joining or pressing tools reciprocating along one axis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/64—Joining a non-plastics element to a plastics element, e.g. by force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/71—General 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 composition of the plastics material of the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/72—General 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 structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/73—General 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
    • B29C66/731—General 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
    • B29C66/7311—Thermal properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/73—General 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
    • B29C66/731—General 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
    • B29C66/7311—Thermal properties
    • B29C66/73115—Melting point
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/73—General 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
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    • B29C66/7392—General 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
    • B29C66/73921—General 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/73—General 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
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/74—Joining plastics material to non-plastics material
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/90—Measuring or controlling the joining process
    • B29C66/93—Measuring or controlling the joining process by measuring or controlling the speed
    • B29C66/939—Measuring or controlling the joining process by measuring or controlling the speed characterised by specific speed values or ranges
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING 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
    • B29K2711/00—Use of natural products or their composites, not provided for in groups B29K2601/00 - B29K2709/00, for preformed parts, e.g. for inserts
    • B29K2711/12—Paper, e.g. cardboard
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/08—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of welds or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)

Abstract

The present invention relates to a kind of manufacture method of the part of appliance of motor vehicles, this method includes providing the composite panel (12) for including the first top layer (22) and the second top layer (24) and distance piece (26), and provides the retaining element (16) for including the cylinder (44) made of thermoplastic (45)；Retaining element is rotated while the cylinder of retaining element is inserted in the composite panel in the first top layer (22) side.Second top layer (24) is included in the hole of the first face (32) upper shed, and first face is fixed on distance piece (26).Continue cylinder insertion until the first end (46) of cylinder contacts with the first face, the friction with second top layer promotes thermoplastic (45) to melt, and the plastic material is pierced into hole；Thermoplastic (45) recovers solid-state after the cooling period, while be connected and fixed element and the second top layer.

Description

The manufacture method and relevant apparatus features of the part of appliance of motor vehicles
Technical field
The present invention relates to a kind of manufacture method of the part of appliance of motor vehicles, the method for the type comprises the following steps：
- composite panel is provided, the composite panel includes：First top layer and the second top layer, in first and second top layer Each include reinforcing fiber, connected between these reinforcing fibers by polymeric substrate；And distance piece, the distance piece bag Include two relative faces, each in the first top layer and the second top layer is fixed on one in the face；
Composite panel has the inserting thickness formed by the first top layer and distance piece；
- retaining element is provided, the retaining element includes the cylinder made of thermoplastic；Then
- rotation retaining element in the first top layer side by the cylinder of the retaining element while insert the composite surface In plate.
Background technology
The method of the above-mentioned type is especially known from document US2014/0140779.The method of this friction welding type allows Thermoplastic insert and the composite panel of " interlayer " type are assembled, the composite panel includes two be fixed on distance piece Individual top layer.Rotation softens the thermoplastic of cylinder by rubbing at a high speed, and then cylinder is fixed on distance piece by deformation.
The insert being connected on panel is used for example as supporting the auxiliary member such as retainer ring of rotary shaft, handle or band The supporting member of part.The part of appliance so formed is, for example, the back shroud, loading base or lateral fitting type of luggage case.
The composite panel that distance piece has " interlayer " type of relatively low surface density is advantageously used in into due to lighter in weight Type part of appliance.However, method as described above is not suitable for this composite panel.In fact, the density of distance piece is not enough to Retaining element is allowed to realize effective fastening.Even if the retaining element therefore with the presence of the tractive force more relaxed and The risk pulled out from panel.
From not yet disclosed document FR1560822, it is known that before distance piece is connected into insert, pass through polymer tree Fat local strengthening distance piece.However, this method implements the production cost of complicated and significant increase part of appliance.
The content of the invention
The present invention is directed to propose a kind of, no matter the surface density of distance piece is how many, it is allowed to by thermoplastic element and " interlayer " class The method for simplifying that the composite panel of type is assembled.
Therefore, the present invention relates to a kind of method of the above-mentioned type, wherein：
Height of the cylinder of-retaining element between the first and second ends is more than the inserting thickness of composite panel；
- the second top layer is included in the hole of the first face upper shed, and first face is fixed on distance piece；
- continue to insert cylinder in composite panel until the first end of the cylinder and first face on the second top layer connect Touch, therefore, the thermoplastic for promoting the first end of cylinder with second friction subsurface melts；Then
The thermoplastic of-the fusing is pierced into the hole in first face；
- stop the rotation retaining element；Then
The thermoplastic of-cylinder recovers solid-state after the cooling period, while the second table of be connected and fixed element and composite panel Layer.
According to other favourable aspects of the present invention, this method can include one or more of following characteristics, and these are special Sign can use individually or according to all possible technical combinations：
The distance piece of-composite panel includes honeycomb, and the distance piece is preferably by the undulation degree of Paper or cardboard type Material is formed；
The porosity on the-the second top layer is more than or equal to 10%；
The polymeric substrate on the-the second top layer is by the similar or identical thermoplasticity of the thermoplastic of the cylinder with retaining element Material is formed；
- during cylinder is inserted into composite panel, the rotary speed of retaining element is more than or equal to 2500 revs/min；
The reinforcing fiber on the-the second top layer is cellulose fibre；
The fusion temperature of the thermoplastic of the cylinder of-retaining element is less than or equal to 200 DEG C；
- retaining element includes the head coupled with the second end of cylinder, and the maximum transverse size on head is more than the cylinder The maximum transverse size of body；
The step of-this method also includes providing to be assembled to auxiliary element on composite panel, the auxiliary element includes Hole is assembled, will be realized in the cylinder insertion composite panel of retaining element through the assembling hole, so as to described Auxiliary element described in lock ring between first face of composite panel and the head of retaining element.
The invention further relates to a kind of part of appliance of motor vehicles, the part of appliance can obtain from above-mentioned manufacture method Arrive.
Brief description of the drawings
, will preferably by reading the description hereafter only carried out as nonrestrictive example and provide and refer to the attached drawing Understand the present invention, in the accompanying drawings：
Fig. 1 is the schematic sectional view of the part of appliance of motor vehicles according to an embodiment of the invention；
Fig. 2 is the sectional view of the manufacture element of Fig. 1 part of appliance；
Fig. 3 is the sectional view of the manufacture element of modified embodiment according to the invention；And
Fig. 4 is the schematic diagram of the manufacturing step of Fig. 1 part of appliance.
Embodiment
Fig. 1 shows the part of appliance 10 of motor vehicles.Part 10 is structure member, e.g. covers the bonnet of luggage case The false bottom or assistant engine of plate, driving cabin or luggage case.
Part of appliance 10 includes composite panel 12, the auxiliary element 14 for being assembled into the panel and the connection composite surface The retaining element 16 of plate 12 and the auxiliary element 14.
Composite panel 12 is the structure of " interlayer " type, and it includes relative the first face 18 and the second face 20.
More properly, composite panel 12 includes the first top layer 22 and the second top layer 24, first top layer and the second top layer point Not Xing Cheng composite panel 12 the first face 18 and the second face 20.Composite panel 12 also includes distance piece 26, and the distance piece is plugged in Between two top layers 22,24.More specifically, the first top layer 22 and the second top layer 24 are fixed on the opposite face of distance piece 26.
Distance piece 26 is based preferably on honeycomb or alveolar structure is made.Therefore, distance piece 26, which has, is substantially perpendicular to face Multiple walls 27 in the face 18,20 of plate 12.Wall 27 defines the central space for the closed outline to form honeycomb.Honeycomb for example defines more Side shape grid, especially hexagonal mesh.
Distance piece 26 is advantageously made up of the light material of such as Paper or cardboard.The surface density of distance piece 26 is preferably less than 1500g/m2, and basically between 400g/m2And 1200g/m2Between.
The surface density on the first top layer 22 and the second top layer 24 is more than the surface density of distance piece 26, and the first top layer 22 and the The thickness on two top layers 24 is preferably less than the thickness of distance piece 26.Each in the top layer 22,24 includes reinforcing fiber 28, connected by polymeric substrate 30 between these reinforcing fibers.Reinforcing fiber 28 is selected from carbon fiber, such as glass fibre Ceramic fibre, also or such as flax fiber, hemp, the cellulose fiber of the natural origin of kenaf or tossa Among dimension.
According to first embodiment, polymeric substrate is thermoplastic matrix, and it is especially included selected from polyamide (PA), polyethylene (PE), one or more materials among polypropylene (PP) and such as poly- (PETP) (PET) polyester.
According to second embodiment, polymeric substrate is thermosetting base material, and it especially includes one or more unsaturated polyester (UP)s.
In the embodiment in figure 1, it is believed that the first top layer 22 and the second top layer 24 are essentially identical.According to modified example, One top layer and the second top layer are different, and the two top layers especially include different reinforcing fiber 28 and/or polymeric substrate 30.
Especially, the second top layer 24 includes the first face 32, and it is contacted with distance piece 26, and the second face 20, and it corresponds to Second face of composite panel 12.Second top layer 24 has significant porosity, especially at first face 32 on the second top layer.Second The hole on top layer 24 is especially in the upper shed of the first face 32.
Especially, the porosity on the second top layer 24 is preferably larger or equal than 10%, more preferably equal to or greater than 15%, especially It is near retaining element 16, and porosity is defined as the ratio between the volume of hole and the cumulative volume on the second top layer 24.
The porosity on the second top layer 24 is adjusted especially by its manufacturing process.According to first embodiment, the second top layer 24 are formed by hot compression substrate, and the substrate includes being mixed into the reinforcing fiber of thermoplastic polymer fibers.With applicant Name the manufacture method of corresponding composite panel 12 is described in EP2822746.As an example, obtained according to this method The porosity on the second top layer 24 is about 30% to 45%.
According to second embodiment, the second top layer 24 is to fold parallel fiber grenadine by hot compression one to be formed, and these are flat Connected between capable fiber grenadine by thermosetting resin.Described with the name of applicant in WO2015055847 corresponding multiple Close the manufacture method of panel 12.As an example, the porosity on the second top layer 24 obtained according to this method is about 20%.
According to 3rd embodiment, the second top layer 24 is formed by the matte of hot compression reinforcing fiber, and the matte is stacked in On thermoplastic polymer layer.The manufacturer of corresponding composite panel 12 is described in document FR3014731 with the name of applicant Method.As an example, the porosity on the second top layer 24 obtained according to this method is about 15%.
Composite panel 12 has inserting thickness 34, and the thickness is thought of as on the first face 18 of the panel and the second top layer 24 The first face 32 between thickness.
The auxiliary element 14 for being assembled into panel 12 is, for example, the fixing metal parts of the annex for such as handle or band. Auxiliary element especially includes the sheet material 36 contacted with the first face 18 of panel 12.Sheet material 36 is passed through by assembling hole 38.
Retaining element 16 is set along axis 40.In part of appliance 10, first face 18 He of the axis 40 perpendicular to panel 12 Second face 20.
Fig. 2 is shown before former part 10, corresponding to the retaining element 16A of Fig. 1 retaining element 16.
Retaining element 16,16A has the shape substantially rotated around axis 40.More properly, retaining element 16,16A Head 42 and cylinder 44,44A including shape substantially in disk form.The first end of the cylinder couples with head 42.
Cylinder 44,44A are formed by thermoplastic 45, be selected from polyamide, polypropylene or such as PET polyester it In.Preferably, head 42 is formed by the part with cylinder 44,44A.
In Fig. 1 and Fig. 2 embodiment, cylinder 44,44A has the shape of basic truncated cone-shaped, and the round platform is from the court of head 42 It is tapered to the second end 46,46A of the cylinder.It is less than auxiliary member close to the cylinder 44,44A on head 42 maximum gauge The diameter of the assembling hole 38 of part 14, again smaller than the diameter on head 42.
In Fig. 1 part of appliance 10, cylinder 44 is inserted in the assembling hole 38 of composite panel 12 and auxiliary element 14, with Just sheet material 36 is maintained between head 42 and the first face 18 of the panel 12.
Fig. 3 shows the retaining element 116A corresponding to retaining element 16A modified example.Retaining element 116A is included as before Described cylinder 44A.The first end of the cylinder is formed by the flat surfaces 142 perpendicular to axis 40.Retaining element 116A It is intended to by being assembled with the phase of composite panel 12 to form part of appliance, the first face 18 of flat surfaces 142 and the panel 12 is flat Together.
Preferably, retaining element 16,16A, 116A include the recess 48 set along axis 40.Recess 48 forms blind hole, The blind hole is in head 42 or the upper shed of flat surfaces 142.As described below, recess 48 is used for retaining element 16A, 116A and equipment The installation tool of part 10 mutually assembles.Especially, recess 48 includes preventing the surface 50 rotated relative to the instrument.The table Cylinder that is that face 50 is, for example, plane and forming hexagon.
Cylinder 44A has the height 52 along axis 40 between the second end 46A and head 42 or flat surfaces 142. Highly 52 are more than the inserting thickness 34 of the related compound panel 12 for former part 10.In the example of fig. 1, fixed member The height 52 of part 16A cylinder is more than the inserting thickness 34 that increase has the thickness of sheet material 36.
As an example, the height 52 of retaining element 16A cylinder is about 2 to 4cm；The height 52 has sheet material 36 with increase Difference between the inserting thickness 34 of thickness is about 1 to 2mm.
In Fig. 1 part of appliance 10, the second end 46 of cylinder 44 is assembled on first face 32 on the second top layer 24. More properly, the partial penetration of thermoplastic 45 of end 46 is into the hole on the second top layer 24, to couple composite panel 12 With retaining element 16.
The manufacture method of Fig. 1 part of appliance 10 will now be described.This method, which especially realizes, rubs retaining element 16 Weld on composite panel 12.
This method is especially implemented with installation tool 60, and the installation tool is partly shown in Fig. 4.This instrument 60 wraps Installation nose 62 is included, the nose can cooperate with retaining element 16,16A recess 48.The peace of this installation tool and correlation Dress method has especially been described in document US 2014/0140779.
First, retaining element 16A is assembled into installation nose 62.The assembly hole of the component being consequently formed and auxiliary element 14 Hole 38 and the first face 18 of panel 12 are oppositely arranged.The axis 40 of retaining element is set perpendicular to first face 18.
Installation nose 62 and then driving retaining element 16A are rotated at a high speed.The speed is preferably larger or equal than 2500 Rev/min, and more preferably between 3000 and 6000 revs/min.
Meanwhile retaining element 16A moves up in the side of panel 12.As shown in figure 4, cylinder 44A the second end 46A connects The first top layer 22 is touched, the top layer is then passed through due to friction and the axial movement of the cylinder.
During the step, the friction with first top layer 22 improves the thermoplastic of the second end 46A 45 temperature.The material is close to its fusing point and may start that clayey texture is presented.
Through after the first top layer 22, cylinder 44A still rotate at high speed passes through distance piece 26.Due to described in formation The lightweight of the material of distance piece, the step hardly generate heat.
Cylinder 44A the second end 46A contacts with first face 32 on the second top layer 24.Friction with first face is by The guiding of thermoplastic 45 of heated cylinder reaches liquid or clayey texture.
Preferably, rotary barrel 44A is continued during the extremely short duration after being contacted with the second top layer 24.Should Duration is about 2 seconds.Abreast, because retaining element 16A axial movement, head 42 contact with sheet material 36, while against Panel 12 fastens auxiliary element 14.
Then, stopped the rotation installation nose 62, and the installation nose is taken out from recess 48.Liquefied thermoplasticity material Material 45 is penetrated into the hole on the second top layer 24 near first face 32 on the second top layer.After cooling, the second end of cylinder 44 Therefore 46 couple with second top layer 24, while ensure the assembling of retaining element 16 and panel 12.Therefore the equipment for obtaining Fig. 1 Part 10.
As shown in figure 1, the second end 46 of cylinder 44 may include the basic ball bubble portion 64 in parabolic shape, ball bubble Portion is arranged on the inside of distance piece 26.Centrifugal action on fluent material of the ball bubble portion by acting on cylinder 44A and Formed.
According to the method similar to the above method, by assemble the retaining element 116A of above-mentioned composite panel 12 and Fig. 3 come Form part of appliance.When the first face 18 of flat surfaces 142 and panel 12 is concordant, stop the rotation installation nose 62.Such group The retaining element being attached on panel especially has the function of the fixation of fastening auxiliary element.It is used for and spiral shell for example, recess 48 has Follow closely the threaded portion of assembling.
Preferably, the polymeric substrate 30 on the second top layer 24 by with retaining element 16,16A, 116A cylinder 44,44A's The similar or identical thermoplastic of thermoplastic 45 is formed.This thermoplastic is, for example, polyamide, polypropylene or poly- Ester.Therefore, cylinder 44,44A fluent material therefore with the more preferable affinity of the base material, be advantageous to the fluent material Penetrate into the hole on the second top layer 24.
According to preferred embodiment, the reinforcing fiber 28 on the second top layer 24 is the cellulose fibre of natural origin, such as flax Fiber.This cellulose fibre generally has about 200 DEG C of degradation temperature.Between retaining element 16A, 116A and the second top layer 24 The shorter friction duration allow to prevent fiber from reaching such temperature near contact area.However, cellulose fibre 28 are preferably connected on the retaining element 16 formed by material 45, and the fusion temperature of this material is less than or equal to 200 DEG C.This Kind material is, for example, polyamide 11.
The rotary speed of installation nose 62 carrys out selection especially in accordance with the property of cylinder 44,44A material 45.The speed Degree is preferably chosen to the sufficiently high friction duration to limit with the second top layer 24, particularly when the second top layer includes fiber During cellulose fiber.In addition, the speed is preferably chosen to the sufficiently small ball bubble portion 64 formed with limitation by the effect of centrifugal force Size.

Claims (10)

1. a kind of manufacture method of the part of appliance of motor vehicles (10), it comprises the following steps：
- composite panel (12) is provided, the composite panel includes：First top layer (22) and the second top layer (24), first top layer Include reinforcing fiber (28) with each in the second top layer, connected between these reinforcing fibers by polymeric substrate (30)； And distance piece (26), the distance piece include two relative faces, each in first top layer and second top layer Fixed on one in the face；
The composite panel has the inserting thickness (34) formed by first top layer (22) and the distance piece (26)；
- retaining element (16A, 116A) is provided, the retaining element includes the cylinder (44A) made of thermoplastic (45)；So Afterwards
- rotation the retaining element from the first top layer (22) side by the cylinder of the retaining element while insert institute State in composite panel；
Methods described is characterised by：
Height (52) of the cylinder of-retaining element between first end (46A) and the second end (42,142) is more than institute State the inserting thickness (34) of composite panel；
- second top layer (24) is included in the hole of the opening on the first face (32), and first face is fixed on the distance piece (26) on；
- continue to insert the cylinder into first end (46A) and second table in the composite panel until the cylinder The first face (32) contact of layer, the friction with second top layer promote the thermoplastic of the first end of the cylinder (45) melt；Then
The thermoplastic of-the fusing is pierced into the hole in first face；
- stop the rotation the retaining element；Then
The thermoplastic (45) of-cylinder recovers solid-state after the cooling period, while couples the retaining element and described compound Second top layer of panel.
2. according to the method for claim 1, wherein, the distance piece (26) of the composite panel includes honeycomb, described Distance piece is preferably formed by the fibrous material of Paper or cardboard type.
3. method according to claim 1 or 2, wherein, the porosity of second top layer (24) is more than or equal to 10%.
4. according to any method of the preceding claims, wherein, the polymeric substrate (30) on second top layer by Similar or identical thermoplastic is formed with the thermoplastic (45) of the cylinder of the retaining element.
5. according to any method of the preceding claims, wherein, the cylinder is being inserted into the composite panel phase Between, the rotary speed of the retaining element is more than or equal to 2500 revs/min.
6. according to any method of the preceding claims, wherein, the reinforcing fiber (28) on second top layer is fine Cellulose fiber.
7. the method according to claim 11, wherein, the fusing temperature of the thermoplastic (45) of the cylinder of the retaining element Degree is less than or equal to 200 DEG C.
8. according to any method of the preceding claims, wherein, the retaining element includes the with the cylinder The head (42) of two ends connection, the maximum transverse size on the head are more than the maximum transverse size of the cylinder.
9. according to the method for claim 8, it also includes providing to be assembled to the auxiliary element on the composite panel (14) the step of, the auxiliary element include assembling hole (38),
The cylinder of the retaining element is inserted in the composite panel and realized through the assembling hole, so as in institute State auxiliary element described in lock ring between the first face (18) of composite panel and the head (42) of the retaining element.
10. a kind of part of appliance of motor vehicles (10), it can be from manufacture according to any one of the preceding claims Method obtains.
CN201710590822.3A 2016-07-20 2017-07-19 The manufacture method and relevant apparatus features of the part of appliance of motor vehicles Pending CN107639844A (en)

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FR1656896A FR3054273B1 (en) 2016-07-20 2016-07-20 METHOD FOR MANUFACTURING A MOTOR VEHICLE EQUIPMENT PIECE AND PART OF EQUIPMENT THEREFOR
FR1656896 2016-07-20

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110439891A (en) * 2018-05-02 2019-11-12 大众汽车有限公司 By dismountable connection for economical space saving fixing component of latch elements
CN111038681A (en) * 2018-10-12 2020-04-21 空中客车营运有限公司 Aircraft assembly
CN112513475A (en) * 2018-07-18 2021-03-16 伊卓特有限两合公司 Connecting element and method for introducing a connecting element

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2569971A (en) * 2018-01-04 2019-07-10 Titus D O O Dekani Improvements in fasteners

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2421556A (en) * 2004-12-27 2006-06-28 Blum Gmbh Julius Method of anchoring a plug element in a building board
US20070062628A1 (en) * 1999-06-18 2007-03-22 Woodwelding Ag Integral joining
CN102256766A (en) * 2008-12-23 2011-11-23 伍德韦尔丁公司 Method of anchoring a connector, and connector
CN104159720A (en) * 2012-03-09 2014-11-19 佛吉亚汽车工业公司 Method of manufacturing a piece of automotive vehicle equipment and associated piece of equipment
DE102013213771A1 (en) * 2013-07-15 2015-01-15 Johann Bartlechner Kg Process for the production of concrete parts with plastic lining and device for carrying out the process
CN104411482A (en) * 2012-05-24 2015-03-11 佛吉亚汽车工业公司 Method for producing a piece of reinforced equipment, in particular for a motor vehicle

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4141616B4 (en) * 1991-12-17 2005-12-29 Steeg, Heinz Bernd, Dr.-Ing. Method for fastening a holding part to a component by friction welding
DE202012011021U1 (en) * 2012-11-16 2014-02-17 Ejot Gmbh & Co. Kg Setzwerkzeugsytem
DE102014105702A1 (en) * 2014-04-23 2015-10-29 Weber Schraubautomaten Gmbh Device for setting a setting element in a component

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070062628A1 (en) * 1999-06-18 2007-03-22 Woodwelding Ag Integral joining
GB2421556A (en) * 2004-12-27 2006-06-28 Blum Gmbh Julius Method of anchoring a plug element in a building board
CN102256766A (en) * 2008-12-23 2011-11-23 伍德韦尔丁公司 Method of anchoring a connector, and connector
CN104159720A (en) * 2012-03-09 2014-11-19 佛吉亚汽车工业公司 Method of manufacturing a piece of automotive vehicle equipment and associated piece of equipment
CN104411482A (en) * 2012-05-24 2015-03-11 佛吉亚汽车工业公司 Method for producing a piece of reinforced equipment, in particular for a motor vehicle
DE102013213771A1 (en) * 2013-07-15 2015-01-15 Johann Bartlechner Kg Process for the production of concrete parts with plastic lining and device for carrying out the process

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
中国工程塑料工业协会: "《工程塑料实用手册》", 30 November 2005, 亚洲国际出版集团（香港）有限公司 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110439891A (en) * 2018-05-02 2019-11-12 大众汽车有限公司 By dismountable connection for economical space saving fixing component of latch elements
CN112513475A (en) * 2018-07-18 2021-03-16 伊卓特有限两合公司 Connecting element and method for introducing a connecting element
US11413797B2 (en) 2018-07-18 2022-08-16 Ejot Gmbh & Co. Kg Connection element and method for introducing a connection element
CN111038681A (en) * 2018-10-12 2020-04-21 空中客车营运有限公司 Aircraft assembly

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Application publication date: 20180130