CN102239027A - Method for joining resin member with metal member, and liquid-cooled jacket manufacturing method - Google Patents
Method for joining resin member with metal member, and liquid-cooled jacket manufacturing method Download PDFInfo
- Publication number
- CN102239027A CN102239027A CN2009801501669A CN200980150166A CN102239027A CN 102239027 A CN102239027 A CN 102239027A CN 2009801501669 A CN2009801501669 A CN 2009801501669A CN 200980150166 A CN200980150166 A CN 200980150166A CN 102239027 A CN102239027 A CN 102239027A
- Authority
- CN
- China
- Prior art keywords
- throw
- hardware
- resin component
- friction stir
- aluminium alloy
- 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.)
- Granted
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
- B23K20/1245—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding characterised by the apparatus
- B23K20/1255—Tools therefor, e.g. characterised by the shape of the probe
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
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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
- 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
- B29C65/0681—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 created by a tool
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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
- 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
- B29C65/44—Joining a heated non plastics element to a plastics element
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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
- 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
- B29C65/645—Joining a non-plastics element to a plastics element, e.g. by force using friction or ultrasonic vibrations
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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
- B29C66/01—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
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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
- B29C66/01—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
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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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
- B29C66/01—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
- B29C66/114—Single butt joints
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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
- B29C66/01—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
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1222—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a lapped joint-segment
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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
- B29C66/01—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
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1224—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a butt joint-segment
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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
- B29C66/40—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
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
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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
- B29C66/50—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
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
- B29C66/542—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles joining hollow covers or hollow bottoms to open ends of container bodies
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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
- B29C66/50—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
- B29C66/65—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 with a relative motion between the article and the welding tool
- B29C66/652—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 with a relative motion between the article and the welding tool moving the welding tool around the fixed article
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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
- B29C66/70—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
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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
- B29C66/70—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
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
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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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8141—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
- B29C66/81427—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined comprising a single ridge, e.g. for making a weakening line; comprising a single tooth
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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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8141—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
- B29C66/81427—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined comprising a single ridge, e.g. for making a weakening line; comprising a single tooth
- B29C66/81429—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined comprising a single ridge, e.g. for making a weakening line; comprising a single tooth comprising a single tooth
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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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- B29C66/00—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
- B29C66/836—Moving relative to and tangentially to the parts to be joined, e.g. transversely to the displacement of the parts to be joined, e.g. using a X-Y table
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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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- B29C66/00—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
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- B29C66/8362—Rollers, cylinders or drums moving relative to and tangentially to the parts to be joined
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- G06F1/16—Constructional details or arrangements
- G06F1/20—Cooling means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
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- B23K2101/12—Vessels
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
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- B23K2101/18—Sheet panels
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B23K2103/10—Aluminium or alloys thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
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- B23K2103/18—Dissimilar materials
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2200/00—Indexing scheme relating to G06F1/04 - G06F1/32
- G06F2200/20—Indexing scheme relating to G06F1/20
- G06F2200/201—Cooling arrangements using cooling fluid
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- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Provided are a method for joining a resin member with a metal member which allows them to be joined easily while achieving a sufficient level of joint strength, and a liquid-cooled jacket manufacturing method. The joining method is characterized in that after a resin member (2) and a metal member (3) are overlapped, a rotating friction stir tool (G) is pressed from the metal member (3) side and the two members are joined by the heat of friction. According to said joining method, after the resin is melted by the heat of friction, the resin member (2) fuses to the metal member (3) as the temperature drops, so the members can be joined easily and firmly.
Description
Technical field
The present invention relates to the joint method of resin component element and hardware and have resin component element and the manufacture method of the liquid-cooled jacket of hardware.
Background technology
The technology that extensive fields such as automobile industry, industry machine industry are being sought bonding or mechanically affixed resin component element and hardware.As with the method for resin component element, can list the use adhesives with the relative simple and easy joint of hardware.And utilizing adhesives, existence can't obtain the problem of enough intensity.Therefore, in patent documentation 1 disclosed technology, behind the hardware insertion mould with aluminium alloy system, the resin ductile material is penetrated to this mould and with two member engages in advance.
Patent documentation 1: the Japan Patent spy opens the 2007-50630 communique
Summary of the invention
Invent technical problem to be solved
Yet,, can exist the shaping of mould and the demoulding etc. to waste time and energy, engage the numerous and diverse problem of operation if use above-mentioned joint method in the past.In addition, in joint method in the past, while, therefore have the problem that can't engage for the resin component of both having deposited owing to be to carry out injection molding resin is engaged with hardware.That is to say that joint method in the past lacks design freedom.
From the above point of view, technical problem of the present invention is to provide and has enough bond strengths and resin component element and the joint method of hardware and the manufacture method of liquid-cooled jacket that can simple and easy joint.
The technical scheme that the technical solution problem is adopted
In order to address the above problem, the invention is characterized in, after making resin component element and hardware overlap, push the throw of rotation from above-mentioned hardware side, make above-mentioned resin component element fusing engage above-mentioned resin component element and above-mentioned hardware by frictional heat.
According to this joint method, utilize the surface of the frictional heat molten resin member that results from hardware, when hardening once more, engage securely with the hardware welding.That is to say, can only more easily engage two members by the throw of pushing rotation.In addition, according to this joint method,, therefore can improve the free degree of design owing to can engage the resin component element both deposited and hardware, and can only push throw in desired portion.
In addition, comparatively it is desirable to, above-mentioned throw is the friction stir throw, and above-mentioned friction stir is pressed on above-mentioned hardware with the end face of throw.According to this joint method,, therefore can improve the joint precision owing to can push hardware very equably.
In addition, comparatively it is desirable to, above-mentioned hardware is aluminum or aluminium alloy system, and above-mentioned friction stir is set at 2~5 times of thickness of above-mentioned hardware with the external diameter of the shoulder of throw.According to this joint method, can improve the bond strength of two members.If the external diameter of shoulder is than 2 times little of the thickness of hardware, then a little less than the bond strength.On the other hand, if the external diameter of shoulder is than 5 times big of the thickness of hardware, then can be to the bigger load of friction stir device effect, so undesirable.
In addition, comparatively it is desirable to, above-mentioned hardware is aluminum or aluminium alloy system, and above-mentioned friction stir is set at the compression distance of throw above-mentioned hardware thickness 5%~20%.According to this joint method, can improve the bond strength of two members.If friction stir is with 5% little than the thickness of hardware of the compression distance of throw, then a little less than the bond strength.On the other hand, if friction stir is with 20% big than the thickness of hardware of the compression distance of throw, then can be to the bigger load of friction stir device effect, so undesirable.
In addition, comparatively it is desirable to, above-mentioned throw is to be frictionally engaged to use throw, and the side face that will be frictionally engaged with throw presses on above-mentioned hardware.According to this joint method, can engage resin component element and hardware with throw with the frictional heat of hardware by being frictionally engaged of rotation.
In addition, comparatively it is desirable to, above-mentioned hardware is aluminum or aluminium alloy system, and before joint, above-mentioned hardware is carried out etch processes or anodized, and form concavo-convex on the surface.If use this joint method, the resin of fusing can enter the recess that is formed at metal component surface, thereby can engage more firmly.
In addition, the invention is characterized in, have heat supply carry fluid to flow and the resinous cover body of the recess of a part of opening on behind the metal system packaging body of mounting with the peristome sealing of above-mentioned recess, push the throw of rotation from above-mentioned encapsulation side, thereby utilize frictional heat to make the part fusing of above-mentioned cover body and engage above-mentioned cover body and above-mentioned packaging body, wherein, above-mentioned heat carries fluid that the heat delivery that the heat production body is produced is extremely outside.
According to the manufacture method of this liquid-cooled jacket, utilize the frictional heat that results from metal packaging body to melt the resin of cover body, when hardening once more, engage securely with the packaging body welding.That is to say, can only come clutch collar body and packaging body, therefore can easily make liquid-cooled jacket by pushing throw.
In addition, comparatively it is desirable to, make throw along the circumference inboard of above-mentioned packaging body around a circle, and engage above-mentioned cover body and above-mentioned packaging body.By this, the peristome of package cover body, and the operation that can improve joint more reliably.
The invention effect
According to the joint method of resin component element of the present invention and hardware, can engage resin component element and hardware easily and with enough bond strengths.In addition, according to the manufacture method of liquid-cooled jacket of the present invention, can easily make liquid-cooled jacket with enough bond strengths.
Description of drawings
Fig. 1 is the stereogram of the joint method of expression resin component element of first embodiment and hardware.
Fig. 2 is the figure of expression friction stir with throw, and Fig. 2 (a) is a cutaway view, and Fig. 2 (b) is a ground plan.
Fig. 3 is the exploded perspective view of the liquid-cooled jacket of expression second embodiment.
Fig. 4 is the stereogram of packaging body of looking up the liquid-cooled jacket of second embodiment from the below.
Fig. 5 is the vertical view of the friction stir operation of expression second embodiment, Fig. 5 (a) expression beginning part, and Fig. 5 (b) represents latter end.
Fig. 6 is the I-I line cutaway view of Fig. 5 (a).
Fig. 7 is the cutaway view of variation of the friction stir operation of expression second embodiment.
Fig. 8 is the stereogram of the joint method of expression resin component element of the 3rd embodiment and hardware.
Fig. 9 is the stereogram in order to explanation embodiment.
The specific embodiment
First embodiment
With reference to accompanying drawing first embodiment of the present invention is elaborated.As shown in Figure 1, in the present embodiment, be that example describes with the situation that tabular hardware 3 forms composite component 1 to engage tabular resin component element 2.
The resin component element of present embodiment comprising with the joint method of hardware (being designated hereinafter simply as " joint method "): overlap operation, resin component element 2 is overlapped with hardware 3; And the friction stir operation, in this operation, hardware 3 is carried out friction stir.
At first, in overlapping operation, as shown in Figure 1, on resin component element 2, the part of the upper surface of resin component element 2 is contacted with the part of the lower surface of hardware 3 hardware 3 mountings.In the present embodiment, resin component element 2 is PET (polyethylene terephthalate; PET) Zhi tabular component.The material of resin component element 2 is not limited to PET, can do suitably to select from thermoplastic resin according to purposes.
In the present embodiment, hardware 3 is tabular components of aluminium alloy system (A5052-O).Hardware 3 can be done suitably to select the metal material of friction stir from aluminium, aluminium alloy, copper, copper alloy, titanium, titanium alloy, magnesium, magnesium alloy etc. according to purposes.Below, also hardware 3 is called " aluminium alloy element 3 ".
Next, in the friction stir operation, shown in Fig. 2 (a) and Fig. 2 (b), use throw G (below be also referred to as friction stir throw G), aluminium alloy element 3 is carried out friction stir from the upper surface side of aluminium alloy element 3.Friction stir with throw G have roughly cylindrical shoulder G1, from outstanding pin (pin) G2 of portion of the lower surface (end face) of shoulder G1.Friction stir is made of tool steel geometric ratio aluminium alloy element 3 also hard metal materials with throw G.Shown in Fig. 2 (b), the G2 of pin portion has and overlooks spiral spire G11, is formed at the central authorities of shoulder G1 and overlooks rounded rounded portions G12.The shape of shoulder G1 and the G2 of pin portion, size etc. can be done suitable setting according to the object that engages.In addition, also can use the smooth friction stir throw of lower surface (end face) that the G2 of pin portion, shoulder G1 are not set.
In the friction stir operation, fixing resin member 2 and aluminium alloy element 3 and after it can't be moved, make the lower surface (end face) and aluminium alloy element 3 subtends of friction stir with throw G, optional position at the upper surface of aluminium alloy element 3 is pressed into (pushing) prescribed depth, and friction stir is relatively moved along the long side direction of aluminium alloy element 3 with throw G.There is no particular restriction for the rotating speed (rotary speed) of friction stir usefulness throw G and engaging speed (feed speed), for example moves with rotating speed 1000rpm, engaging speed 300mm/min.
At the upper surface of aluminium alloy element 3, form plastification zone W with the motion track of throw G along friction stir.At this, " plastification zone " comprises because of friction stir and is heated the state that shows as plastification, friction stir with throw G this two states of state by getting back to normal temperature with the frictional heat of throw G.In the present embodiment, with plastification zone W not the compression distance of the degree of contact pressure resin member 2 carry out friction stir.In addition, preferably will be because of the burr excision of friction stir in the upper surface generation of aluminium alloy element 3 by machining.
If use above-mentioned joint method, for the intersection of resin component element 2 with aluminium alloy element 3, the friction stir of pushing rotation from the top of aluminium alloy element 3 is with throw G and move it, utilize frictional heat to come the resin of molten resin member 2 surfaces (top layer part), and make its underhardening again along with the temperature reduction.By this, resin component element 2 is welded in the lower surface of aluminium alloy element 3 and engages.That is to say, can only more easily engage two members with throw G by pushing friction stir.In addition, in above-mentioned existing method, owing to carry out engaging of the injection molding of resin and resin component element and aluminium alloy element simultaneously, therefore can not the member of both having deposited be engaged, but, then also can resin component element 2 and the aluminium alloy element of both having deposited 3 be engaged if use the joint method of present embodiment.
In addition, owing to only push friction stir throw G at desired joint, thus can improve the free degree of design.In addition, because, therefore can improve the joint precision by the end face of friction stir with throw G is pressed into aluminium alloy element 3 and can balancedly pushes hardware.In addition, also can be bonded into the plastification zone W that forms because of friction stir and contact, but also can be shown in present embodiment, carry out more shallow friction stir with resin component element 2 discontiguous degree and engage with the regional W of plastification with resin component element 2.
In addition, comparatively it is desirable to, friction stir is set at 2~5 times of thickness of aluminium alloy element 3 with the external diameter of the shoulder G1 of throw G.In addition, comparatively it is desirable to, friction stir is set at the compression distance of throw G (being pressed into till from the upper surface of aluminium alloy element 3 to the lower surface of shoulder G1 length) aluminium alloy element 3 thickness 5%~20%.By external diameter or the friction stir of shoulder G1 are done above-mentioned setting with the compression distance of throw G, can improve bond strength.It is according to narration below.
In addition, comparatively it is desirable to, aluminium alloy element 3 at least with face that resin component element 2 contacts on, carry out etch processes or pellumina (anodic oxidation) and handle, form on this contact-making surface concavo-convex after, carry out above-mentioned friction stir operation.If use this joint method, the recess that can enter aluminium alloy element 3 owing to the resin that has melted increases the contact area of resin component element 2 and aluminium alloy element 3, so can engage more firmly.
Etch processes for example is aluminium alloy element 3 to be impregnated in hydrochloric acid solution add aluminum chloride hexahydrate and modulate the etching solution that forms and carry out.On the other hand, pellumina is handled and to be to use dilute sulfuric acid or oxalic acid etc. and to be that anode is done electrolysis with the aluminium alloy, thereby in electrochemical mode the surface oxidation of aluminium alloy element 3 is carried out.
In addition, become the surface treatment of convex-concave surface, be not defined as etch processes or pellumina and handle, for example also can utilize metal plug lapped faces such as (wire brush) to make its alligatoring and form concavo-convex as the surface that makes aluminium alloy element 3.
Second embodiment
Next, second embodiment of the present invention is described.In the present embodiment, as shown in Figure 3, the situation that has resinous cover body 10 and the liquid-cooled jacket P of the packaging body 30 of metal system (being aluminium alloy system in the present embodiment) with manufacturing is that example describes.Liquid-cooled jacket P for example is used for CPU (central processing unit; CPU) cooling of heat production body such as.
As shown in Figure 3, liquid-cooled jacket P carries the water (not shown) of fluid to flow and the cover body 10 of the recess 11 of a part of opening, the packaging body 30 of peristome 12 that is fixed in the encapsulation recess 11 of cover body 10 are constituted by having the heat of being provided as, and wherein above-mentioned heat carries heat delivery that fluid will be produced as the CPU (not shown) of heat production body to the outside.
The liquid-cooled jacket P central authorities of the cover plate portion 31 of side above it is equipped with CPU (not shown) across fin (not shown), under the state that CPU is installed, cooling water is circulated in liquid-cooled jacket P, capture the heat that CPU produces, and carry out heat exchange with cooling water at internal circulation.By this, cover plate portion 31 will be passed to cooling water from the heat that CPU obtains, and consequently, can cool off CPU effectively.In addition, fin is the tablet that is used for the heat of CPU is passed to effectively cover plate portion 31, for example is to be formed by the metal that copper etc. has a high-termal conductivity.
Around openings edge part 12a at the recess 11 that overlaps body 10 is formed with step surface 15 at the upper surface from perisporium 14 to the position of next segment distance.Distance (degree of depth) till from the upper surface of perisporium 14 to step surface 15 is identical with the gauge of the cover plate portion 31 of hereinafter described packaging body 30.The periphery of the cover plate portion 31 of mounting packaging body 30 on step surface 15.In order to ensure the volume of the recess 11 that supplies flow of cooling water, preferably set the width W 1 of step surface 15 as far as possible little, and in the present embodiment, form bigger with the external diameter of the shoulder G1 of throw G than friction stir.
In a pair of wall 14a of portion, the 14a of the mutual subtend of perisporium 14, form the promising through hole 16,16 that makes cooling water flow into recess 11 respectively.In the present embodiment, through hole 16,16 extends along the subtend direction (directions X among Fig. 3) of the 14a of wall portion, 14a, and has circular cross-section, is formed at the pars intermedia of the depth direction of recess 11.In addition, the shape and the position of through hole 16 are not limited to this, can do suitably change according to the kind of cooling water, flow etc.
As shown in Figures 3 and 4, packaging body 30 has tabular cover plate portion 31 and a plurality of fin 32,32 ... its cover plate portion 31 has the flat shape with the peristome 12 (with reference to Fig. 3) of the recess 11 that overlaps body 10 identical shaped (being square in present embodiment), a plurality of fins 32,32 ... be located at the lower surface of cover plate portion 31.
A plurality of fins 32,32 ... be configured to be parallel to each other and with cover plate portion 31 quadratures, and form one with cover plate portion 31.By this, heat can be successfully at cover plate portion 31 and fin 32,32 ... between transmit.As shown in Figure 3, fin 32,32 ... be configured to going up extension with the 14a of wall portion of the perisporium 14 that is formed with through hole 16,16, the direction (X-direction among Fig. 3) of 14a quadrature.The height of fin 32 (degree of depth) size (the Z-direction length among Fig. 3) equates with the depth dimensions of recess 11, makes its leading section be connected to the bottom surface of recess 11.By this, be installed at packaging body 30 under the state of cover body 10, utilize the cover plate portion 31 of packaging body 30, adjacent fin 32,32, the bottom surface of recess 11 to mark off the space of tubular, the function in this space is as the stream 33 (with reference to Fig. 5 (a)) for flow of cooling water.In addition, fin 32,32 ... length dimension (the X-direction length among Fig. 3) shorter than the length dimension on one side of recess 11, and the internal face of each 14a of wall portion, 14a of the perisporium 14 of its two ends and recess 11 is respectively across predetermined distance.By this, under the state that packaging body 30 is installed on cover body 10, fin 32,32 ... the 14a of wall portion of the perisporium 14 two ends outsides and recess 11 between the space constitute from through hole 16 and compile portion 34 (with reference to Fig. 5 (a)) towards stream with direction (Y direction Fig. 3) expansion of the bearing of trend quadrature of fin 32.
Next, with Fig. 5 the manufacture method of liquid-cooled jacket P is specifically described.The manufacture method of the liquid-cooled jacket of present embodiment comprises: the mounting operation, in this operation, with packaging body 30 mountings in the cover body 10; And the friction stir operation, in this operation, friction stir is carried out in 40 inboard along the docking section.
In the mounting operation, shown in Fig. 3 and Fig. 5 (a), make fin 32 be positioned at downside and packaging body 30 inserted the recess 11 of cover bodies 10, thereby with cover plate portion 31 mountings of packaging body 30 on step surface 15.At this, the opening circumference 12a of the recess 11 of cover body 10 docks with the circumference 30a of packaging body 30, thereby constitutes docking section 40.
In the friction stir operation, friction stir is relatively moved along the inboard of this docking section 40 with throw G.After friction stir is pushed with packaging body 30 subtends and with the regulation compression distance with the lower surface (end face) of throw G, its step surface 15 (with reference to Fig. 3) along cover body 10 is moved with the intersection that the cover plate portion 31 of packaging body 30 overlaps.Comparatively it is desirable to this moment, and the circumferential surface at the perisporium 14 that overlaps body 10 puts the anchor clamps (not shown) that surround cover body 10 from four direction in advance, so that cover body 10 does not move.
In the friction stir operation,, friction stir is set in the inboard of docking section 40 with the insertion position (starting end 54a) of throw G as Fig. 5 (a) and shown in Figure 6.Then, with friction stir with the overlapping state in the center of the width of the pivot Q of throw G and step surface 15 under, make friction stir move cover plate portion 31 made friction stir with throw G.
Afterwards, the continuation friction stir is used the rotation of throw G and is moved, and shown in Fig. 5 (b), makes friction stir form plastification zone W around making a circle in week of peristome 12 with throw G.At this moment, friction stir is overlapping with the starting end 54a (with reference to Fig. 5 (a)) of throw G with finishing end 54b (with reference to Fig. 5 (b)), makes that the part of plastification zone W is overlapping.
As mentioned above, friction stir the inboard of 40 (with reference to Fig. 5 (a)) is detoured week and carry out friction stir along the docking section with throw G, thereby packaging body 30 is fixed in cover body 10, form liquid-cooled jacket P by this.
According to the manufacture method of the liquid-cooled jacket P of present embodiment, the packaging body 30 of aluminium alloy system is made friction stir, utilize its frictional heat to melt the resin of cover body 10, and when hardening once more, weld and engage securely with packaging body 30.That is to say, can be only by pushing friction stir with throw G and it is relatively moved and clutch collar body 10 and packaging body 30, therefore can easily make liquid-cooled jacket P.In addition, detour a week around packaging body 30 with throw G, can improve bond strength, and can improve the operation of joint by making friction stir.In addition, even, still can engage with plastification zone W and step surface 15 compression distance of exposure level not.
In addition, comparatively it is desirable to, friction stir is set at 2~5 times of thickness of the cover plate portion 31 of packaging body 30 with the external diameter of the shoulder G1 of throw G.In addition, comparatively it is desirable to, friction stir is set at the compression distance of throw G (being pressed into till from the upper surface of cover plate portion 31 to the lower surface of shoulder G1 length) packaging body 30 cover plate portion 31 thickness 5%~20%.By external diameter or the friction stir of shoulder G1 are done above-mentioned setting with the compression distance of throw G, can improve bond strength.It is according to narration below.
In addition, also can be before carrying out the friction stir operation, the face that contact with the step surface 15 of cover body 10 at least of the cover plate portion 31 of packaging body 30 is carried out etch processes or pellumina processing.Form concavo-convexly by the surface at the packaging body 30 of aluminium alloy system, the resin that has melted can enter this recess and increase contact area, thereby can make more firm joint.
In addition, in the present embodiment, be provided with step surface 15, packaging body 30 mountings in step surface 15, but are not limited to this at cover body 10.For example shown in Figure 7, also can be with cover plate portion 31 mountings of packaging body 30 upper surface in the perisporium 14 of cover body 10, friction stir is relatively moved along the lap of perisporium 14 and cover plate portion 31 with throw G carry out the friction stir operation.
The 3rd embodiment
Next, the 3rd embodiment of the present invention is described.In first embodiment and second embodiment, use friction stir to carry out the friction stir operation with throw G, thereby engage resin component element 2 and hardware 3, and in the 3rd embodiment, in that to use throw F to carry out the friction process this point different with first embodiment and second embodiment.
The joint method of present embodiment comprises: overlap operation, in this operation, resin component element 2 is overlapped with hardware 3; And friction process, in this operation, the member that has overlapped is frictionally engaged.About overlapping operation, omit its explanation owing to identical with first embodiment.
In friction process, as shown in Figure 8, use throw F (below be also referred to as to be frictionally engaged use throw F) to come resin component element 2 and hardware 3 (aluminium alloy element 3) are frictionally engaged.
Be frictionally engaged and have rotating shaft F1, be arranged at the tool body F2 of rotating shaft F1 front end with throw F.Rotating shaft F1 and tool body F2 are with coaxial formation.The base end side of rotating shaft F1 and not shown drive unit link.Tool body F2 is subjected to the driving of the drive unit that transmitted via rotating shaft F1, and rotates at a high speed around axle.Tool body F2 is discoideus, is made of the also hard metal material of tool steel geometric ratio aluminium alloy.
Be frictionally engaged with the shape of throw F, size etc., can do suitable setting according to the member that engages, and in the present embodiment, the diameter that uses tool body F2 for example is the width of 100mm, the side face F3 throw as 4mm.In addition, the compression distance of the usefulness that is frictionally engaged throw F, rotating speed, engaging speed etc., can do suitable setting according to the member that engages, and in the present embodiment, for example setting compression distance for is that 0.2mm, rotating speed are that 3000rpm, engaging speed are 500~1500mm/min.
In friction process, fixing resin member 2 and aluminium alloy element 3 and after it can't be moved, make on one side and be frictionally engaged with throw F rotation, side face F3 with tool body F2 is pressed into (pushing) prescribed depth at the upper surface of aluminium alloy element 3 on one side, and it is moved along the lap of resin component element 2 with aluminium alloy element 3.In friction process, utilizing is frictionally engaged comes the surface of molten resin member 2 with the frictional heat of throw F and aluminium alloy element 3, thus when hardening once more welding aluminum alloy member 3 and joint securely.
By the joint method of the 3rd embodiment, also can obtain the effect roughly the same with first embodiment.In addition, in friction process, owing to can engage with the pressing force littler than the pressing force of first embodiment, thereby can be applicable to the thin situation of member of joint.
In addition, in the 3rd embodiment, also can carry out etch processes or pellumina (anodic oxidation) to the face that contacts with resin component element 2 at least of aluminium alloy element 3 and handle, this contact-making surface is formed concavo-convex after, carry out above-mentioned friction process.In addition, in the 3rd embodiment, be that example explains with the situation that engages tabular resin component element 2 and aluminium alloy element 3, but be not limited to this.For example also can as put down in writing, second embodiment when making liquid-cooled jacket, carry out friction process and replace the friction stir operation.
Use friction stir to be frictionally engaged with the embodiment 4 of throw F with embodiment 1~embodiment 3, the use of throw G.
Fig. 9 is the stereogram in order to explanation embodiment 1~embodiment 3.In embodiment 1~embodiment 3, as shown in Figure 9, after making tabular resin component element 2 and tabular aluminium alloy element 3 overlap, from the top of aluminium alloy element 3 this coincidence part branch pressure type is pushed friction stir throw G, and the breakdown strength that engages composite component 1 by frictional heat is measured.The mensuration of breakdown strength is that composite component shown in Figure 91 is arranged at the known stretching testing machine, and the outboard end of resin component element 2 and the outboard end of aluminium alloy element 3 are carried out towards the direction stretching, the destruction that are separated from each other.
In embodiment 1,, under these six kinds of conditions of test 1-a~test 1-f, measure the breakdown strength (hot strength) under the situation of doing to engage with the regulation compression distance in order to draw the only compression distance of friction stir with throw G.The condition of each test is shown in table 1.
[table 1]
The kind of aluminium | The thickness of slab of aluminium (mm) | Shoulder external diameter (mm) | Instrument rotating speed (rpm) | |
Test 1-a | A5052- |
3 | 15.0 | 1500 |
Test 1-b | A5052-O | 5 | 15.0 | 1500 |
Test 1-c | A1100- |
3 | 12.5 | 2500 |
Test 1-d | A1100-H14 | 5 | 12.5 | 2500 |
Test 1-e | A6061- |
3 | 17.5 | 700 |
Test 1-f | A6061-T6 | 5 | 17.5 | 700 |
To test among 1-a~test 1-f, the breakdown strength under the regulation compression distance the results are shown in table 2.And in the judgement hurdle in table 2, table 4 and the table 6, " * " expression does not engage, the hot strength of joint is weak though expression has " △ ", " zero " expression has enough hot strengths.
[table 2]
As shown in table 2, the result of development test 1-a and test 1-b, if compression distance be more than the 0.2mm then breakdown strength be more than the 3000N, but if compression distance is below the 0.05mm, then since the shallow excessively skin section that causes resin component element 2 of compression distance do not melt and can not engage.In addition we know, if compression distance is 0.1mm, being that the situation of 5mm is next at the thickness of slab of aluminium alloy element 3 engages, if thickness of slab is 3mm, although it is little then to take place to engage breakdown strength.At compression distance is under the situation of 0.2mm, with respect to the ratio of the thickness of slab of aluminium alloy element 3, at thickness of slab be under the situation of 3mm be 6.7%, situation that thickness of slab is 5mm is next is 4%.
In addition, development test 1-c and test 1-d, test 1-e and test 1-f as can be known, therefore its result is roughly the same with test 1-a and test 1-b, can know that the kind of aluminium alloy element 3 can not exert an influence to breakdown strength.
As mentioned above, even friction stir is set at 5% little than the thickness of slab of aluminium alloy element 3 with the compression distance of throw G, still can engage resin component element 2 and aluminium alloy element 3, but in order to obtain enough hot strengths, comparatively it is desirable to, friction stir is set at more than 5% of thickness of slab of aluminium alloy element 3 with the compression distance of throw G.
On the other hand, if set greatlyyer with the compression distance of throw G friction stir, then, the formed plastification of friction stir zone causes metal and mixed with resin because of may contacting with resin component element 2.In addition, if set greatlyyer with the compression distance of throw G friction stir, then can be to the excessive load of friction stir device effect.Therefore,, then comparatively it is desirable to, friction stir is set at below 20% of thickness of slab of aluminium alloy element 3 with the compression distance of throw G if consider these factors.
[embodiment 2]
In embodiment 2, in order to draw the external diameter of friction stir with the only shoulder G1 (with reference to Fig. 2) of throw G, under test 2-a~test 2-b these two kinds of conditions, the breakdown strength (hot strength) under the situation that mensuration engages with throw G with the friction stir of the external diameter of shoulder G1 with regulation.The condition of each test is shown in table 3.
[table 3]
The kind of aluminium | The thickness of slab of aluminium (mm) | Compression distance (mm) | |
Test 2-a | A5052- |
3 | 0.8 |
Test 2-b | A5052-O | 5 | 0.8 |
In test 2-a, test 2-b, the breakdown strength of the external diameter of the shoulder of regulation the results are shown in table 4.
[table 4]
As shown in table 4, in test 2-a, if the external diameter ratio of shoulder
Greatly then breakdown strength is more than the 3000N, if
Significantly descend with next breakdown strength.
On the other hand, in test 2-b, if the external diameter of shoulder is
Below then breakdown strength is more than the 3000N, if
Significantly descend with next breakdown strength.
As mentioned above, even friction stir is set at than the thickness of slab of aluminium alloy element 32 times little with the external diameter of the shoulder G1 of throw G, still can engage resin component element 2 and aluminium alloy element 3, but in order to obtain enough hot strengths, comparatively it is desirable to, making friction stir is more than 2 times of thickness of slab of aluminium alloy element 3 with the external diameter of the shoulder G1 of throw G.In addition, though since the external diameter of shoulder G1 than the 5 times also big of thickness of slab of aluminium alloy element 3, intensity is no change still, considers the load that the friction stir device is applied, and comparatively it is desirable to, and the external diameter of shoulder G1 is set at below 5 times of thickness of slab of aluminium alloy element 3.
[embodiment 3]
In embodiment 3, the surface at aluminium alloy element 3 formed under the concavo-convex situation test with the relation of breakdown strength.Under test 3-a~test 3-b these three kinds of conditions, the breakdown strength (hot strength) under the situation that mensuration carries out engaging after the predetermined processing to the surface of aluminium alloy element 3.The condition of each test is shown in table 5.
[table 5]
The kind of aluminium | The thickness of slab of aluminium (mm) | The external diameter of shoulder (mm) | Compression distance (mm) | |
Test 3-a | A5052-O | 5 | 15.0 | 0.8 |
Test 3-b | A6061- |
3 | 15.0 | 0.8 |
Test 3-c | A1100- |
3 | 12.5 | 0.8 |
In test 3-a~test 3-c, the breakdown strength in each surface treatment of aluminium alloy element 3 the results are shown in table 6.
" non-processor " in the surface treatment that carry out on the surface at aluminium alloy element 3 in the table 6 is not meant aluminium alloy element 3 carried out surface treatment.
In addition, in " etching A ", carry out etching pre-treatment and etching shown below and formally handle.In the etching pre-treatment, at first, at normal temperatures aluminium alloy element 3 is flooded 5 minutes in the salpeter solution of 30wt% after, wash fully with ion exchange water.Next, 1 minute after washing of dipping in the sodium hydroxide solution at 5wt% under 50 ℃, 3 minutes after washings of dipping in the salpeter solution at 30wt% under the normal temperature again.
In the formal processing of etching, carry out following etch processes, the aluminum chloride hexahydrate that impregnated in 54g/L at the 66 ℃ of following aluminium alloy elements 3 that will finish the etching pre-treatment makes an addition to 4 minutes after washings in the etching solution of being modulated in the hydrochloric acid solution of 25wt% (chlorine ion concentration is 48g/L), in the salpeter solution at 30wt% under the normal temperature, flood 3 minutes after washings again, carry out 5 minutes drying again with 120 ℃ hot blast.
In addition, in " etching B ", after finishing above-mentioned etching pre-treatment, carry out etching shown below and formally handle.That is to say, in the formal processing of this etching, flood 4 minutes after washings in the phosphoric acid solution of aluminium alloy element 3 after will carrying out the etching pre-treatment under 66 ℃, carry out 5 minutes drying afterwards with 120 ℃ hot blast at 50wt%.
In addition, in " alumina-free film sealing of hole ", carry out pellumina pre-treatment, pellumina shown below and formally handle.In the pellumina pre-treatment, at first, after at normal temperatures aluminium alloy element 3 being flooded 5 minutes in the salpeter solution of 30wt%, wash fully with ion exchange water, next, 1 minute after washing of dipping in the sodium hydroxide solution at 5wt% under 50 ℃, 3 minutes after washings of dipping in the salpeter solution at 30wt% under the normal temperature again.
In the formal processing of pellumina; is that 18 ℃ sulfuric acid concentration is to carry out anodic oxidation in the solution of 160g/L to make diaphragm thickness be 10 μ m after washings with the aluminium alloy element 3 that carries out after the pellumina pre-treatment in the liquid temperature, carries out 5 minutes drying again with 120 ℃ hot blast.
In addition, in " the pellumina sealing of hole is arranged ", after carrying out above-mentioned pellumina pre-treatment, carry out above-mentioned pellumina and formally handle.Afterwards, in the water of boiling, boiled 10 minutes.By this, in " the pellumina sealing of hole is arranged ", carry out the sealing of hole processing and pore is narrowed down.
In addition, in " metal plug ", use known metal plug (wire brush) that alligatoring is carried out on the surface of aluminium alloy element 3 and cut and do concavo-convex processing.
[table 6]
As shown in table 6, the result of development test 3-a and test 3-b has carried out surface treatment and has made the surface irregularity of aluminium alloy element 3 as can be known, and its hot strength is higher.In addition we know, even aluminium alloy element 3 is not carried out still can obtaining enough hot strengths under the surface-treated situation.
In addition, research is with the thickness of slab attenuation of aluminium alloy element 3 and dwindle friction stir with the result of the test 3-c of the shoulder external diameter of throw G as can be known, carry out " etching A ", " etching B " reaches under the surface-treated situation of " alumina-free film sealing of hole ", can obtain higher draw tensile strength.
[embodiment 4]
In embodiment 4, the breakdown strength of the member that engaged in the joint method that illustrates at the 3rd embodiment (ginseng cover Fig. 8) is measured.The member that has engaged is arranged at cupping machine, the outboard end of resin component element 2 and the outboard end of aluminium alloy element 3 are stretched, destroy the mensuration of carrying out breakdown strength towards separated direction.
The diameter that is frictionally engaged with throw F tool using body F2 is that 100mm, width are that the instrument C of 4mm and the diameter of tool body F2 are that 105mm, width are these two kinds of instruments of instrument D of 10mm.For instrument C, be 3000rpm with speed setting, for instrument D, be 2857rpm then with speed setting.The peripheral speed of instrument C and instrument D all is set at 942000 (mm/min).
In embodiment 4, change the combination of the thickness of each member and throw and set three kinds of (test 4~test 6) preconditions, and be that parameter is carried out failure test with compression distance and engaging speed (feed speed).
Test 4 the table 7 that the results are shown in.
[table 7]
<test 4〉stretch test result (N)
Test 5 the table 8 that the results are shown in.
[table 8]
<test 5〉stretch test result (N)
According to table 7 and table 8, the bond strength that the compression distance of instrument C and instrument D is under the 0.2mm situation is lower, and is that bond strength under the 0.4mm situation is higher at compression distance.When engaging speed is 500mm/min, destroy from resin component element 2.Till engaging speed reaches 1500mm/min, all have enough bond strengths, and under the situation of 2000mm/min, bond strength is lower.
On the other hand, for the influence of the thickness of slab of studying aluminium alloy element 3, be the table 9 that the results are shown in of the test 6 carried out of 1mm with the thickness of slab of aluminium alloy element 3.
[table 9]
<test 6〉stretch test result (N)
As shown in table 9, even the thickness of slab of aluminium alloy element 3 is 1mm, still obtaining with thickness of slab is the roughly the same result of situation (with reference to table 8) of 2mm.
(symbol description)
1: composite component;
2: resin component element;
3: hardware (aluminium alloy element);
10: cover body (resin component element);
11: recess;
12: peristome;
12a: opening circumference;
14: perisporium;
15: step surface;
30: packaging body (aluminium alloy element);
30a: circumference;
31: cover plate portion;
32: fin;
F: throw (be frictionally engaged and use throw);
G: throw (friction stir throw);
P: liquid-cooled jacket.
Claims (8)
1. the joint method of resin component element and hardware is characterized in that,
After making resin component element and hardware overlapping, push the throw of rotation, utilize frictional heat to make the fusing of described resin component element and engage described resin component element and described hardware from described hardware side.
2. the joint method of resin component element as claimed in claim 1 and hardware is characterized in that,
Described throw is the friction stir throw,
Described friction stir is pressed on described hardware with the end face of throw.
3. the joint method of resin component element as claimed in claim 2 and hardware is characterized in that,
Described hardware is aluminum or aluminium alloy system,
Described friction stir is set at 2~5 times of thickness of described hardware with the external diameter of the shoulder of throw.
4. as the joint method of claim 2 or 3 described resin component elements and hardware, it is characterized in that,
Described hardware is aluminum or aluminium alloy system,
Described friction stir is set at the compression distance of throw described hardware thickness 5%~20%.
5. the joint method of resin component element as claimed in claim 1 and hardware is characterized in that,
Described throw is to be frictionally engaged to use throw,
The side face that is frictionally engaged with throw is pressed on described hardware.
6. the joint method of resin component element as claimed in claim 1 and hardware is characterized in that,
Described hardware is aluminum or aluminium alloy system,
Before joint, described hardware is carried out etch processes or anodized and form concavo-convex on the surface.
7. the manufacture method of a liquid-cooled jacket is characterized in that,
Have heat supply carry fluid to flow and the resinous cover body of the recess of a part of opening on behind the metal packaging body of mounting with the peristome sealing of described recess, push the throw of rotation from described encapsulation side, engage described cover body and described packaging body and utilize frictional heat that the part of described cover body is melted, described heat carries fluid that the heat delivery that the heat production body is produced is extremely outside.
8. the manufacture method of liquid-cooled jacket as claimed in claim 7 is characterized in that,
Make described throw along the inboard of the circumference of described packaging body around a circle, engage described cover body and described packaging body.
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JP2009260768A JP5531573B2 (en) | 2008-12-09 | 2009-11-16 | Method for joining resin member and metal member, method for manufacturing liquid cooling jacket, and liquid cooling jacket |
JP2009-260768 | 2009-11-16 | ||
PCT/JP2009/070541 WO2010067796A1 (en) | 2008-12-09 | 2009-12-08 | Method for joining resin member with metal member, and liquid-cooled jacket manufacturing method |
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KR (3) | KR101471796B1 (en) |
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CN104308357B (en) | 2016-06-29 |
CN102239027B (en) | 2014-12-03 |
KR20110102412A (en) | 2011-09-16 |
KR20140034326A (en) | 2014-03-19 |
KR20130085060A (en) | 2013-07-26 |
JP5531573B2 (en) | 2014-06-25 |
CN104308357A (en) | 2015-01-28 |
TW201437601A (en) | 2014-10-01 |
KR101302349B1 (en) | 2013-08-30 |
KR101471796B1 (en) | 2014-12-10 |
KR101465406B1 (en) | 2014-11-25 |
TWI552856B (en) | 2016-10-11 |
TW201029826A (en) | 2010-08-16 |
WO2010067796A1 (en) | 2010-06-17 |
JP2010158885A (en) | 2010-07-22 |
TWI609166B (en) | 2017-12-21 |
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