JPS6264528A - Joining of synthetic resin material and different material - Google Patents

Joining of synthetic resin material and different material

Info

Publication number
JPS6264528A
JPS6264528A JP60205764A JP20576485A JPS6264528A JP S6264528 A JPS6264528 A JP S6264528A JP 60205764 A JP60205764 A JP 60205764A JP 20576485 A JP20576485 A JP 20576485A JP S6264528 A JPS6264528 A JP S6264528A
Authority
JP
Japan
Prior art keywords
plate member
synthetic resin
resin material
joint surface
joining
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
JP60205764A
Other languages
Japanese (ja)
Inventor
Toshihisa Terasawa
寺沢　利久
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP60205764A priority Critical patent/JPS6264528A/en
Publication of JPS6264528A publication Critical patent/JPS6264528A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
    • B29C37/0082—Mechanical anchoring
    • B29C37/0085—Mechanical anchoring by means of openings in the layers
    • 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
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16—Laser beams
    • B29C65/1629—Laser beams characterised by the way of heating the interface
    • B29C65/1635—Laser beams characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. laser transmission 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
    • B29C65/44—Joining a heated non plastics element to a plastics element
    • 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
    • B29C65/606—Riveting or staking the rivets being integral with one of the parts to be joined, i.e. staking
    • 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
    • B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/024—Thermal pre-treatments
    • B29C66/0246—Cutting or perforating, e.g. burning away by using a laser or using hot air
    • 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
    • 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
    • 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
    • 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
    • B29C66/52—Joining tubular articles, bars or profiled elements
    • B29C66/522—Joining tubular articles
    • B29C66/5221—Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other
    • 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
    • B29C66/712—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 the composition of one of the parts to be joined being different from the composition of the other part
    • 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
    • B29C66/70—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
    • 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
    • B29C66/7428—Transition metals or their alloys
    • B29C66/74283—Iron or alloys of iron, e.g. steel
    • 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
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16—Laser beams
    • B29C65/1603—Laser beams characterised by the type of electromagnetic radiation
    • B29C65/1612—Infrared [IR] radiation, e.g. by infrared lasers
    • B29C65/1616—Near infrared radiation [NIR], e.g. by YAG lasers
    • 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
    • B29C65/46—Joining a heated non plastics element to a plastics element heated by induction
    • 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
    • B29C65/606—Riveting or staking the rivets being integral with one of the parts to be joined, i.e. staking
    • B29C65/608—Riveting or staking the rivets being integral with one of the parts to be joined, i.e. staking the integral 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
    • B29C66/12—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
    • 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
    • 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
    • B29C66/74—Joining plastics material to non-plastics material
    • B29C66/746—Joining plastics material to non-plastics material to inorganic materials not provided for in groups B29C66/742 - B29C66/744
    • B29C66/7461—Ceramics
    • 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
    • B29C66/746—Joining plastics material to non-plastics material to inorganic materials not provided for in groups B29C66/742 - B29C66/744
    • B29C66/7461—Ceramics
    • B29C66/74611—Carbides; Nitrides
    • 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
    • B29C66/746—Joining plastics material to non-plastics material to inorganic materials not provided for in groups B29C66/742 - B29C66/744
    • B29C66/7465—Glass
    • 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
    • B29L2031/737—Articles provided with holes, e.g. grids, sieves

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Health & Medical Sciences (AREA)
  • Electromagnetism (AREA)
  • Toxicology (AREA)
  • Chemical & Material Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

PURPOSE:To easily perform the joining work of synthetic resin material and different material by a method wherein the synthetic resin material, which is non-absorptive to laser beams, is used in this case and placed upon the different material, on which through holes are made, so as to heat and melt the synthetic resin material by means of the heat generated in the different material by irradiating the different material with laser beam through the synthetic resin material in order to push out the resultant melt into the through holes to join both the materials. CONSTITUTION:The joint surface 2b of a plate member 2 is set to the joint surface 1a of a plate member 1 so as to mate with each other. The irradiation nozzle 3 of a YAG:Nd<3+> laser is abutted against the top surface of the plate member 2 at the position corresponding to a through hole 1c made on the plate member 1 in order that irradiation is made with YAG laser beams 4 with a wave length of 1.06mum and the output of 20W through a working lens 5. The YAG laser beams 4, which reach the joint surface 1a of the plate member 1, are stored in the form of energy at and around the irradiated portion and at the same time the joint surface of the plate member 1 is heated by said stored energy. The joint surface 2b of the plate member 2 is heated and melted by the heat transmitted from the joint surface 1a. After that, the joint surface 1a of the plate member 1 is applied with load in the direction indicated with the arrow A by means of the irradiation nozzle 3, while being heated by the YAG laser beams 4.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、合成樹脂材料と異種材料の接合方法に関し、
さらに詳しくは、合成樹脂材料と穴明き異種材料を重ね
合わせ、合成樹脂材料の方向からレーザ光を照射して、
その溶融物によって両材料を接合する方法に係るもので
ある。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a method for joining synthetic resin materials and dissimilar materials,
More specifically, by overlapping a synthetic resin material and a different material with holes, and irradiating a laser beam from the direction of the synthetic resin material,
This relates to a method of joining both materials using the melt.

〔従来の技術〕[Conventional technology]

従来、合成樹脂材料と異種材料の一つである鋼板とを接
合する際には、第２図に示すようなインブラント接合方
法が利用されている。Conventionally, when joining a synthetic resin material and a steel plate, which is one of the dissimilar materials, an implant joining method as shown in FIG. 2 has been used.

第２図において、５１は金属材料からなる円筒部材であ
って、この円筒部材５１の上端部に内径の大きな溝５２
が形成されており、その上面には金属材料からなるリン
グ５３が設けられている。In FIG. 2, reference numeral 51 denotes a cylindrical member made of a metal material, and a groove 52 with a large inner diameter is formed at the upper end of the cylindrical member 51.
is formed, and a ring 53 made of a metal material is provided on its upper surface.

また、このリング５３の上面には円筒部材５１の溝５２
から挿入された熱可塑性樹脂からなる筒状部材５４が載
１されており、その内径は円筒部材５１の内径と同一と
されている。さらに、円筒部材５１と筒状部材５４との
外周には間隔を有して誘導コイル５５が配設されており
、その一端は図示を省略した高周波電流発生器に接続さ
れている。Further, on the upper surface of this ring 53, a groove 52 of the cylindrical member 51 is provided.
A cylindrical member 54 made of thermoplastic resin inserted from the cylindrical member 51 is placed thereon, and its inner diameter is the same as the inner diameter of the cylindrical member 51. Further, an induction coil 55 is disposed at a distance between the outer peripheries of the cylindrical member 51 and the cylindrical member 54, and one end of the induction coil 55 is connected to a high frequency current generator (not shown).

そして、円筒部材５１と筒状部材５４を接合する際には
、高周波電流発生器から誘導コイル５５に高周波電流を
付与し、円筒部材５１と筒状部材５４の間に設けられて
いるリング５３に誘導発熱を起こさせ、その発熱によっ
て熱可塑性樹脂からなる筒状部材５４を加熱・溶融させ
る。そして、この状態で、筒状部材５４の上方から矢印
Ａのごとく荷重を加えて、筒状部材５４の溶融物（図示
せず）をリング５３と円筒部材５１とに絡ませて硬化さ
せる。これによって、円筒部材５１と筒状部材５４とが
接合される。When joining the cylindrical member 51 and the cylindrical member 54, a high frequency current is applied from a high frequency current generator to the induction coil 55, and a high frequency current is applied to the ring 53 provided between the cylindrical member 51 and the cylindrical member 54. Induction heat generation is caused, and the heat generated heats and melts the cylindrical member 54 made of thermoplastic resin. In this state, a load is applied from above the cylindrical member 54 as indicated by arrow A, so that the molten material (not shown) of the cylindrical member 54 is entangled with the ring 53 and the cylindrical member 51 and hardened. Thereby, the cylindrical member 51 and the cylindrical member 54 are joined.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

しかしながら、このようなインブラント接合方法におい
ては、接合しようとする円筒部材５１と筒状部材５４の
周囲を誘導コイル５５で覆う必要があるため、接合部材
の形状に制約があることはもとより、円筒部材５１と筒
状部材５４にあったリング５３を接合の都度組み付けな
ければならず、接合作業が煩雑となる不具合がある。However, in such an implant joining method, since it is necessary to cover the periphery of the cylindrical member 51 and the cylindrical member 54 to be joined with the induction coil 55, there are restrictions on the shape of the joining member, and there are also restrictions on the shape of the cylindrical member 51 and the cylindrical member 54. It is necessary to assemble the ring 53 that fits the member 51 and the cylindrical member 54 each time they are to be joined, resulting in a problem that the joining work becomes complicated.

従って、この発明は、上記の不具合を解消するためにな
されたもので、合成樹脂材料をレーザ光に対して非吸収
性とし、前記異種材料に貫通穴を形成して重ね合わせ、
合成樹脂材料の方向からレーザ光を照射して溶融し、そ
の溶融物を貫通穴に押し出して両材料を接合させること
によって、接合部材の形状に制約をうけることなく、し
かも容易に接合作業を行なうことにある。Therefore, the present invention has been made to solve the above-mentioned problems, and includes making a synthetic resin material non-absorbent to laser light, forming through holes in the different materials, and overlapping them.
By irradiating a laser beam from the direction of the synthetic resin material to melt it, and then extruding the melted material into a through hole to join both materials, the joining work can be easily performed without being restricted by the shape of the joining parts. There is a particular thing.

〔問題点を解決するための手段〕[Means for solving problems]

すなわち、この発明に係る合成樹脂材料と異種材料の接
合方法においては、合成樹脂材料と異種材料とを重ね合
わせ、合成樹脂材料の方向からレーザ光を照射して両材
料を接合するにあたり、前記合成樹脂材料をレーザ光に
対して非吸収性とし、前記異種材料に貫通穴を形成せし
め、この金属材料と合成樹脂材料とを重ね合わせ、この
合成樹脂材料の方向からレーザ光を照射して異種材料を
加熱すると共に、その熱によって合成樹脂材料を加熱・
溶融し、この溶融物を異種材料の貫通孔に押し出すよう
にしたものである。That is, in the method for joining a synthetic resin material and a dissimilar material according to the present invention, the synthetic resin material and the dissimilar material are superimposed and a laser beam is irradiated from the direction of the synthetic resin material to join the two materials. A resin material is made non-absorbent to laser light, a through hole is formed in the different material, this metal material and a synthetic resin material are overlapped, and a laser light is irradiated from the direction of this synthetic resin material to separate the different material. At the same time, the heat heats the synthetic resin material.
The material is melted and the molten material is extruded into a through hole in a different material.

そして、合成樹脂材料としては、熱可塑性樹脂材料が通
しており、例えば、ポリエチレン、ポリプロピレン、ポ
リスチレン、ＡＢＳ樹脂、アクリル系樹脂、酢酸ビニル
系樹脂、塩化ビニル樹脂、塩化ビニリデン樹脂、フッ素
樹脂、ポリエステル樹脂、飽和ポリアミド樹脂、ポリカ
ーボネート樹脂、ポリエーテル樹脂等を挙げることがで
きる。As synthetic resin materials, thermoplastic resin materials are used, such as polyethylene, polypropylene, polystyrene, ABS resin, acrylic resin, vinyl acetate resin, vinyl chloride resin, vinylidene chloride resin, fluororesin, and polyester resin. , saturated polyamide resin, polycarbonate resin, polyether resin, etc.

また、合成樹脂材料と接合される異種材料としては、鉄
、銅、真鍮、ステンレス、ニッケル、アルミニウム等の
金属材料もしくはガラス、セメント等のオールドセラミ
ックスあるいは人工的に合成した窒化ケイ素、炭化ケイ
素等を原料として成形、焼成したニューセラミックスな
どを挙げることができる。In addition, dissimilar materials to be bonded to synthetic resin materials include metal materials such as iron, copper, brass, stainless steel, nickel, and aluminum, old ceramics such as glass and cement, and artificially synthesized silicon nitride and silicon carbide. Examples of raw materials include new ceramics formed and fired.

そして、異種材料に形成される貫通穴としては、溝、穴
等であって、これらは異種材料の表面側から裏面側に向
けてストレートに形成されたもの、表面側から裏面側に
向けて順次縮小するテーパ面に形成したもの、表面側か
ら裏面側に向けて順次拡大するテーパ面を形成したもの
等であり、その形状は特に限定されるものではない。例
えば、穴の場合には円形、長方形、正方形、楕円形、多
角形等に形成することができ、溝の場合には線状、半球
状、台形状等に形成することができる。そして、貫通穴
の大きさは、０．５ｆｌないし１０鶴の範囲が適してお
り、その大きさが０．５　ｔｍ以下では合成樹脂材料の
溶融物を押し出しにくく、必要以上の押し圧力を必要と
し、１０＋ｎ以上では押し出された合成樹脂材料の溶融
物が部分的となり、接合強度が低下する恐れがある。Through-holes formed in dissimilar materials include grooves, holes, etc., which are formed straight from the front side to the back side of the dissimilar material, and those formed sequentially from the front side to the back side of the dissimilar material. It may be formed with a tapered surface that shrinks, or it may be formed with a tapered surface that gradually expands from the front side toward the back side, and the shape is not particularly limited. For example, a hole can be formed in a circular, rectangular, square, elliptical, polygonal, etc. shape, and a groove can be formed in a linear, hemispherical, trapezoidal, etc. shape. The suitable size of the through hole is in the range of 0.5 fl to 10 mm; if the size is less than 0.5 tm, it will be difficult to extrude the molten synthetic resin material, and more pressing force than necessary will be required. , 10+n or more, the extruded synthetic resin material melts only partially, and there is a risk that the bonding strength will decrease.

また、合成樹脂材料の方向から照射されるレーザとして
は、ガラス：ネオジウム３＋レーザ、ＹＡＧ：ネオジウ
ム１“レーザ、ルビーレーザ、ヘリウム−ネオンレーザ
、クリプトンレーザ、アルゴンレーザ、Ｈ，レーザ、Ｎ
２レーザ等を挙げることができる。Lasers irradiated from the direction of the synthetic resin material include glass: neodymium 3+ laser, YAG: neodymium 1" laser, ruby laser, helium-neon laser, krypton laser, argon laser, H, laser, N
2 lasers, etc.

また、レーザの波長としては、異種材料を加熱して、そ
の熱によって合成樹脂材料を溶融せしめる波長が必要で
あり、合成樹脂材料と異種材料のもつ吸収スペクトル特
性によって決まる。例えば、ポリプロピレン樹脂からな
る板部材と金属材料からなる板部材の組み合わせにおい
ては、ＹＡＧ　：ネオジウム３＋レーザの発振波長であ
る１、０６μｍが適している。Further, the wavelength of the laser must be a wavelength that can heat a different material and melt the synthetic resin material with the heat, and is determined by the absorption spectrum characteristics of the synthetic resin material and the different material. For example, in a combination of a plate member made of polypropylene resin and a plate member made of a metal material, the oscillation wavelength of 1.06 μm, which is the oscillation wavelength of a YAG:neodymium 3+ laser, is suitable.

また、レーザの出力においては、異種材料を加熱して、
その熱によって合成樹脂材料を溶融するに十分な出力が
必要であって、最適な条件を適宜選択して決定される。In addition, the laser output heats dissimilar materials,
A sufficient output is required to melt the synthetic resin material with the heat, and the optimum conditions are appropriately selected and determined.

この時、出力が大きすぎると異種材料の加熱のみにとど
まらず、その熱によって合成樹脂材料が参発し、て接合
が困難となるので考慮する必要がある。例えば、ＹＡＧ
　：ネオジウムコ“レーザによる際の目安としては、５
ないし、２５０Ｗ程度が通している。At this time, if the output is too large, not only will the dissimilar materials be heated, but the heat will also cause the synthetic resin material to join, making joining difficult, so this must be taken into account. For example, YAG
：Neodymium Co "As a guideline when using a laser, 5
No, about 250W is passing through it.

〔実施例〕〔Example〕

以下、本発明に係る接合方法の一実施例を図面に基づい
て説明する。Hereinafter, one embodiment of the joining method according to the present invention will be described based on the drawings.

第１図は本発明に係る合成樹脂材料と異種材料の接合方
法を説明する概略断面図である。FIG. 1 is a schematic cross-sectional view illustrating a method of joining a synthetic resin material and different materials according to the present invention.

第１図の（ａ）ないしくｄ）において、１はステンレス
鋼板からなる板部材であって、この板部材１の板厚は２
．０ｆｌに形成されており、その上面は平担に形成され
た接合面１ａとされ、　下面も平担に形成されて台座（
図示せず）等に支持する載置面１ｂとされている。In (a) to d) of FIG. 1, 1 is a plate member made of a stainless steel plate, and the plate member 1 has a thickness of 2.
．． 0 fl, its upper surface is a flat joint surface 1a, and its lower surface is also flat and forms a pedestal (
(not shown), etc., is the mounting surface 1b.

また、天部材１の上部にはポリプロピレン樹脂からなる
板部材２が配設されており、その板厚は４．０ｆｌに形
成されている。そして、この板部材２の上面は平担面２
ａされており、下面は板部材２の上面１ａに当接する接
合面２ｂとされている。Further, a plate member 2 made of polypropylene resin is disposed above the top member 1, and the plate member 2 is formed to have a thickness of 4.0 fl. The upper surface of this plate member 2 is a flat surface 2
a, and the lower surface is a joint surface 2b that comes into contact with the upper surface 1a of the plate member 2.

また、板部材２の原材料は乳白色とされており、１．０
６μｍ以下のレーザ光に対しては非吸収性の性質を有し
ている。In addition, the raw material of the plate member 2 is milky white, and has a 1.0
It has a non-absorbing property for laser light of 6 μm or less.

そして、両部材１．２を接合する際には、第１図の（ａ
）に示すように板部材１の上方にＹＡＧ：ネオジウム１
ル−ザ装置の照射ノズル３を載置させる。この状態で照
射ノズル３から波長が１゜０６μｍで、出力が２００Ｗ
のＹＡＧＬ／−ザ光４を加工レンズ５を通過させて照射
すると共に、ＹＡＧレーザ光４と同軸にアシストガス６
を噴出させる。When joining both members 1.2, (a
), YAG:Neodymium 1 is placed above the plate member 1.
Place the irradiation nozzle 3 of the laser device. In this state, the wavelength is 1°06μm and the output is 200W from the irradiation nozzle 3.
The YAGL/- laser beam 4 is irradiated through a processing lens 5, and an assist gas 6 is emitted coaxially with the YAG laser beam 4.
erupt.

その際、ＹＡＧレーザ光４は、その波長と金属材料の吸
収スペクトルとの関連によって、ステンレス鋼板からな
る板部材１に対して吸収となるため、その照射部位にエ
ネルギとしてＭ積されると共に、そのエネルギによって
板部材１かすみやかに加熱・溶融され、またアシストガ
ス６の噴出にて貫通穴ＩＣが形成される。At this time, the YAG laser beam 4 is absorbed by the plate member 1 made of a stainless steel plate due to the relationship between its wavelength and the absorption spectrum of the metal material, so that the YAG laser beam 4 is multiplied as energy at the irradiation site and is The energy quickly heats and melts the plate member 1, and the assist gas 6 is ejected to form the through hole IC.

そして、この時の貫通穴ＩＣの大きさは、第１図の（ｂ
）に示すように略中央部の直径が３日程度であり、接合
面ｌａ側および載置面１ｂ側にそれぞれが７日程度に形
成され、両面の１ｂ側にそれぞれに拡大する円錐形状と
なっている。The size of the through hole IC at this time is (b) in FIG.
), the diameter of the approximately central part is about 3 days, and the diameter is about 7 days on the bonding surface la side and the mounting surface 1b side, respectively, and it has a conical shape that expands on both sides of the 1b side. ing.

次に、第１図の（ｄ）に示すように板部材１の接合面１
ａに板部材２の接合面２ｂを重ね合わせてセットする。Next, as shown in FIG. 1(d), the joint surface 1 of the plate member 1 is
The bonding surface 2b of the plate member 2 is placed on top of the plate member 2a.

この状態で板部材１に形成されている貫通穴ＩＣに相当
する天部材２の上面にＹＡＧ：ネオジウム３＋レーザ装
置の照射ノズル３を当接させる。その後、照射ノズル３
から波長が１゜０６、ｃｒｍで、出力が２０ＷのＹＡＧ
レーザ光４を加工レンズ５に通過させて照射する。In this state, the irradiation nozzle 3 of the YAG:Neodymium 3+ laser device is brought into contact with the upper surface of the top member 2 corresponding to the through hole IC formed in the plate member 1. After that, irradiation nozzle 3
YAG with a wavelength of 1°06, crm and an output of 20W.
Laser light 4 is passed through processing lens 5 and irradiated.

その際、ＹＡＧレーザ光４は、その波長と合成樹脂材料
の吸収スペクトルとの関連によって、ポリプロピレン樹
脂からなる板部材２に対して非吸収となるため、天部材
２の中を反射および屈折を繰り返しながら透過すると共
に、ステンレスからなる板部材ｌの接合面１ａに達する
。At this time, the YAG laser beam 4 is not absorbed by the plate member 2 made of polypropylene resin due to the relationship between its wavelength and the absorption spectrum of the synthetic resin material, so it is repeatedly reflected and refracted inside the top member 2. As the light passes through, it reaches the joint surface 1a of the plate member 1 made of stainless steel.

そして、板部材１の接合面１ａに達したＹＡＧレーザ光
４は、その部位および周辺でエネルギとして蓄積される
と共に、そのエネルギによって板部材１の接合面１ａが
加熱される。それにともない接合面ｌａの熱がこの板部
材１の接合面１ａに当接している板部材２の接合面２ｂ
に伝達されて加熱・溶融される。The YAG laser beam 4 that has reached the bonding surface 1a of the plate member 1 is accumulated as energy in and around the area, and the bonding surface 1a of the plate member 1 is heated by the energy. Accordingly, the heat of the joint surface la is transferred to the joint surface 2b of the plate member 2 which is in contact with the joint surface 1a of the plate member 1.
and is heated and melted.

その後、ＹＡＧレーザ光４によって板部材１の接合面１
ａを加熱しつつ、照射ノズル３によって矢印Ａ方向から
荷重を加える。その際、天部材２の溶融物２Ｃが下部の
板部材１に形成されている貫通穴ＩＣに押し出される。Thereafter, the joining surface 1 of the plate member 1 is
While heating a, a load is applied from the direction of arrow A using the irradiation nozzle 3. At this time, the melt 2C of the top member 2 is pushed out into the through hole IC formed in the lower plate member 1.

そして、上部の板部材２の溶融物２ｃが貫通穴１ｃに十
分に押し出され、両板部材１．２の接合面１ａ、２ｂが
当接するまでＹＡＧレーザ光４の照射と矢印Ａ方向から
の荷重を継続する。Then, the YAG laser beam 4 is irradiated and the load is applied from the direction of arrow A until the melt 2c of the upper plate member 2 is sufficiently pushed out into the through hole 1c and the joint surfaces 1a and 2b of both plate members 1.2 come into contact. Continue.

そして、上部の板部材２の溶融物２ｃが板部材１の貫通
穴１ｃに十分に押し出され、両板部材１．２の接合面１
ａ、２ｂが十分に当接したところで、ＹＡＧレーザ光４
の照射を停止すると共に、板部材２への矢印Ａ方向から
の荷重を取り除く、その後、照射ノズル４を板部材２か
ら離反させて遠ざける。Then, the melt 2c of the upper plate member 2 is sufficiently pushed out into the through hole 1c of the plate member 1, and the joint surface 1 of both plate members 1.2
When a and 2b are in sufficient contact, the YAG laser beam 4
At the same time, the load on the plate member 2 from the direction of arrow A is removed, and then the irradiation nozzle 4 is moved away from the plate member 2.

これによって、第１図の（ｄ）に示すように板部材１に
形成されている貫通穴ＩＣに板部材２の溶融物２ｃが充
満した状態で硬化し、ステンレスからなる板部材１とポ
リプロピレン樹脂からなる板部材２とが強固に接合され
る。As a result, as shown in FIG. 1(d), the through hole IC formed in the plate member 1 is filled with the melt 2c of the plate member 2, and the plate member 2 is cured, and the plate member 1 made of stainless steel and the polypropylene resin are cured. The plate member 2 consisting of the above is firmly joined.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明に係る合成樹脂材料と異種
材料との接合方法においては、合成樹脂材料をレーザ光
に対して非吸収性とし、前記異種材料に貫通穴を形成し
て重ね合わせ、この合成樹脂材料の方向からレーザ光を
照射して異種材料を加熱し、その熱によって合成樹脂材
料を加熱・溶融すると共に、その溶融物を貫通穴に押し
出して接合するようにしたから、接合しようとする接合
材料の形状に制約することなく、両材料を接合すること
ができる効果がある。As explained above, in the method of joining a synthetic resin material and a dissimilar material according to the present invention, the synthetic resin material is made non-absorbent to laser light, a through hole is formed in the dissimilar material, and the dissimilar materials are overlapped, Laser light is irradiated from the direction of the synthetic resin material to heat the dissimilar materials, and the heat heats and melts the synthetic resin material, and the molten material is pushed out into the through hole to join. This has the effect that both materials can be joined without being restricted in the shape of the joining materials.

また、本発明に係る接合方法においては、接合しようと
する合成樹脂材料の方向からレーザ光を照射して接合す
るようにしたから、両材料の接合作業を容易に実施する
ことができる効果がある。Further, in the joining method according to the present invention, since the joining is performed by irradiating the laser beam from the direction of the synthetic resin materials to be joined, there is an effect that the joining work of both materials can be carried out easily. .

また、本発明に係る接合方法においては、合成樹脂材料
の溶融物を異種材料の貫通穴に押し出して接合するよう
にしたから従来の接合方法に比較して接合強度を著しく
向上させる効果がある。Furthermore, in the joining method according to the present invention, since the molten material of the synthetic resin material is extruded into the through hole of different materials to join them, it has the effect of significantly improving the joining strength compared to the conventional joining method.

【図面の簡単な説明】[Brief explanation of the drawing]

第１ｖｌ！Ｊは本発明に係る接合方法の合成樹脂材料と
異種材料の接合方法を説明する概略断面図である。 第２図は従来のインブラント接合方法を説明する概略断
面図である。 １・−・・・・板部材 ｌａ−一・・−接合面 １ｃ・−・−貫通穴 ２・−−−−一板部材 ２ｂ−−−−−一接合面 ２ｃｍ−・−溶融物 ３−−−−−一照射ノズル ４−・−・−ＹＡＧレーザ光 ５−−−−−一加エレンズ 出願人　　トヨタ自動車株式会社 （Ｃ）　　　　　　　　　　　　　　（ｄン第１図1st vl! J is a schematic cross-sectional view illustrating a method of joining a synthetic resin material and a different material according to the present invention. FIG. 2 is a schematic cross-sectional view illustrating a conventional implant bonding method. 1...Plate member la-1...Jointing surface 1c...-Through hole 2---One plate member 2b---One bonding surface 2cm--Melted material 3- ----Irradiation nozzle 4--YAG laser beam 5-----Irradiation nozzle 4-----Ellens applicant Toyota Motor Corporation (C) (Fig. 1

Claims (1)

【特許請求の範囲】[Claims] 合成樹脂材料と異種材料とを重ね合わせ、合成樹脂材料
の方向からレーザ光を照射して両材料を接合するにあた
り、前記合成樹脂材料をレーザ光に対して非吸収性とし
、前記異種材料に貫通穴を形成せしめ、この金属材料と
合成樹脂材料とを重ね合わせ、この合成樹脂材料の方向
からレーザ光を照射して異種材料を加熱すると共に、そ
の熱によって合成樹脂材料を加熱・溶融し、この溶融物
を異種材料の貫通穴から押し出すようにしたことを特徴
とする合成樹脂材料と異種材料の接合方法。When a synthetic resin material and a dissimilar material are overlapped and a laser beam is irradiated from the direction of the synthetic resin material to bond the two materials, the synthetic resin material is made non-absorbent to the laser beam and the dissimilar material is penetrated. A hole is formed, this metal material and a synthetic resin material are overlapped, and a laser beam is irradiated from the direction of this synthetic resin material to heat the dissimilar material, and the synthetic resin material is heated and melted by the heat, and the synthetic resin material is heated and melted. A method for joining synthetic resin materials and dissimilar materials, characterized in that a molten material is extruded through a through hole in the dissimilar materials.
JP60205764A 1985-09-18 1985-09-18 Joining of synthetic resin material and different material Pending JPS6264528A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60205764A JPS6264528A (en) 1985-09-18 1985-09-18 Joining of synthetic resin material and different material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60205764A JPS6264528A (en) 1985-09-18 1985-09-18 Joining of synthetic resin material and different material

Publications (1)

Publication Number Publication Date
JPS6264528A true JPS6264528A (en) 1987-03-23

Family

ID=16512279

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60205764A Pending JPS6264528A (en) 1985-09-18 1985-09-18 Joining of synthetic resin material and different material

Country Status (1)

Country Link
JP (1) JPS6264528A (en)

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US5351844A (en) * 1993-06-01 1994-10-04 Miner Enterprises, Inc. Elastomeric spring unit
US5397512A (en) * 1993-09-10 1995-03-14 Critikon, Inc. Process for sealing catheter tip to insertion needle
WO2011067014A1 (en) * 2009-12-02 2011-06-09 Robert Bosch Gmbh Connection between a first component and a second component
CN102431173A (en) * 2011-11-30 2012-05-02 杨政委 Extrusion device
US8759710B2 (en) 2005-11-21 2014-06-24 Lpkf Laser & Electronics Ag Process and device for form locked joining of two components
JP2014159133A (en) * 2013-02-20 2014-09-04 Asahi Kasei Chemicals Corp Bonding method
JP2015100847A (en) * 2013-11-26 2015-06-04 現代自動車株式会社 Device and method for adhering different kinds of materials
US20150280767A1 (en) * 2014-03-31 2015-10-01 Apple Inc. Laser welding of transparent and opaque materials
WO2016027776A1 (en) * 2014-08-22 2016-02-25 オムロン株式会社 Bonding structure manufacturing method and bonding structure
KR20170020496A (en) * 2014-08-22 2017-02-22 오므론 가부시키가이샤 Production method for bonded structure, and bonded structure
US10200516B2 (en) 2014-08-28 2019-02-05 Apple Inc. Interlocking ceramic and optical members
JP2019511398A (en) * 2016-03-23 2019-04-25 フラウンホーファー−ゲゼルシャフト ツゥア フェアデルング デア アンゲヴァンドテン フォァシュング エー．ファウ． At least one metallic or ceramic component having material continuity or having material continuity and shape compatibility, and a component formed of a thermoplastic polymer or formed of a thermoplastic polymer Apparatus and method for establishing or disconnecting
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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5351844A (en) * 1993-06-01 1994-10-04 Miner Enterprises, Inc. Elastomeric spring unit
US5397512A (en) * 1993-09-10 1995-03-14 Critikon, Inc. Process for sealing catheter tip to insertion needle
US8759710B2 (en) 2005-11-21 2014-06-24 Lpkf Laser & Electronics Ag Process and device for form locked joining of two components
WO2011067014A1 (en) * 2009-12-02 2011-06-09 Robert Bosch Gmbh Connection between a first component and a second component
CN102431173A (en) * 2011-11-30 2012-05-02 杨政委 Extrusion device
JP2014159133A (en) * 2013-02-20 2014-09-04 Asahi Kasei Chemicals Corp Bonding method
JP2015100847A (en) * 2013-11-26 2015-06-04 現代自動車株式会社 Device and method for adhering different kinds of materials
US20150280767A1 (en) * 2014-03-31 2015-10-01 Apple Inc. Laser welding of transparent and opaque materials
US9787345B2 (en) * 2014-03-31 2017-10-10 Apple Inc. Laser welding of transparent and opaque materials
KR20170020496A (en) * 2014-08-22 2017-02-22 오므론 가부시키가이샤 Production method for bonded structure, and bonded structure
JP2016043561A (en) * 2014-08-22 2016-04-04 オムロン株式会社 Manufacturing method of joint structure, and joint structure
KR20170020495A (en) * 2014-08-22 2017-02-22 오므론 가부시키가이샤 Bonding structure manufacturing method and bonding structure
CN106536169A (en) * 2014-08-22 2017-03-22 欧姆龙株式会社 Bonding structure manufacturing method and bonding structure
US20170210058A1 (en) * 2014-08-22 2017-07-27 Omron Corporation Manufacturing method of bonding structure and bonding structure
WO2016027776A1 (en) * 2014-08-22 2016-02-25 オムロン株式会社 Bonding structure manufacturing method and bonding structure
EP3184283A4 (en) * 2014-08-22 2018-04-18 Omron Corporation Bonding structure manufacturing method and bonding structure
US10471660B2 (en) 2014-08-22 2019-11-12 Omron Corporation Manufacturing method of bonding structure and bonding structure
TWI704994B (en) * 2014-08-22 2020-09-21 日商歐姆龍股份有限公司 Method for manufacturing joint structure and joint structure
US10200516B2 (en) 2014-08-28 2019-02-05 Apple Inc. Interlocking ceramic and optical members
JP2019511398A (en) * 2016-03-23 2019-04-25 フラウンホーファー−ゲゼルシャフト ツゥア フェアデルング デア アンゲヴァンドテン フォァシュング エー．ファウ． At least one metallic or ceramic component having material continuity or having material continuity and shape compatibility, and a component formed of a thermoplastic polymer or formed of a thermoplastic polymer Apparatus and method for establishing or disconnecting
US11660824B2 (en) 2016-03-23 2023-05-30 Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. Apparatus and method for establishing or for separating a connection having material continuity or having material continuity and shape matching of at least one metal or ceramic component and of a component formed from or by a thermoplastic polymer
EP3695932A4 (en) * 2017-10-12 2020-11-25 LG Chem, Ltd. Method for producing a bonded body of different materials

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