JP2018058279A - Production method of resin-metal joined article and resin-metal joined article - Google Patents

Production method of resin-metal joined article and resin-metal joined article Download PDF

Info

Publication number
JP2018058279A
JP2018058279A JP2016197812A JP2016197812A JP2018058279A JP 2018058279 A JP2018058279 A JP 2018058279A JP 2016197812 A JP2016197812 A JP 2016197812A JP 2016197812 A JP2016197812 A JP 2016197812A JP 2018058279 A JP2018058279 A JP 2018058279A
Authority
JP
Japan
Prior art keywords
resin
aluminum material
array
joining
nanospike
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
Application number
JP2016197812A
Other languages
Japanese (ja)
Other versions
JP6809680B2 (en
Inventor
厚志 細井
Atsushi Hosoi
厚志 細井
宏之 川田
Hiroyuki Kawada
宏之 川田
暉 阿部
Hikaru Abe
暉 阿部
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.)
Waseda University
Original Assignee
Waseda University
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 Waseda University filed Critical Waseda University
Priority to JP2016197812A priority Critical patent/JP6809680B2/en
Publication of JP2018058279A publication Critical patent/JP2018058279A/en
Application granted granted Critical
Publication of JP6809680B2 publication Critical patent/JP6809680B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/44Joining a heated non plastics element to a plastics element
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/026Chemical pre-treatments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/303Particular design of joint configurations the joint involving an anchoring effect
    • B29C66/3032Particular 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
    • B29C66/30321Particular 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 protrusions belonging to at least one of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/349Cooling the welding zone on the welding spot
    • B29C66/3494Cooling the welding zone on the welding spot while keeping the welding zone under pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General 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
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7212Fibre-reinforced materials characterised by the composition of the fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7394General 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 thermoset
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/74Joining plastics material to non-plastics material
    • B29C66/742Joining plastics material to non-plastics material to metals or their alloys
    • B29C66/7422Aluminium or alloys of aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/90Measuring or controlling the joining process
    • B29C66/91Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
    • B29C66/919Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
    • B29C66/9192Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
    • B29C66/91921Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature
    • B29C66/91941Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to Tg, i.e. the glass transition temperature, of the material of one of the parts to be joined
    • B29C66/91945Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to Tg, i.e. the glass transition temperature, of the material of one of the parts to be joined lower than said glass transition temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

PROBLEM TO BE SOLVED: To obtain sufficient joining strength without using joining members such as bolts and rivets or adhesives when joining various resins and aluminum materials.SOLUTION: The method of manufacturing a resin-metal joined article 10 according to the present invention is to sequentially carry out a nano spike array fabricating step of fabricating a nano spike array 13 consisting of plural acicular protrusions 13A protruding on the surface of an aluminum material 11, a silane coupling treatment step of carrying out the silane coupling treatment on the surface of the aluminum material 11 where the nano spike array 13 is formed, and a joining step of joining the aluminum material 11 and a resin 21 by solidifying the resin 21 in molten state after entering a gap S formed between the respective protrusions 13A.SELECTED DRAWING: Figure 2

Description

本発明は、樹脂金属接合体の製造方法及び樹脂金属接合体に係り、特に、ボルトやリベット等の接合部材を用いることなく、熱可塑性若しくは熱硬化性の炭素繊維強化樹脂とアルミニウム材とを接合する樹脂金属接合体の製造方法及び樹脂金属接合体に関する。   The present invention relates to a method for producing a resin-metal bonded body and a resin-metal bonded body, and in particular, bonds a thermoplastic or thermosetting carbon fiber reinforced resin and an aluminum material without using a bonding member such as a bolt or a rivet. The present invention relates to a method for producing a resin-metal bonded body and a resin-metal bonded body.

炭素繊維と樹脂の複合材として炭素繊維強化プラスチック(CFRP)が知られており、このCFRPとしては、母材に熱硬化性樹脂を用いた熱硬化性のCFRPの他に、母材に熱可塑性樹脂を用いた熱可塑性炭素繊維強化プラスチック(CFRTP)がある。これらCFRPは、軽量且つ高強度であるため、航空機や自動車等の部品として広く用いられている。特に、自動車分野では、適材適所に種々の材料を採用するマルチマテリアル化がなされる傾向があり、成形性の観点から熱可塑性樹脂を母材としたCFRTPが用いられている。当該CFRTPは、保管や量産性に優れており、後加工も容易でリサイクル可能等の理由から、製造コストが安価となる。   Carbon fiber reinforced plastic (CFRP) is known as a composite material of carbon fiber and resin. As CFRP, in addition to thermosetting CFRP using a thermosetting resin as a base material, a thermoplastic material is used as a base material. There is a thermoplastic carbon fiber reinforced plastic (CFRTP) using a resin. Since these CFRPs are lightweight and have high strength, they are widely used as parts for aircrafts and automobiles. In particular, in the automobile field, there is a tendency to adopt multi-materials by adopting various materials at appropriate positions, and CFRTP using a thermoplastic resin as a base material is used from the viewpoint of moldability. The CFRTP is excellent in storage and mass productivity, is easy to post-process and can be recycled, and the manufacturing cost is low.

これらCFRPが航空機や自動車等の部品の材料として用いられる際には、金属材料からなる他の部品との接合が必要になる。例えば、航空機では、CFRP製の部品とアルミニウム製の部品との接合に、ボルトやリベット等の接合部材が多く用いられる。しかしながら、このような接合部材を用いた接合は、ボルトやリベット自体の重量が嵩み、CFRPを用いることによる軽量化のメリットを阻害する要因となるばかりか、ボルト孔が損傷発生の起点となり易く、近年では、これらCFRP等の樹脂とアルミニウム材の接合をボルトレス化することが求められている。   When these CFRPs are used as materials for parts such as aircraft and automobiles, it is necessary to join with other parts made of a metal material. For example, in an aircraft, a joining member such as a bolt or a rivet is often used for joining a CFRP part and an aluminum part. However, joining using such a joining member not only increases the weight of the bolt or rivet itself, but hinders the advantages of weight reduction by using CFRP, and the bolt hole tends to be a starting point of damage occurrence. In recent years, there has been a demand for boltless bonding between the resin such as CFRP and the aluminum material.

ところで、特許文献1〜3には、ボルトやリベット等の接合部材を用いずに、CFRPと金属とを接合する様々な手法が開示されている。すなわち、特許文献1には、金属表面にナノメートルオーダの微細凹凸を設けた上で、当該金属表面とCFRPとをエポキシ系接着剤を用いて接着する方法が開示されている。また、特許文献2には、金属表面にトリアジンチオール誘導体を含有する層を形成した上で、当該層とCFRP間に熱可塑性樹脂層を更に設け、熱可塑性樹脂層を溶融させることで、金属とCFRPを接合する方法が開示されている。更に、特許文献3には、1000〜100000本の単繊維を含有する短冊状の繊維束からなる炭素繊維を40〜80重量%含有した熱可塑性樹脂と、接合面の面粗度が1〜100μmとなる金属とを振動溶着する方法が開示されている。   By the way, Patent Documents 1 to 3 disclose various methods for joining CFRP and metal without using a joining member such as a bolt or a rivet. That is, Patent Document 1 discloses a method in which fine unevenness of nanometer order is provided on a metal surface, and then the metal surface and CFRP are bonded using an epoxy adhesive. In Patent Document 2, a layer containing a triazine thiol derivative is formed on the metal surface, a thermoplastic resin layer is further provided between the layer and the CFRP, and the thermoplastic resin layer is melted so that the metal and A method for bonding CFRP is disclosed. Furthermore, in Patent Document 3, a thermoplastic resin containing 40 to 80% by weight of carbon fibers made of strip-like fiber bundles containing 1000 to 100,000 single fibers, and a surface roughness of the joining surface of 1 to 100 μm. A method of vibration welding with a metal to be obtained is disclosed.

特開2010−269534号公報JP 2010-269534 A 国際公開WO2012/074083号公報International Publication WO2012 / 074083 特開2016−34734号公報JP 2016-34734 A

しかしながら、前記特許文献1の方法にあっては、接着剤としてエポキシ樹脂が必要になることから、接着剤の硬化に時間がかかるばかりか、接着剤の経年劣化による接着強度の低下を招来するとともに、当該接着剤の存在によりリサイクル性が低下するという問題がある。また、前記特許文献2の方法にあっては、接合対象の金属とCFRPとの間に、リアジンチオール誘導体層及び熱可塑性樹脂層が介在することになるため、金属とCFRPの接合体の高重量化を招来するとともに、特許文献1と同様にリサイクル性が低下するという問題がある。更に、前記特許文献3の方法にあっては、使用できる炭素繊維複合材料が限られており、広い種類のCFRPに適用することができない。   However, since the method of Patent Document 1 requires an epoxy resin as an adhesive, it takes time to cure the adhesive, and also causes a decrease in adhesive strength due to aging of the adhesive. There exists a problem that recyclability falls by presence of the said adhesive agent. Further, in the method of Patent Document 2, since the lyazine thiol derivative layer and the thermoplastic resin layer are interposed between the metal to be joined and CFRP, the height of the joined body of the metal and CFRP is high. In addition to incurring weight, there is a problem that the recyclability is reduced as in Patent Document 1. Furthermore, in the method of Patent Document 3, usable carbon fiber composite materials are limited, and cannot be applied to a wide variety of CFRP.

なお、前記特許文献1の背景技術として、アルミニウム合金をエッチングすることで、アルミニウム合金の表面に凹凸を形成してから、当該凹部に溶融した熱可塑性樹脂を高圧で射出して侵入させることで、当該熱可塑性樹脂とアルミニウム合金を接合する方法が開示されている。しかしながら、この方法では、前記凹部の形状から凹部に樹脂を十分侵入させるために射出成形が前提であり、複雑な形状の樹脂と金属との接合が困難になる。また、前記凹部の形状がある一定の領域に延びるなだらかな谷状になるため、当該凹部に樹脂が係合するスパイク効果が不十分となり得る。従って、特許文献1で提案されているように、この背景技術の手法のみでは十分な接着強度が得られず、接着剤を併用する必要性が生じる。   In addition, as a background art of the above-mentioned Patent Document 1, by etching the aluminum alloy, after forming irregularities on the surface of the aluminum alloy, by injecting and injecting the molten thermoplastic resin into the concave portion at a high pressure, A method for joining the thermoplastic resin and the aluminum alloy is disclosed. However, this method is premised on injection molding in order to allow the resin to sufficiently enter the recess from the shape of the recess, and it becomes difficult to join the resin and metal having a complicated shape. In addition, since the concave portion has a gentle valley shape extending to a certain region, the spike effect that the resin engages with the concave portion may be insufficient. Therefore, as proposed in Patent Document 1, sufficient adhesion strength cannot be obtained only by this background art method, and it is necessary to use an adhesive in combination.

また、前記特許文献2の背景技術として、微小なポーラスが表面に形成されたアルミニウム材に樹脂を射出することにより、ポーラス内に樹脂が入り込んで固化するアンカー効果によりCFRTPとアルミニウム材とを接合する方法が開示されている。この方法にあっても、射出成形が前提であることから、複雑な形状の樹脂と金属との接合が困難である他、ポーラスの奥まで樹脂が行き渡り難く、十分なアンカー効果が得られ難い。   Further, as a background art of Patent Document 2, the CFRTP and the aluminum material are joined to each other by an anchor effect in which the resin enters into the porous body and solidifies by injecting the resin into the aluminum material having a minute porous formed on the surface. A method is disclosed. Even in this method, since injection molding is premised, it is difficult to join a resin having a complicated shape and a metal, and it is difficult for the resin to reach the back of the porous body, and it is difficult to obtain a sufficient anchor effect.

本発明は、このような課題を解決するために案出されたものであり、その目的は、様々な樹脂とアルミニウム材とを接合する際に、ボルトやリベット等の接合部材や接着剤を用いることなく、十分な接合強度が得られる樹脂金属接合体の製造方法及び樹脂金属接合体を提供することにある。   The present invention has been devised in order to solve such problems, and its purpose is to use a bonding member such as a bolt or a rivet or an adhesive when bonding various resins and aluminum materials. It is providing the manufacturing method of a resin metal joined body and resin metal joined body from which sufficient joint strength is obtained without it.

前記目的を達成するため、主として、本発明は、樹脂とアルミニウム材を接合してなる樹脂金属接合体の製造方法において、前記アルミニウム材の表面に多数突出する針状の突起からなるナノスパイクアレイを作製するナノスパイクアレイ作製工程と、前記各突起の間に形成された隙間に溶融状態の前記樹脂を侵入させてから固化することで、前記アルミニウム材と前記樹脂を接合する接合工程とを順に行う、という手法を採っている。   In order to achieve the above-mentioned object, the present invention mainly provides a nano-spike array comprising needle-like protrusions protruding on the surface of the aluminum material in a method for producing a resin-metal bonded body obtained by bonding a resin and an aluminum material. The nano spike array manufacturing process to be manufactured and the bonding process of bonding the aluminum material and the resin by sequentially injecting the molten resin into the gap formed between the protrusions and solidifying the resin are sequentially performed. , Is adopted.

また、本発明は、樹脂とアルミニウム材の接合体において、前記樹脂に接合する前記アルミニウム材の接合部分には、平面視で多数散在する錐体状の突起が形成され、当該各突起の間に前記樹脂が入り込むことで、前記樹脂と前記アルミニウム材とが噛み合った状態で接合している、という構成を採っている。   Further, according to the present invention, in the joined body of resin and aluminum material, a large number of cone-shaped projections scattered in a plan view are formed at a joined portion of the aluminum material joined to the resin, and the gaps between the projections are formed. A configuration is adopted in which the resin and the aluminum material are joined in a state of being engaged with each other when the resin enters.

本発明では、樹脂との接合部分となるアルミニウム材の表面に多数突出する針状の突起からなるナノスパイクアレイが形成され、各突起の間の隙間に溶融の樹脂を侵入させて固化することで、樹脂とアルミニウム材とが接合される。この際、突起の先端が尖っているため、樹脂とアルミニウム材との接合状態において、その突起を、樹脂の接合部分側から内部に向かって深く食い込んだ状態にすることができ、高いスパイク効果を得ることができる。また、突起の外周面が急峻になることから、その先端側から当該外周面に流れ込んだ樹脂が基部側に達し易くなり、前記隙間の奥まで樹脂を行き渡らせることができ、高いアンカー効果を得ることができる。これにより、本発明によれば、ボルトやリベット等の接合部材や接着剤を用いることなく、強固に接合された樹脂とアルミニウム材との接合体を得ることができる。加えて、本発明に係る製造方法は、射出成形が必須ではなく、熱可塑性樹脂熱及び硬化性樹脂の何れにも適用することができ、様々な樹脂をアルミニウム材に接合することが可能になる。   In the present invention, a nanospike array consisting of many needle-like protrusions protruding on the surface of the aluminum material to be a joint portion with the resin is formed, and the molten resin is intruded into the gaps between the protrusions to solidify. The resin and the aluminum material are joined. At this time, since the tip of the protrusion is sharp, in the bonded state of the resin and the aluminum material, the protrusion can be deeply cut in from the bonded portion side of the resin to the inside, and a high spike effect is achieved. Can be obtained. In addition, since the outer peripheral surface of the protrusion is steep, the resin that has flowed into the outer peripheral surface from the distal end side can easily reach the base side, and the resin can be spread to the back of the gap to obtain a high anchor effect. be able to. Thereby, according to this invention, the joined body of resin and aluminum material joined firmly can be obtained, without using joining members and adhesives, such as a volt | bolt and a rivet. In addition, the manufacturing method according to the present invention does not require injection molding, and can be applied to both thermoplastic resin heat and curable resin, and can bond various resins to an aluminum material. .

(A)本実施形態に係る樹脂金属接合体の製造方法での陽極酸化処理を経たアルミニウム材の状態を模式的に表した断面図であり、(B)は、(A)の状態からエッチング処理を経たアルミニウム材の状態を示す模式的に表した断面図である。(A) It is sectional drawing which represented typically the state of the aluminum material which passed through the anodizing process in the manufacturing method of the resin metal joined body which concerns on this embodiment, (B) is an etching process from the state of (A). It is sectional drawing which represented typically the state of the aluminum material which passed through. (A)、(B)は、本実施形態に係る樹脂金属接合体の製造方法での接合工程を順に模式的に表した断面図である。(A), (B) is sectional drawing which represented typically the joining process in the manufacturing method of the resin metal joined body which concerns on this embodiment in order.

本発明の詳細と実施例について、適宜図面を使用しながら以下に説明する。   Details and examples of the present invention will be described below with appropriate drawings.

本発明に係る製造方法は、樹脂とアルミニウム材との接合方法に特徴を有する樹脂金属接合体の製造方法である。当該製造方法は、前記樹脂との接合部分となるアルミニウム材の表面に多数突出する針状の突起からなるナノスパイクアレイを作製するナノスパイクアレイ作製工程と、ナノスパイクアレイが形成されたアルミニウム材の表面にシランカップリング処理を行うシランカップリング処理工程と、シランカップリング処理後のアルミニウム材の表面を樹脂の接合部分に接合する接合工程とが順に行われる。   The manufacturing method which concerns on this invention is a manufacturing method of the resin metal joined body characterized by the joining method of resin and an aluminum material. The manufacturing method includes a nanospike array manufacturing step of manufacturing a nanospike array composed of a plurality of needle-like protrusions protruding on the surface of an aluminum material to be a joint portion with the resin, and an aluminum material on which the nanospike array is formed. A silane coupling treatment step for performing a silane coupling treatment on the surface and a joining step for joining the surface of the aluminum material after the silane coupling treatment to the joining portion of the resin are sequentially performed.

本発明においては、前記樹脂として、炭素繊維強化プラスチック(CFRP)等に適用可能であり、当該CFRPとして、母材に熱可塑性樹脂を用いた熱可塑性炭素繊維強化プラスチック(CFRTP)と、母材に熱硬化性樹脂が用いられた熱硬化性のCFRPとの双方の適用が可能である。なお、CFRTPとしては、母材樹脂としてポリアミド(PA6、PA66、PA12等)の他に、ポリプロピレン、ポリカーボネート、ポリオキシメチレン、ポリフェニレンスルフィド、ポリフェニレンエーテル、変性ポリフェニレンエーテル、ポリエチレンテレフタレート、ポリブチレンテレフタレート、ポリエチレンナフタレート、ポリエチレン、ポリスチレン、ポリメチルメタクリレート、ポリエーテルエーテルケトン、ポリエーテルイミド、ポリアミドイミド、エポキシ、AS樹脂、ABS樹脂等が用いられたもの等、様々な種類のものを適用できる。   In the present invention, the resin can be applied to a carbon fiber reinforced plastic (CFRP) or the like. As the CFRP, a thermoplastic carbon fiber reinforced plastic (CFRTP) using a thermoplastic resin as a base material, and a base material. Both application with thermosetting CFRP using a thermosetting resin is possible. As CFRTP, in addition to polyamide (PA6, PA66, PA12, etc.) as a base resin, polypropylene, polycarbonate, polyoxymethylene, polyphenylene sulfide, polyphenylene ether, modified polyphenylene ether, polyethylene terephthalate, polybutylene terephthalate, polyethylene naphthalate. Various types of materials such as those using phthalate, polyethylene, polystyrene, polymethyl methacrylate, polyether ether ketone, polyether imide, polyamide imide, epoxy, AS resin, ABS resin, and the like can be used.

また、本発明においては、前記アルミニウム材として、純アルミニウムの他に、アルミニウムを主成分としたアルミニウム合金の適用が可能である。   In the present invention, as the aluminum material, in addition to pure aluminum, an aluminum alloy containing aluminum as a main component can be applied.

前記ナノスパイクアレイ作製工程では、脱脂したアルミニウム材を酸性の電解液中で陽極酸化することにより、図1(A)に示されるように、アルミニウム材11の表面に多孔性酸化被膜であるポーラスアルミナ層12を形成する陽極酸化処理と、陽極酸化処理で形成された多数のポーラスを有するポーラスアルミナ層12を除去するエッチング処理とが順に行われる。   In the nano spike array manufacturing step, the degreased aluminum material is anodized in an acidic electrolytic solution, so that porous alumina is formed on the surface of the aluminum material 11 as shown in FIG. An anodizing process for forming the layer 12 and an etching process for removing the porous alumina layer 12 having a large number of porous layers formed by the anodizing process are sequentially performed.

前記陽極酸化処理は、金属を陽極として電解液中で通電して当該金属の表面に酸化皮膜を形成する公知の手法が採用され、電解液としては、例えば、クエン酸、硫酸、シュウ酸、リン酸、スルファミン酸、ホウ酸、クロム酸、マロン酸、セレン酸等を含むものが用いられる。   The anodizing treatment employs a known method of forming an oxide film on the surface of the metal by energizing in the electrolytic solution with the metal as the anode. Examples of the electrolytic solution include citric acid, sulfuric acid, oxalic acid, phosphorus Those containing acid, sulfamic acid, boric acid, chromic acid, malonic acid, selenic acid and the like are used.

前記エッチング処理では、リン酸、クロム酸、シュウ酸等の少なくとも1種類を含む酸性の処理液に、ポーラスアルミナ層12を含むアルミニウム材11の部分を浸漬してポーラスアルミナ層12を除去することで、図1(B)に示されるように、その後のアルミニウム材11の新たな表面に残されたナノスパイクアレイ13が表出することになる。このナノスパイクアレイ13は、前記表面上を突出する先端の尖った針状の突起13Aが平面視で多数散在する華道用剣山のような形状をなす。これら突起13Aは、その基部側からほぼ点状をなす先端側に向かって次第に窄まる錐体状となっている。ここで形成されたナノスパイクアレイ13は、樹脂と接合するアルミニウム材11の接合部分11Aとなる。   In the etching process, the porous alumina layer 12 is removed by immersing a portion of the aluminum material 11 including the porous alumina layer 12 in an acidic processing solution containing at least one of phosphoric acid, chromic acid, oxalic acid, and the like. As shown in FIG. 1B, the nanospike array 13 left on the new surface of the aluminum material 11 thereafter appears. This nano spike array 13 has a shape like a sword mountain for flower arrangement in which many needle-like protrusions 13A protruding on the surface are scattered in a plan view. These protrusions 13A have a conical shape that gradually narrows from the base side toward the distal end side that is substantially dotted. The nano spike array 13 formed here becomes a joining portion 11A of the aluminum material 11 to be joined to the resin.

前記シランカップリング処理工程では、ナノスパイクアレイ13が形成されたアルミニウム材11を樹脂により強固に接合するために、ナノスパイクアレイ13の部分にシランカップリング剤が塗布される。ここで用いられるシランカップリング剤としては、主として、イソシアネート基を有するものが用いられるが、本発明はこれに限らず、アミノ基、メルカプト基、チオール基、ジスルフィド基、シアノ基、ハロゲン基、スルフォン基を有するものを用いることもできる。   In the silane coupling process, a silane coupling agent is applied to the nanospike array 13 in order to firmly bond the aluminum material 11 on which the nanospike array 13 is formed with a resin. As the silane coupling agent used here, one having an isocyanate group is mainly used, but the present invention is not limited to this, and an amino group, mercapto group, thiol group, disulfide group, cyano group, halogen group, sulfone is used. Those having a group can also be used.

前記接合工程では、前記樹脂が熱可塑性のCFRTPである場合、図2(A)に示されるように、加熱によって溶融状態となった樹脂21の接合部分21Aとアルミニウム材11の接合部分11Aとを相互に接近する方向に押圧するホットプレス処理により、各接合部分11A,21A同士が接合される。具体的に、ここでのホットプレス処理は、シランカップリング剤が接合部分11Aに塗布されたアルミニウム材11をホットプレートH等に載置する等によって加熱し、その接合部分11Aに樹脂21の接合部分21Aを重ね合わせて樹脂21を溶融させた上で、樹脂21をアルミニウム材11に向かって加圧したまま、樹脂21を冷却して固化させることで、アルミニウム材11と樹脂21とが接合される。なお、ホットプレス処理の温度条件としては、母材樹脂の種類によって異なり、ガラス転移温度以上で、所望とする形状を維持可能な温度未満に設定される。   In the joining step, when the resin is thermoplastic CFRTP, as shown in FIG. 2 (A), the joining portion 21A of the resin 21 that has been melted by heating and the joining portion 11A of the aluminum material 11 are combined. The joining portions 11A and 21A are joined to each other by a hot press process of pressing in directions approaching each other. Specifically, in this hot press treatment, the aluminum material 11 having the silane coupling agent applied to the joining portion 11A is heated by being placed on a hot plate H or the like, and the resin 21 is joined to the joining portion 11A. After the portions 21A are overlapped and the resin 21 is melted, the resin 21 is cooled and solidified while the resin 21 is pressurized toward the aluminum material 11, whereby the aluminum material 11 and the resin 21 are joined. The The temperature condition for the hot press treatment varies depending on the type of the base resin, and is set to a temperature equal to or higher than the glass transition temperature and lower than a temperature at which a desired shape can be maintained.

また、前記樹脂21が熱硬化性のCFRPの場合、当該樹脂21を成形する際に、その接合部分21Aにアルミニウム材11の接合部分11Aを重ね合わせた状態で行われる。例えば、半硬化状態のプリプレグシートを使い、オートクレーブ等によって加圧しながら硬化させる過程で、アルミニウム材11を樹脂21に接合させる。   Further, when the resin 21 is a thermosetting CFRP, when the resin 21 is molded, the bonding portion 11A of the aluminum material 11 is superposed on the bonding portion 21A. For example, the aluminum material 11 is joined to the resin 21 in the process of curing while applying pressure by an autoclave or the like using a semi-cured prepreg sheet.

以上の接合工程においては、アルミニウム材11の接合部分11Aがナノスパイクアレイ13となっているため、当該接合部分11Aが樹脂21側に突き刺さるように強固に接合され、スパイク効果を高めることができる。また、溶融状態の樹脂12が各突起13Aの間に形成される隙間Sに侵入する際に、各突起13Aの先端側がほぼ点状となっており、当該先端間の樹脂入口部分を広く確保できるとともに、隙間Sの深部に向かって隣り合う突起13Aの離間距離が次第に狭くなるため、突起S内への樹脂21の流入を効率的且つ十分に行うことができ、アンカー効果をも高めることができる。   In the above joining process, since the joining portion 11A of the aluminum material 11 is the nano spike array 13, the joining portion 11A is firmly joined so as to pierce the resin 21 side, and the spike effect can be enhanced. Further, when the molten resin 12 enters the gap S formed between the projections 13A, the tip side of each projection 13A is substantially point-like, and a wide resin inlet portion between the tips can be secured. At the same time, the separation distance between the adjacent protrusions 13A toward the deep part of the gap S is gradually reduced, so that the resin 21 can be efficiently and sufficiently introduced into the protrusion S, and the anchor effect can be enhanced. .

前記製造方法で得られた樹脂金属接合体10は、図2(B)に示されるように、アルミニウム材11の接合部分11Aに、平面視で多数散在する先端が尖った針状の突起13Aが形成され、それぞれ隣り合う各突起13Aの間に樹脂21が入り込んで、アルミニウム材11と樹脂21とが噛み合って接合した状態となる。   As shown in FIG. 2 (B), the resin-metal bonded body 10 obtained by the above manufacturing method has a needle-like protrusion 13A having a sharp point on the bonding portion 11A of the aluminum material 11 scattered in a plan view. The resin 21 enters between the adjacent protrusions 13A, and the aluminum material 11 and the resin 21 are engaged and joined.

なお、本発明においては、前記シランカップリング処理工程を省略して、前記ナノスパイクアレイ作製工程の後に前記接合工程に移行しても良いが、シランカップリング処理工程を経た方が、アルミニウム材11と樹脂21との接合強度を高めることができる。   In the present invention, the silane coupling treatment step may be omitted and the nanospike array production step may be followed by the joining step. However, the aluminum material 11 is more easily subjected to the silane coupling treatment step. The bonding strength between the resin 21 and the resin 21 can be increased.

次に、樹脂金属接合体10の製造方法に係る一実施例について説明する。   Next, an example according to the method for manufacturing the resin-metal bonded body 10 will be described.

アルミニウム材11としては、A1050のアルミニウム材からなる板材を用い、樹脂21としては、母材をポリアミド(PA6)として炭素繊維と複合させた熱可塑性のCFRTPからなる板材を用い、次の手順により、アルミニウム材11と樹脂21の接合体10が得られた。   As the aluminum material 11, a plate material made of aluminum material of A1050 is used, and as the resin 21, a plate material made of thermoplastic CFRTP in which the base material is combined with carbon fiber as polyamide (PA6) is used. A joined body 10 of the aluminum material 11 and the resin 21 was obtained.

先ず、ナノスパイクアレイ作製工程により、アルミニウム材11の表面にナノスパイクアレイ13を形成する。すなわち、ここでは、最初に、アルミニウム合金に対して脱脂等の前処理を行う。ここでの脱脂は、アセトン中にアルミニウム材を浸し、超音波洗浄により行われるが、この前処理として、アルミニウム材11の表面酸化膜を無機材で完全にエッチングする処理を行うこともでき、その後、以降の処理を行うことで、より効果的なナノスパイクアレイ13の作製が可能になると考えられる。その上で、アルミニウム材11の陽極酸化処理が行われる。ここでの電解液としては、2重量%のクエン酸、2重量%のエチレングリコールを含むものが用いられる。また、印加電圧を400V、電流密度を1.2mA/cmとし、電解液を冷却する冷却水の温度を0℃とし、通電時間を9時間とした。すると、アルミニウム材11の表面に、図1(A)に模式的に示されるポーラスアルミナ層12が形成された。次に、ポーラスアルミナ層12を除去するためのエッチング処理が行われる。ここでは、処理液として、2重量%のリン酸、1.5重量%のクロム酸を含むものが用いられ、温度63℃で60分間行われる。すると、図1(B)に模式的に示される針状の突起13Aを多数有するナノスパイクアレイ13が、アルミニウム材11の表面に多数残され、このナノスパイクアレイ13が樹脂21に接合される接合部分11Aとなる。 First, the nano spike array 13 is formed on the surface of the aluminum material 11 by the nano spike array manufacturing process. That is, here, first, pretreatment such as degreasing is performed on the aluminum alloy. The degreasing here is performed by immersing an aluminum material in acetone and performing ultrasonic cleaning. However, as this pretreatment, a treatment of completely etching the surface oxide film of the aluminum material 11 with an inorganic material can be performed. Thus, it is considered that the nano spike array 13 can be more effectively manufactured by performing the subsequent processing. Then, anodizing treatment of the aluminum material 11 is performed. As the electrolytic solution here, one containing 2 wt% citric acid and 2 wt% ethylene glycol is used. The applied voltage was 400 V, the current density was 1.2 mA / cm 2 , the temperature of the cooling water for cooling the electrolyte was 0 ° C., and the energization time was 9 hours. Then, a porous alumina layer 12 schematically shown in FIG. 1A was formed on the surface of the aluminum material 11. Next, an etching process for removing the porous alumina layer 12 is performed. Here, a treatment solution containing 2% by weight phosphoric acid and 1.5% by weight chromic acid is used, and the treatment is performed at a temperature of 63 ° C. for 60 minutes. Then, a large number of nanospike arrays 13 having a large number of needle-like protrusions 13A schematically shown in FIG. 1B are left on the surface of the aluminum material 11, and the nanospike array 13 is bonded to the resin 21. It becomes part 11A.

更に、シランカップリング処理工程により、アルミニウム材11の表面側のナノスパイクアレイ13の部分にシランカップリング処理が施される。ここでは、先ず、アルミニウム材11をアセトンに浸漬しながら超音波洗浄を行う。そして、3−イソシアネートプロピルトリエトキシシランを主成分とするシランカップリング剤を1重量%に希釈し、5分間撹拌する。更に、ナノスパイクアレイ13が形成されたアルミニウム材11の表面部分に、シランカップリング剤を1重量%で希釈した溶液を含浸させた紙製のウエスを被せ1分間放置する。その後、当該ウエスを取り除いたアルミニウム材11を100℃に加熱したオーブンに入れ、アルミニウム材11の表面に付着したシランカップリング剤が乾燥するまでアルミニウム材11を放置する。   Furthermore, a silane coupling process is performed on the portion of the nano spike array 13 on the surface side of the aluminum material 11 by the silane coupling process. Here, first, ultrasonic cleaning is performed while the aluminum material 11 is immersed in acetone. And the silane coupling agent which has 3-isocyanate propyl triethoxysilane as a main component is diluted to 1 weight%, and is stirred for 5 minutes. Further, the surface portion of the aluminum material 11 on which the nanospike array 13 is formed is covered with a paper waste impregnated with a solution obtained by diluting a silane coupling agent at 1% by weight and left for 1 minute. Thereafter, the aluminum material 11 from which the waste has been removed is placed in an oven heated to 100 ° C., and the aluminum material 11 is left until the silane coupling agent attached to the surface of the aluminum material 11 is dried.

次に、接合工程により、ナノスパイクアレイ13が形成されたアルミニウム材11と樹脂21との各接合部分11A,21Aが接合される。ここでは、シランカップリング剤が塗布されたアルミニウム材11について、図2(A)に示されるように、ナノスパイクアレイ13が形成された接合部分11A側を上向きにして、290℃に加熱したホットプレートH上に載置して1分間放置した後、接合部分11Aに樹脂21の接合部分21Aを重ね合わせる。その上で、接合部分21A側が溶融状態になった樹脂21の同図中上方から125.4kPaの圧力を加えて加圧状態とし、そのまま3分間放置する。その後、当該加圧状態を維持したまま、ホットプレートHの電源を落とし、空冷により室温程度まで温度を低下させることで、樹脂21を固化させてアルミニウム材11に接合し、図2(B)のような樹脂金属接合体10が得られた。   Next, the joining portions 11A and 21A of the aluminum material 11 on which the nano spike array 13 is formed and the resin 21 are joined by a joining process. Here, as shown in FIG. 2 (A), the aluminum material 11 coated with the silane coupling agent is heated to 290 ° C. with the joining portion 11A side where the nanospike array 13 is formed facing upward. After being placed on the plate H and left for 1 minute, the joining portion 21A of the resin 21 is overlaid on the joining portion 11A. Then, a pressure of 125.4 kPa is applied from above in the figure of the resin 21 in which the joining portion 21A side is in a molten state to make it a pressurized state and left as it is for 3 minutes. Thereafter, the hot plate H is turned off while maintaining the pressurized state, and the temperature is lowered to about room temperature by air cooling, so that the resin 21 is solidified and joined to the aluminum material 11, as shown in FIG. Such a resin-metal bonded body 10 was obtained.

本発明者らによって行われた樹脂金属接合体10の接合強度実験(せん断試験)によれば、本実施例に係る樹脂金属接合体10の接合強度は、27.8MPaとなった。一方、前記実施例と同一のアルミニウム材11について、ナノスパイクアレイ13を形成せずに、シランカップリング処理を行ってから実施例と同一の樹脂21とを接合してなる従来の樹脂金属接合体(比較例1)について、前述と同一条件の接合強度実験を行うと、その接合強度が22.6MPaとなった。また、前記実施例と同一のアルミニウム材11について、ナノスパイクアレイ13を形成せずに、エポキシ樹脂及びアクリル樹脂からなる粘接着シートを用いて前記実施例と同一の樹脂21とを接合してなる従来の樹脂金属接合体(比較例2)について、前述と同一条件の接合強度実験を行うと、その接合強度が25.0MPaとなった。   According to the bonding strength experiment (shear test) of the resin / metal bonded body 10 conducted by the present inventors, the bonding strength of the resin / metal bonded body 10 according to this example was 27.8 MPa. On the other hand, for the same aluminum material 11 as in the previous embodiment, a conventional resin-metal bonded body obtained by bonding the same resin 21 as in the embodiment after performing the silane coupling treatment without forming the nano spike array 13. With respect to (Comparative Example 1), when a bonding strength experiment was performed under the same conditions as described above, the bonding strength was 22.6 MPa. Moreover, about the same aluminum material 11 as the said Example, the same resin 21 as the said Example was joined, without forming the nano spike array 13, using the adhesive sheet which consists of an epoxy resin and an acrylic resin. For the conventional resin-metal bonded body (Comparative Example 2), when the bonding strength experiment was performed under the same conditions as described above, the bonding strength was 25.0 MPa.

以上の実験結果によれば、本実施例に係る樹脂金属接合体10は、各比較例に係る従来の樹脂金属接合体よりも、アルミニウム材11と樹脂21との接合強度が高くなることが実証された。   According to the above experimental results, it is proved that the resin-metal bonded body 10 according to the present example has higher bonding strength between the aluminum material 11 and the resin 21 than the conventional resin-metal bonded bodies according to the comparative examples. It was done.

なお、他の実施例として、前記実施例に対して、シランカップリング処理工程を省略することによっても、図2(B)に模式的に示される樹脂金属接合体10が得られた。   As another example, the resin-metal bonded body 10 schematically shown in FIG. 2B was also obtained by omitting the silane coupling treatment step with respect to the above example.

本発明は、前述した樹脂の他の樹脂にも適用可能である。   The present invention is also applicable to other resins described above.

10 樹脂金属接合体
11 アルミニウム材
11A 接合部分
12 ポーラスアルミナ層
13 ナノスパイクアレイ
13A 突起
21 樹脂
21A 接合部分
H ホットプレート
S 隙間
DESCRIPTION OF SYMBOLS 10 Resin metal joined body 11 Aluminum material 11A Joining part 12 Porous alumina layer 13 Nano spike array 13A Protrusion 21 Resin 21A Joining part H Hot plate S Gap

Claims (5)

樹脂とアルミニウム材を接合してなる樹脂金属接合体の製造方法において、
前記アルミニウム材の表面に多数突出する針状の突起からなるナノスパイクアレイを作製するナノスパイクアレイ作製工程と、前記各突起の間に形成された隙間に溶融状態の前記樹脂を侵入させてから固化することで、前記アルミニウム材と前記樹脂を接合する接合工程とを順に行うことを特徴とする樹脂金属接合体の製造方法。
In the method for producing a resin-metal bonded body obtained by bonding a resin and an aluminum material,
A nanospike array manufacturing process for manufacturing a nanospike array consisting of a plurality of needle-like protrusions protruding on the surface of the aluminum material, and solidifying after injecting the molten resin into the gap formed between the protrusions Then, the joining process which joins the said aluminum material and the said resin in order is performed, The manufacturing method of the resin metal joined body characterized by the above-mentioned.
前記ナノスパイクアレイ作製工程では、前記アルミニウム材を陽極酸化処理することで、当該アルミニウム材の表面にポーラス構造のポーラスアルミナを形成した後、エッチング処理により前記ポーラスアルミナを除去することで、前記アルミニウム材の新たな表面に前記ナノスパイクアレイを形成することを特徴とする請求項1記載の樹脂金属接合体の製造方法。   In the nano spike array manufacturing step, the aluminum material is anodized to form porous alumina having a porous structure on the surface of the aluminum material, and then the porous alumina is removed by an etching process. The method for producing a resin-metal bonded body according to claim 1, wherein the nanospike array is formed on a new surface. 前記ナノスパイクアレイ作製工程と前記接合工程との間に、前記ナノスパイクアレイが形成された前記アルミニウム材の表面にシランカップリング処理を行うシランカップリング処理工程を行い、
前記接合工程では、シランカップリング処理後の前記アルミニウム材の表面に前記樹脂を接合することを特徴とする請求項1又は2記載の樹脂金属接合体の製造方法。
A silane coupling treatment step is performed between the nanospike array manufacturing step and the bonding step to perform a silane coupling treatment on the surface of the aluminum material on which the nanospike array is formed,
The method for producing a resin-metal bonded body according to claim 1 or 2, wherein, in the bonding step, the resin is bonded to the surface of the aluminum material after the silane coupling treatment.
前記樹脂は、母材に熱可塑性樹脂を用いた熱可塑性炭素繊維強化樹脂であり、
前記接合工程では、加熱によって溶融状態となった前記樹脂の接合部分と、前記ナノスパイクアレイが形成された前記アルミニウム材の接合部分とを相互に接近させる方向に押圧するホットプレス処理により、前記各接合部分が接合されることを特徴とする請求項1、2又は3記載の樹脂金属接合体の製造方法。
The resin is a thermoplastic carbon fiber reinforced resin using a thermoplastic resin as a base material,
In the joining step, each of the above-described resin components is hot-pressed by pressing in a direction in which the joint portion of the resin that has been melted by heating and the joint portion of the aluminum material on which the nanospike array is formed are brought close to each other. The method for producing a resin-metal bonded body according to claim 1, 2 or 3, wherein the bonded portion is bonded.
樹脂とアルミニウム材の接合体において、
前記樹脂に接合する前記アルミニウム材の接合部分には、平面視で多数散在する錐体状の突起が形成され、当該各突起の間に前記樹脂が入り込むことで、前記樹脂と前記アルミニウム材とが噛み合った状態で接合していることを特徴とする樹脂金属接合体。
In the joined body of resin and aluminum,
A large number of cone-shaped projections scattered in a plan view are formed in the joining portion of the aluminum material to be joined to the resin, and the resin and the aluminum material are formed by the resin entering between the projections. A resin-metal bonded body characterized by being bonded in a meshed state.
JP2016197812A 2016-10-06 2016-10-06 Manufacturing method of resin metal joint Active JP6809680B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2016197812A JP6809680B2 (en) 2016-10-06 2016-10-06 Manufacturing method of resin metal joint

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2016197812A JP6809680B2 (en) 2016-10-06 2016-10-06 Manufacturing method of resin metal joint

Publications (2)

Publication Number Publication Date
JP2018058279A true JP2018058279A (en) 2018-04-12
JP6809680B2 JP6809680B2 (en) 2021-01-06

Family

ID=61909537

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016197812A Active JP6809680B2 (en) 2016-10-06 2016-10-06 Manufacturing method of resin metal joint

Country Status (1)

Country Link
JP (1) JP6809680B2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110284142A (en) * 2019-07-24 2019-09-27 东莞智富五金制品有限公司 A kind of aluminium radiator and clinching method improving the embedding structure of riveting
CN113085194A (en) * 2021-03-11 2021-07-09 卓外(上海)医疗电子科技有限公司 Heterogeneous connection method suitable for endoscope structure
CN113490588A (en) * 2019-03-08 2021-10-08 睦月电机株式会社 Method for producing metal-resin bonded body
JP2021169189A (en) * 2020-04-17 2021-10-28 国立大学法人大阪大学 Dissimilar material joining member and its manufacturing method
CN114340877A (en) * 2020-08-07 2022-04-12 睦月电机株式会社 Metal-resin bonded body and method for producing metal-resin bonded body
JP2022161063A (en) * 2021-04-08 2022-10-21 Jfeスチール株式会社 Galvanized steel sheet, and method of producing the same
CN116061509A (en) * 2023-01-20 2023-05-05 太原科技大学 Method for preparing carbon fiber/stainless steel thin layer laminated board based on anodic oxidation process

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005059472A (en) * 2003-08-18 2005-03-10 Mitsubishi Alum Co Ltd Manufacturing method of resin-coated aluminum material, resin-coated can lid and aluminum container
JP2009166502A (en) * 2004-12-03 2009-07-30 Sharp Corp Reflection preventing material, stamper, stamper manufacturing method, and reflection preventing material manufacturing method using the stamper
JP2012187861A (en) * 2011-03-11 2012-10-04 Teijin Ltd Method of manufacturing connector of carbon fiber composite material
WO2013146656A1 (en) * 2012-03-26 2013-10-03 シャープ株式会社 Mold release treatment method and method for producing anti-reflective film
JP2015514861A (en) * 2012-02-24 2015-05-21 シェンゼェン ビーワイディー オート アールアンドディー カンパニーリミテッド Aluminum alloy, aluminum alloy resin composite, and preparation method thereof

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005059472A (en) * 2003-08-18 2005-03-10 Mitsubishi Alum Co Ltd Manufacturing method of resin-coated aluminum material, resin-coated can lid and aluminum container
JP2009166502A (en) * 2004-12-03 2009-07-30 Sharp Corp Reflection preventing material, stamper, stamper manufacturing method, and reflection preventing material manufacturing method using the stamper
JP2012187861A (en) * 2011-03-11 2012-10-04 Teijin Ltd Method of manufacturing connector of carbon fiber composite material
JP2015514861A (en) * 2012-02-24 2015-05-21 シェンゼェン ビーワイディー オート アールアンドディー カンパニーリミテッド Aluminum alloy, aluminum alloy resin composite, and preparation method thereof
WO2013146656A1 (en) * 2012-03-26 2013-10-03 シャープ株式会社 Mold release treatment method and method for producing anti-reflective film

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113490588A (en) * 2019-03-08 2021-10-08 睦月电机株式会社 Method for producing metal-resin bonded body
CN110284142A (en) * 2019-07-24 2019-09-27 东莞智富五金制品有限公司 A kind of aluminium radiator and clinching method improving the embedding structure of riveting
CN110284142B (en) * 2019-07-24 2023-12-15 东莞智富五金制品有限公司 Aluminum radiator with improved riveting structure and riveting method
JP2021169189A (en) * 2020-04-17 2021-10-28 国立大学法人大阪大学 Dissimilar material joining member and its manufacturing method
JP7477097B2 (en) 2020-04-17 2024-05-01 国立大学法人大阪大学 Dissimilar material joint member and manufacturing method thereof
CN114340877A (en) * 2020-08-07 2022-04-12 睦月电机株式会社 Metal-resin bonded body and method for producing metal-resin bonded body
CN114340877B (en) * 2020-08-07 2024-06-07 睦月电机株式会社 Metal-resin bonded body and method for producing metal-resin bonded body
CN113085194A (en) * 2021-03-11 2021-07-09 卓外(上海)医疗电子科技有限公司 Heterogeneous connection method suitable for endoscope structure
JP2022161063A (en) * 2021-04-08 2022-10-21 Jfeスチール株式会社 Galvanized steel sheet, and method of producing the same
JP7476840B2 (en) 2021-04-08 2024-05-01 Jfeスチール株式会社 Zinc-coated steel sheet and its manufacturing method
CN116061509A (en) * 2023-01-20 2023-05-05 太原科技大学 Method for preparing carbon fiber/stainless steel thin layer laminated board based on anodic oxidation process

Also Published As

Publication number Publication date
JP6809680B2 (en) 2021-01-06

Similar Documents

Publication Publication Date Title
JP6809680B2 (en) Manufacturing method of resin metal joint
JP2019166638A (en) Manufacturing method of resin-metal joined body and resin-metal joined body
JP5094839B2 (en) Aluminum alloy composite
CN107709002B (en) Metal resin composite molded body and method for producing same
JP6341156B2 (en) Resin bonded body, resin bonded body manufacturing method, and vehicle structure
JP5094849B2 (en) Stainless steel composite
US10105898B2 (en) Resin joined body, manufacturing method of resin joined body, and vehicle structure
US20160318292A1 (en) Metal or ceramic component comprising at least one multi-dimensionally structured connection portion and method for the production thereof
US9770863B2 (en) Systems and methods to reduce air pocket formation during welding
US20190168462A1 (en) Method for producing a composite component for a motor vehicle
CN112046037B (en) Method for integrating a first part and a second part comprising a composite material
JP2018039247A (en) Composite body of cfrtp and metal
JP6400399B2 (en) Composite structure of metal and reinforced fiber thermoplastic resin and method for producing the same
KR102300339B1 (en) Welding method for steel sheet and carbon fiber reinforced plastics sheet
KR101804661B1 (en) Resin joined body, method of producing resin joined body, and vehicular structural body
JP7468836B2 (en) FRP and metal bonded products and their manufacturing method
Tamura et al. Ultrasonic joining of carbon fiber reinforced thermoplastic and Ti alloy
CN112313071A (en) Joined structure and method for manufacturing same
KR102299731B1 (en) Welding method for steel sheet and carbon fiber reinforced plastics sheet
JP2023025546A (en) Method of manufacturing composite of cfrp and metal materials and the composite
JP2018069658A (en) Adhesion structure and bonding method
KR102300341B1 (en) Welding method for aluminium sheet and carbon fiber reinforced plastics sheet
JP2019503281A (en) Improvements in or related to fiber reinforced composites
US20240217184A1 (en) Method of ultrasonic welding thermoplastic composite components
JP6610859B2 (en) Composite member and method for manufacturing the composite member

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20190920

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20200924

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20201005

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20201026

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20201202

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20201202

R150 Certificate of patent or registration of utility model

Ref document number: 6809680

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250