JP2003145625A - Method for connecting thermoplastic resin member and method for connecting fiber-reinforced thermoplastic resin member - Google Patents

Method for connecting thermoplastic resin member and method for connecting fiber-reinforced thermoplastic resin member

Info

Publication number
JP2003145625A
JP2003145625A JP2001344818A JP2001344818A JP2003145625A JP 2003145625 A JP2003145625 A JP 2003145625A JP 2001344818 A JP2001344818 A JP 2001344818A JP 2001344818 A JP2001344818 A JP 2001344818A JP 2003145625 A JP2003145625 A JP 2003145625A
Authority
JP
Japan
Prior art keywords
thermoplastic resin
resin member
fiber
probe
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
JP2001344818A
Other languages
Japanese (ja)
Inventor
Shuji Inoue
修次 井上
Mikiyuki Shimizu
幹幸 清水
Kiyotaka Nakai
清隆 中井
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.)
Aisin Corp
Original Assignee
Aisin Seiki Co Ltd
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 Aisin Seiki Co Ltd filed Critical Aisin Seiki Co Ltd
Priority to JP2001344818A priority Critical patent/JP2003145625A/en
Publication of JP2003145625A publication Critical patent/JP2003145625A/en
Pending legal-status Critical Current

Links

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
    • 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
    • B29C65/06Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
    • B29C65/0681Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding created by a tool
    • 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
    • B29C66/114Single butt joints
    • B29C66/1142Single butt to butt 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
    • B29C66/32Measures for keeping the burr form under control; Avoiding burr formation; Shaping the burr
    • B29C66/324Avoiding burr formation
    • 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
    • B29C66/72General 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
    • B29C66/7214Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72143Fibres of discontinuous lengths
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/814General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8141General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
    • B29C66/81427General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined comprising a single ridge, e.g. for making a weakening line; comprising a single tooth
    • B29C66/81429General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined comprising a single ridge, e.g. for making a weakening line; comprising a single tooth comprising a single tooth
    • 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
    • B29C66/836Moving relative to and tangentially to the parts to be joined, e.g. transversely to the displacement of the parts to be joined, e.g. using a X-Y table
    • 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
    • B29C66/93Measuring or controlling the joining process by measuring or controlling the speed
    • B29C66/934Measuring or controlling the joining process by measuring or controlling the speed by controlling or regulating the speed
    • B29C66/93451Measuring or controlling the joining process by measuring or controlling the speed by controlling or regulating the speed by controlling or regulating the rotational speed, i.e. the speed of revolution
    • 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
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/812General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/8122General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps characterised by the composition of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • 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
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/814General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8141General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
    • B29C66/81411General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined characterised by its cross-section, e.g. transversal or longitudinal, being non-flat
    • B29C66/81421General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined characterised by its cross-section, e.g. transversal or longitudinal, being non-flat being convex or concave
    • B29C66/81422General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined characterised by its cross-section, e.g. transversal or longitudinal, being non-flat being convex or concave being convex
    • 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
    • B29C66/93Measuring or controlling the joining process by measuring or controlling the speed
    • B29C66/939Measuring or controlling the joining process by measuring or controlling the speed characterised by specific speed values or ranges

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

PROBLEM TO BE SOLVED: To prevent a burr from occurring in the connection of a thermoplastic resin and to increase the connecting strength in the case of connecting a fiber- reinforced thermoplastic resin. SOLUTION: The method for connecting the thermoplastic resin member comprises the steps of bringing a first thermoplastic resin member 1 into contact with a second thermoplastic resin member 2, then pushing the first thermoplastic resin member 1 including the predetermined part of the surface boundary line 7a between the member 1 and the member 2 against a rotating probe 8 on the surface of the member 2.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は熱可塑性樹脂部材の
接合方法および繊維強化熱可塑性樹脂部材の接合方法に
関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for joining thermoplastic resin members and a method for joining fiber reinforced thermoplastic resin members.

【0002】[0002]

【従来の技術】従来、熱可塑性樹脂部材の接合は、接合
面同士を当接させた後に振動、超音波、樹脂部材同士の
摩擦などにより接合面が溶融するまでエネルギーを付与
するか、予め接合面を熱板に押し当てて接合面が溶融す
るまでエネルギーを付与した後に接合面同士を当接させ
て行っていた。
2. Description of the Related Art Conventionally, for joining thermoplastic resin members, energy is applied until the joining surfaces are melted by vibrating, ultrasonic waves, friction between the resin members or the like after the joining surfaces are brought into contact with each other, or by previously joining. The surface was pressed against a hot plate, energy was applied until the bonded surfaces were melted, and then the bonded surfaces were brought into contact with each other.

【0003】一方、樹脂の中にガラスファイバ、カーボ
ンファイバなどの繊維を含有させた繊維強化樹脂の接合
も振動、超音波、樹脂部材同士の摩擦、熱板などを使用
した接合が行われていた。例えば、特開平08−142
197号公報には、繊維を接合面に向かって配向した繊
維強化樹脂と繊維を含まない樹脂を当接し、振動溶着す
る樹脂部品の製造方法が開示されている。
On the other hand, the joining of fiber reinforced resin containing fibers such as glass fiber and carbon fiber in resin has also been performed by using vibration, ultrasonic waves, friction between resin members, and hot plate. . For example, Japanese Patent Laid-Open No. 08-142
Japanese Patent Laid-Open No. 197 discloses a method of manufacturing a resin component in which a fiber-reinforced resin in which fibers are oriented toward a joint surface and a resin containing no fibers are brought into contact with each other and vibration welding is performed.

【0004】[0004]

【発明が解決しようとする課題】しかしながら、振動、
超音波、樹脂部材同士の摩擦、熱板など、いずれの方法
でも接合面付近が溶融された状態で、ある所定の加圧力
で接合面同士を押し付けているので、接合部分にバリが
発生する問題があった。バリが発生すると、それを除去
する工程が必要でコストアップする問題点がある。ま
た、バリが除去できない場合、製品によっては性能に悪
影響を生ずる。例えばインテークマニホールドの内径側
のように、発生したバリを除去できないと、そのバリが
燃料の供給量を低下させる問題が発生する。
However, vibration,
With any method such as ultrasonic waves, friction between resin members, hot plate, etc., since the joining surfaces are pressed with a certain predetermined pressure with the vicinity of the joining surfaces being melted, burrs occur at the joining part. was there. When burrs are generated, there is a problem that a step of removing the burrs is required and the cost is increased. Further, if the burr cannot be removed, the performance may be adversely affected depending on the product. For example, if the generated burr cannot be removed like the inner diameter side of the intake manifold, there is a problem that the burr reduces the fuel supply amount.

【0005】一方、繊維強化樹脂の場合は以下の問題点
が存在する。繊維強化樹脂は、繊維の配向が強度に影響
することが良く知られている。つまり、繊維の配向方向
に平行な方向の応力には強く、繊維の配向方向と直交す
る方向の応力には弱い。したがって、接合強度の大きく
するためには、繊維の配向方向を接合面に直交させてお
くことがのぞましい。そのため、上記の公報では、接合
前に、繊維を接合面に向かって配向させている。しかし
ながら、接合前に、繊維を接合面に向かって配向させて
いても、接合する部材同士を押さえ付けておく必要があ
るため、図7に示すように、振動溶着時に繊維20が振
動方向と平行すなわち第1樹脂部材22と第2樹脂部材
23の接合面21と平行に配向してしまい、接合面21
と直交する方向の引張強度(接合強度)が母材の約20
〜30%程度の接合強度レベルまで低下する問題点があ
る。なお、繊維の配向方向とは、繊維の長軸の方向であ
る。
On the other hand, the fiber-reinforced resin has the following problems. It is well known that the fiber orientation affects the strength of the fiber orientation. That is, it is strong against the stress in the direction parallel to the fiber orientation direction and weak against the stress in the direction orthogonal to the fiber orientation direction. Therefore, in order to increase the bonding strength, it is desirable to make the fiber orientation direction orthogonal to the bonding surface. Therefore, in the above publication, the fibers are oriented toward the joint surface before joining. However, even if the fibers are oriented toward the bonding surface before bonding, it is necessary to press the members to be bonded together. Therefore, as shown in FIG. 7, the fibers 20 are parallel to the vibration direction during vibration welding. That is, the first resin member 22 and the second resin member 23 are oriented parallel to the joint surface 21, and the joint surface 21
Tensile strength (joint strength) in the direction orthogonal to
There is a problem that the bonding strength level is lowered to about 30%. The fiber orientation direction is the direction of the long axis of the fiber.

【0006】本発明は上記課題を解決したもので、バリ
が発生しない樹脂部材の接合方法を提供するか、繊維強
化樹脂の接合にあっては接合強度の大きな接合方法を提
供するものである。
The present invention has solved the above-mentioned problems and provides a method for joining resin members in which burrs do not occur, or a joining method with high joining strength in joining fiber-reinforced resin.

【0007】[0007]

【課題を解決するための手段】上記技術的課題を解決す
るために、本発明の請求項1において講じた技術的手段
(以下、第1の技術的手段と称する。)は、第1熱可塑
性樹脂部材と第2熱可塑性樹脂部材を当接後、前記第1
熱可塑性樹脂部材と前記第2熱可塑性樹脂部材との表面
境界線の所定部分を含む前記第1熱可塑性樹脂部材と前
記第2熱可塑性樹脂部材の表面部に回転するプローブを
押し当てて前記表面境界線に沿って移動させることを特
徴とする熱可塑性樹脂部材の接合方法である。ここで、
表面境界線とは、第1熱可塑性樹脂部材と第2熱可塑性
樹脂部材との当接部分のうち表面に露出している部分の
ことである。
In order to solve the above technical problems, the technical means taken in claim 1 of the present invention (hereinafter referred to as the first technical means) is the first thermoplastic resin. After contacting the resin member and the second thermoplastic resin member,
A surface of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined part of the surface boundary line between the thermoplastic resin member and the second thermoplastic resin member is pressed against the surface portion by rotating a probe. A method for joining thermoplastic resin members is characterized by moving along a boundary line. here,
The surface boundary line is a portion of the contact portion between the first thermoplastic resin member and the second thermoplastic resin member, which is exposed on the surface.

【0008】上記第1の技術的手段によれば、回転する
プローブと熱可塑性樹脂部材との摩擦による発熱により
熱可塑性樹脂部材のプローブが押し当てられている部分
が溶融すると共に、溶融部分がプローブにより押し付け
られているので、溶融した樹脂が押さえられバリの発生
を抑止できる。さらに詳しく述べれば、回転するプロー
ブの前方部分が押し当てられている熱可塑性樹脂部材が
溶融し、第1熱可塑性樹脂部材と第2熱可塑性樹脂部材
が接合し、プローブの後方部分が押し当てられている部
分で固化する。この溶融、接合、固化の間、溶融した部
分はプローブにより押さえられているので、樹脂がプロ
ーブ側に出てくることができない。したがって、バリが
発生することがない。なお、プローブの前方、後方と
は、プローブが前進する方向とその逆の方向のことであ
る。また、熱可塑性樹脂部材のプローブが押し当てられ
ている側の表面に対向する裏面側には両熱可塑性樹脂部
材に密着する支持部材が設けられている。以下の説明で
も同様である。
According to the first technical means, heat generated by friction between the rotating probe and the thermoplastic resin member melts the portion of the thermoplastic resin member against which the probe is pressed, and the melted portion is the probe. Since it is pressed by, the melted resin is pressed and the occurrence of burrs can be suppressed. More specifically, the thermoplastic resin member against which the front portion of the rotating probe is pressed melts, the first thermoplastic resin member and the second thermoplastic resin member are joined, and the rear portion of the probe is pressed against. It solidifies in the part where it is. During the melting, joining, and solidification, the melted portion is held down by the probe, so the resin cannot come out to the probe side. Therefore, burrs do not occur. The front and rear of the probe are the direction in which the probe moves forward and the opposite direction. In addition, a support member that is in close contact with both thermoplastic resin members is provided on the back surface side of the thermoplastic resin member that faces the surface of the side on which the probe is pressed. The same applies to the following description.

【0009】上記技術的課題を解決するために、本発明
の請求項2において講じた技術的手段(以下、第2の技
術的手段と称する。)は、第1熱可塑性樹脂部材と第2
熱可塑性樹脂部材の少なくとも一方が繊維強化樹脂から
なり、前記第1熱可塑性樹脂部材と前記第2熱可塑性樹
脂部材を当接後、前記第1熱可塑性樹脂部材と前記第2
熱可塑性樹脂部材との表面境界線の所定部分を含む前記
第1熱可塑性樹脂部材と前記第2熱可塑性樹脂部材の表
面部に回転するプローブを押し当てて前記表面境界線に
沿って移動させることを特徴とする繊維強化熱可塑性樹
脂部材の接合方法である。ここで、表面境界線とは、第
1の技術的手段と同様、第1熱可塑性樹脂部材と第2熱
可塑性樹脂部材との当接部分のうち表面に露出している
部分のことである。
In order to solve the above technical problems, the technical means taken in claim 2 of the present invention (hereinafter referred to as the second technical means) are the first thermoplastic resin member and the second thermoplastic resin member.
At least one of the thermoplastic resin members is made of fiber reinforced resin, and after contacting the first thermoplastic resin member and the second thermoplastic resin member, the first thermoplastic resin member and the second thermoplastic resin member
Pressing the rotating probe against the surface portions of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined portion of the surface boundary line with the thermoplastic resin member and moving the probe along the surface boundary line. And a method for joining fiber-reinforced thermoplastic resin members. Here, the surface boundary line is a portion of the contact portion between the first thermoplastic resin member and the second thermoplastic resin member that is exposed on the surface, as in the first technical means.

【0010】上記第2の技術的手段によれば、回転する
プローブと熱可塑性樹脂部材との摩擦による発熱により
熱可塑性樹脂部材のプローブが押し当てられている部分
が溶融すると共に、プローブの前方部分で溶融した熱可
塑性樹脂部材中の繊維がプローブの回転に引きずられて
配向方向が変えられ、プローブの後方部分で当接部の当
接面にほぼ直交する方向に繊維が配向された状態で固化
するので、接合強度の大きな接合が実現できる。
According to the second technical means, heat generated by friction between the rotating probe and the thermoplastic resin member melts the portion of the thermoplastic resin member against which the probe is pressed and the front portion of the probe. The orientation of the fibers in the thermoplastic resin melted by the probe is changed by the rotation of the probe, and the fibers are solidified in the rear part of the probe with the fibers oriented in a direction almost orthogonal to the contact surface of the contact part. As a result, it is possible to realize a bond having a high bonding strength.

【0011】そのメカニズムを以下のように推論してい
る。図1〜4を用いて説明する。図1は接合前の第1繊
維強化樹脂部材と第2繊維強化樹脂部材を当接した状態
を上面から見た断面説明図、図2は図1と同じ状態を側
面から見た断面説明図である。図2は図1のAA断面に
相当する。
The mechanism is inferred as follows. This will be described with reference to FIGS. FIG. 1 is a cross-sectional explanatory view of the state in which the first fiber-reinforced resin member and the second fiber-reinforced resin member before joining are in contact with each other as seen from above, and FIG. 2 is a cross-sectional explanatory view of the same state as that in FIG. 1 seen from the side. is there. FIG. 2 corresponds to the AA cross section of FIG.

【0012】第1繊維強化樹脂部材1、第2繊維強化樹
脂部材2は、共に熱可塑性樹脂3、4と繊維5、6を混
合し、射出成形により成形された部材である。射出成形
時の樹脂の流れ方向に沿って繊維が配向している。図
1、2では第1繊維強化樹脂部材1と第2繊維強化樹脂
部材2の当接面7に直交する方向に繊維5、6が配向し
ている。ただし、当接面7は、第1繊維強化樹脂部材
1、第2繊維強化樹脂部材2の成形時の端部であり、樹
脂の流れの終端であるので、図1、2の繊維5a、6a
のように当接面7に平行な方向に配向している。
The first fiber reinforced resin member 1 and the second fiber reinforced resin member 2 are members formed by injection molding in which thermoplastic resins 3 and 4 and fibers 5 and 6 are mixed. The fibers are oriented along the direction of resin flow during injection molding. In FIGS. 1 and 2, the fibers 5 and 6 are oriented in a direction orthogonal to the contact surfaces 7 of the first fiber-reinforced resin member 1 and the second fiber-reinforced resin member 2. However, since the contact surface 7 is an end portion of the first fiber-reinforced resin member 1 and the second fiber-reinforced resin member 2 at the time of molding, and is the end of the resin flow, the fibers 5a and 6a of FIGS.
As described above, it is oriented in a direction parallel to the contact surface 7.

【0013】図3は接合中の第1繊維強化樹脂部材と第
2繊維強化樹脂部材を当接した状態を上面から見た断面
説明図、図4は図3と同じ状態を側面から見た接合完了
部分の断面説明図である。図4は図3のBB断面に相当
する。第1繊維強化樹脂部材1と第2繊維強化樹脂部材
2との表面境界線7aの所定部分を含む第1繊維強化樹
脂部材1、第2繊維強化樹脂部材2の表面部に回転する
プローブ8を押し当てて、表面境界線7aに沿ってD方
向に移動させている。表面境界線7aは当接面7の樹脂
表面に露出している部分である。プローブ8の回転方向
はC方向である。プローブ8の前方部分8aでは、プロ
ーブ8の回転による摩擦熱で熱可塑性樹脂が溶融する。
溶融した樹脂はプローブ8の回転力で引きずられ、回転
方向に沿って移動する。溶融した樹脂の移動によって第
1繊維強化樹脂部材1と第2繊維強化樹脂部材2の熱可
塑性樹脂同士が混合される。これにより第1繊維強化樹
脂部材1と第2繊維強化樹脂部材2が接合する。溶融し
た樹脂がプローブ8の回転方向に移動するとき、プロー
ブ8の前方部分8aにあった繊維9aは溶融した樹脂と
共に移動する。このとき、繊維9aはプローブ8の回転
力により、繊維9b、9c、9dのようにプローブ8の
回転方向に沿って配向方向が変えられ、プローブ8の後
方部分8bで樹脂が固化するときに位置が繊維9dのよ
うに固定される。固定された繊維9dの配向方向は、当
接面7にほぼ直交する方向となる。この結果、当接面7
に直交する方向の引張応力に対する接合強度を大きくす
ることができる。接合時の樹脂溶融部分の周辺では配向
方向が当接面7と直交していない繊維が存在するが、接
合強度に大きな影響をもたらさない。これは、第1繊維
強化樹脂部材1と第2繊維強化樹脂部材2の母材の部分
であり、接合部分の強度より大きいからである。
FIG. 3 is a cross-sectional explanatory view showing a state in which the first fiber-reinforced resin member and the second fiber-reinforced resin member being joined are in contact with each other as viewed from above, and FIG. 4 is a side view showing the same state as in FIG. It is a section explanatory view of a completed portion. FIG. 4 corresponds to the BB cross section of FIG. A probe 8 rotating on the surface of the first fiber reinforced resin member 1 and the second fiber reinforced resin member 2 including a predetermined portion of the surface boundary line 7a between the first fiber reinforced resin member 1 and the second fiber reinforced resin member 2. It is pressed and moved in the D direction along the surface boundary line 7a. The surface boundary line 7a is a portion exposed on the resin surface of the contact surface 7. The rotation direction of the probe 8 is the C direction. At the front portion 8a of the probe 8, the thermoplastic resin is melted by the frictional heat generated by the rotation of the probe 8.
The molten resin is dragged by the rotational force of the probe 8 and moves along the rotational direction. Due to the movement of the molten resin, the thermoplastic resins of the first fiber reinforced resin member 1 and the second fiber reinforced resin member 2 are mixed. As a result, the first fiber-reinforced resin member 1 and the second fiber-reinforced resin member 2 are joined. When the molten resin moves in the rotation direction of the probe 8, the fibers 9a in the front portion 8a of the probe 8 move together with the molten resin. At this time, the orientation of the fiber 9a is changed by the rotational force of the probe 8 along the rotational direction of the probe 8 like the fibers 9b, 9c, and 9d, and when the resin is solidified at the rear portion 8b of the probe 8, the position is changed. Are fixed like fibers 9d. The orientation direction of the fixed fiber 9d is substantially orthogonal to the contact surface 7. As a result, the contact surface 7
The joint strength with respect to the tensile stress in the direction orthogonal to can be increased. There are fibers whose orientation direction is not orthogonal to the contact surface 7 around the resin-melted portion at the time of joining, but this does not significantly affect the joining strength. This is because it is the base material portion of the first fiber reinforced resin member 1 and the second fiber reinforced resin member 2, and is larger than the strength of the joint portion.

【0014】[0014]

【発明の実施の形態】以下、本発明の実施例について、
図面に基づいて説明する。図5は実施例に使用したプロ
ーブの断面図である。プローブ8は、シャフト部10と
撹拌子部11から構成され、その材質はSKD61(窒
化処理)である。シャフト部10は直径15mm、長さ
100mmの円柱状で、その長さ方向の一方端に撹拌子
部11が設けられている。撹拌子部11が設けられてい
るシャフト部10の撹拌子部11周辺部分はショルダ部
12である。ショルダ部12は、接合時に樹脂と当接す
る部分である。撹拌子11は、直径4mmの円柱の先端
に半径2mmの半球が設けられた形状である。ショルダ
部12から半球の先端までの距離(撹拌子出代)は4.
22mmである。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below.
It will be described with reference to the drawings. FIG. 5 is a cross-sectional view of the probe used in the examples. The probe 8 is composed of a shaft portion 10 and a stirrer portion 11, and the material thereof is SKD61 (nitriding treatment). The shaft portion 10 has a cylindrical shape with a diameter of 15 mm and a length of 100 mm, and an agitator portion 11 is provided at one end in the length direction. The portion around the stirrer portion 11 of the shaft portion 10 provided with the stirrer portion 11 is a shoulder portion 12. The shoulder portion 12 is a portion that comes into contact with the resin at the time of joining. The stirrer 11 has a shape in which a hemisphere having a radius of 2 mm is provided at the tip of a cylinder having a diameter of 4 mm. The distance from the shoulder portion 12 to the tip of the hemisphere (stirring allowance) is 4.
It is 22 mm.

【0015】図6は接合中のプローブの状態を説明する
説明図である。プローブ8のシャフト部10は、図示し
ないプローブ8を回転駆動させる立フライス盤装置のプ
ローブ保持部に保持されている。このときプローブ8の
円柱軸は、プローブ8を押し当てる樹脂13の表面13
aに垂直な軸からプローブ8の前進方向と反対の方向に
前進角だけ傾斜されて設けられている。実施例では前進
角は0.5°に設定されている。なお、樹脂13とは接
合する二つの樹脂を区別せずに表したものである。
FIG. 6 is an explanatory view for explaining the state of the probe during joining. The shaft portion 10 of the probe 8 is held by a probe holding portion of a vertical milling machine device that rotationally drives the probe 8 (not shown). At this time, the cylindrical axis of the probe 8 is the surface 13 of the resin 13 against which the probe 8 is pressed.
The probe 8 is inclined from the axis perpendicular to a in the direction opposite to the forward direction of the probe 8 by the forward angle. In the embodiment, the advance angle is set to 0.5 °. It should be noted that the resin 13 is a representation of the two resins to be joined without distinction.

【0016】プローブ8を230rpmで回転させ、図
3における表面境界線7aに沿って一方端7bから他方
端7cにプローブ8を加工速度20mm/minで移動
させる。このとき、プローブ8のショルダ部12を樹脂
13の表面13aから所定深さに樹脂13中に圧入する
ように設定されている。この所定深さをショルダ圧入深
さと称する。
The probe 8 is rotated at 230 rpm, and the probe 8 is moved from the one end 7b to the other end 7c along the surface boundary line 7a in FIG. 3 at a processing speed of 20 mm / min. At this time, the shoulder portion 12 of the probe 8 is set to be pressed into the resin 13 to a predetermined depth from the surface 13a of the resin 13. This predetermined depth is referred to as the shoulder press-fitting depth.

【0017】実施例1では、第1熱可塑性樹脂部材、第
2熱可塑性樹脂部材として共に100mm×100m
m、厚さ5mmの大きさの6ナイロン材(宇部興産株式
会社製:1013NW8)を使用した。厚さ5mmの一
辺同士を当接させ、その表面境界線7aに沿って上記の
ように回転するプローブ8を押し当てながらショルダ圧
入深さ0.05〜0.5mmの条件で接合した。第1熱
可塑性樹脂部材、第2熱可塑性樹脂部材は、互いに当接
する方向に軽く押さえるとともに、スプリングにより上
部から押さえて位置ずれを防いでいる。また図示されて
いないが、第1熱可塑性樹脂部材、第2熱可塑性樹脂部
材のプローブ8が押し当てられている表面の反対側の裏
面には第1熱可塑性樹脂部材、第2熱可塑性樹脂部材に
密着している支持部材(金属平板)が設けられている。
In Example 1, both the first thermoplastic resin member and the second thermoplastic resin member are 100 mm × 100 m.
A 6 nylon material (1013NW8 manufactured by Ube Industries, Ltd.) having a size of m and a thickness of 5 mm was used. The sides with a thickness of 5 mm were brought into contact with each other, and the probe 8 rotating as described above was pressed along the surface boundary line 7a while joining under the condition of a shoulder press-fitting depth of 0.05 to 0.5 mm. The first thermoplastic resin member and the second thermoplastic resin member are lightly pressed in the directions in which they come into contact with each other, and are pressed from above by a spring to prevent displacement. Although not shown, the first thermoplastic resin member and the second thermoplastic resin member are provided on the back surface of the first thermoplastic resin member and the second thermoplastic resin member opposite to the surfaces on which the probes 8 are pressed. A supporting member (a metal flat plate) that is in close contact with is provided.

【0018】比較例2では、実施例1と同様の第1熱可
塑性樹脂部材、第2熱可塑性樹脂部材を用いて、加圧力
21〜28kgf/cm、振幅1.7mm、溶着代
1.8mm、周波数240Hzの条件で振動溶着した。
In Comparative Example 2, the same first thermoplastic resin member and second thermoplastic resin member as in Example 1 were used, and the applied pressure was 21 to 28 kgf / cm 2 , the amplitude was 1.7 mm, and the welding margin was 1.8 mm. Then, vibration welding was performed under the condition of a frequency of 240 Hz.

【0019】実施例1、比較例1とも接合後、接合部を
目視で観察した。比較例1では接合部にバリが発生して
いたが、実施例1にはバリは見られなかった。この結
果、本発明の接合方法では、接合後のバリ取りの必要が
なく製造コストを低減できる。
After joining both Example 1 and Comparative Example 1, the joints were visually observed. In Comparative Example 1, burr was generated at the joint, but in Example 1, no burr was observed. As a result, in the joining method of the present invention, it is not necessary to remove burrs after joining, and the manufacturing cost can be reduced.

【0020】実施例2〜4では、第1熱可塑性樹脂部
材、第2熱可塑性樹脂部材としてガラス繊維入りの6ナ
イロンGF30材(宇部興産株式会社製:1015GN
KE)を使用した。直径約11μm、長さ約200μm
のガラス繊維が30重量%含まれている。ショルダ圧入
深さ以外は実施例1と同じ条件で、第1熱可塑性樹脂部
材と第2熱可塑性樹脂部材を接合した。第1熱可塑性樹
脂部材、第2熱可塑性樹脂部材ともガラス繊維の主配向
方向が当接面に直交するようになっている。実施例2、
実施例3、実施例4のショルダ圧入深さ条件は0.25
mm、0.10mm、0.05mmである。いずれの実
施例も3回実施した。すべての接合でバリは見られなか
った。接合後、JIS K 7162の1BAにしたが
って機械加工により試験片(全長:80mm、平行部厚
さ:3.5、平行部幅:5mm、平行部長さ:30m
m、標線間距離:25mm)を切り出した。試験片は、
接合部が平行部長さのほぼ真ん中で、当接面が平行部の
長さ方向すなわち引張方向と直交するように切り出され
ている。この試験片を用いて、5mm/minの引張速
度で引張強度試験を行った。
In Examples 2 to 4, glass fiber-containing 6-nylon GF30 material (manufactured by Ube Industries, Ltd .: 1015GN) was used as the first thermoplastic resin member and the second thermoplastic resin member.
KE) was used. Diameter about 11μm, length about 200μm
30% by weight of the glass fiber. The first thermoplastic resin member and the second thermoplastic resin member were joined under the same conditions as in Example 1 except for the shoulder press-fitting depth. In both the first thermoplastic resin member and the second thermoplastic resin member, the main orientation direction of the glass fiber is orthogonal to the contact surface. Example 2,
The shoulder press-fitting depth conditions of Example 3 and Example 4 are 0.25.
mm, 0.10 mm and 0.05 mm. All examples were performed 3 times. No burrs were found on all joints. After joining, the test piece was machined according to JIS K 7162 1BA (total length: 80 mm, parallel part thickness: 3.5, parallel part width: 5 mm, parallel part length: 30 m).
m, distance between marked lines: 25 mm) was cut out. The test piece is
The joining portion is cut out so that the contact surface is substantially in the middle of the length of the parallel portion and the contact surface is orthogonal to the length direction of the parallel portion, that is, the pulling direction. Using this test piece, a tensile strength test was performed at a pulling speed of 5 mm / min.

【0021】比較例2では、実施例2〜4と同じ材質の
第1熱可塑性樹脂部材、第2熱可塑性樹脂部材を用い
て、加圧力21〜28kgf/cm、振幅1.7m
m、深さ1.8mm、周波数240Hzの条件で振動溶
着した。第1熱可塑性樹脂部材、第2熱可塑性樹脂部材
ともガラス繊維の主配向方向が当接面に直交するように
なっている。比較例2も3回おこなったが、いずれの場
合も比較例1と同じように接合部にバリが発生した。接
合後、実施例2〜4と同様に試験片を切り出して、実施
例2〜4と同じ条件で引張強度試験を行った。
In Comparative Example 2, the first thermoplastic resin member and the second thermoplastic resin member made of the same materials as those in Examples 2 to 4 were used, and the applied pressure was 21 to 28 kgf / cm 2 and the amplitude was 1.7 m.
Vibration welding was performed under the conditions of m, depth 1.8 mm, and frequency 240 Hz. In both the first thermoplastic resin member and the second thermoplastic resin member, the main orientation direction of the glass fiber is orthogonal to the contact surface. Comparative Example 2 was also performed 3 times, but in all cases, burrs were generated in the joint portion as in Comparative Example 1. After joining, test pieces were cut out in the same manner as in Examples 2 to 4 and a tensile strength test was performed under the same conditions as in Examples 2 to 4.

【0022】次に、母材すなわち第1熱可塑性樹脂部
材、第2熱可塑性樹脂部材として用いた6ナイロンGF
30を用いて実施例2〜4、比較例2と同様の試験片を
ガラス繊維の主配向方向が引張方向と平行になるように
切り出し、実施例2〜4と同じ条件で引張強度試験を行
った。母材についても、3回試験した。
Next, 6 nylon GF used as the base material, that is, the first thermoplastic resin member and the second thermoplastic resin member
Test pieces similar to those in Examples 2 to 4 and Comparative Example 2 were cut out using No. 30 so that the main orientation direction of the glass fibers was parallel to the tensile direction, and a tensile strength test was performed under the same conditions as in Examples 2 to 4. It was The base material was also tested three times.

【0023】表1に、実施例2〜4、比較例2、母材の
引張強度試験結果を示した。それぞれの3回の引張強度
とその平均強度および母材の強度を基準とした相対強度
(母材強度保持率)を示した。比較例2では母材強度の
約20%に低下しているが、実施例2〜4では母材強度
の50%以上の強度を確保できている。ここで試験した
母材強度は、繊維強化樹脂として最も高強度となる方向
で試験した結果である。その強度の50%以上を確保で
きたことは、実用上優れた結果である。例えば、繊維の
方向がランダムな無配向の材料でも、上記したメカニズ
ムにより接合部では当接面に直交するように繊維が配向
するため母材強度以上の接合強度が実現できる。ショル
ダ深さは0.05〜0.5mmが望ましい。ショルダ深
さが大きすぎるとショルダ部で樹脂がはねのけられてバ
リが発生する恐れがある。ショルダ深さが小さすぎると
ショルダ部で樹脂を押さえられなくなり接合部に溝がで
きる。表1のように、望ましくはショルダ深さが0.2
5mm以下がよく、さらに望ましくは0.1mm以下が
よい。
Table 1 shows the results of tensile strength tests of Examples 2 to 4, Comparative Example 2 and the base material. The relative strength (base metal strength retention rate) based on the tensile strength of each of three times, its average strength, and the strength of the base material was shown. In Comparative Example 2, the strength is reduced to about 20% of the base metal strength, but in Examples 2 to 4, the strength of 50% or more of the base metal strength can be secured. The base material strength tested here is the result of testing in the direction of the highest strength of the fiber reinforced resin. The fact that 50% or more of the strength can be secured is an excellent result in practical use. For example, even in the case of a non-oriented material in which the direction of the fibers is random, the fibers are oriented so as to be orthogonal to the contact surface at the joining portion by the mechanism described above, so that a joining strength higher than the base material strength can be realized. The shoulder depth is preferably 0.05 to 0.5 mm. If the shoulder depth is too large, the resin may be repelled at the shoulder and burr may occur. If the shoulder depth is too small, the shoulder portion cannot hold the resin and a groove is formed at the joint. As shown in Table 1, the shoulder depth is preferably 0.2.
It is preferably 5 mm or less, more preferably 0.1 mm or less.

【0024】[0024]

【表1】 以上のように、熱可塑性樹脂同士を当接させ、その表面
境界線の所定部分を含む樹脂表面に回転するプローブを
押し当てて表面境界線に沿って移動させることによって
バリが発生しない接合が実現できる。また繊維強化樹脂
の場合にはバリの発生を防止できると同時に高強度の接
合を実現できる。
[Table 1] As described above, the thermoplastic resin is brought into contact with each other, and the rotating probe is pressed against the resin surface including the predetermined part of the surface boundary line and moved along the surface boundary line to realize the bonding without burr. it can. Further, in the case of the fiber reinforced resin, it is possible to prevent the occurrence of burrs and at the same time realize high strength bonding.

【0025】なお、実施例ではプローブの回転数を23
0rpmで行ったが、特に限定されず、摩擦熱により樹
脂を溶融できる回転数以上であればよい。摩擦熱の熱量
は撹拌子の形状によるので、一義的ではないが、実施例
の撹拌子形状では200〜500rpmが望ましい。2
00rpmより小さいと発熱量が十分でなく樹脂の溶融
が不十分で接合が不十分となり、500rpmより大き
いと摩擦熱が大きくなりすぎ、材料が逃げたり軟化する
場合があるし、ひどい場合は樹脂の発泡や酸化分解など
が起こりやすくなり、表面が凹凸した外観のものとな
り、接合部の接合内部品質も得られない。前進角につい
ても特に限定されないが、0.5〜1.5°が望まし
い。
In the embodiment, the number of rotations of the probe is set to 23.
Although the rotation speed was 0 rpm, the rotation speed is not particularly limited as long as it is equal to or higher than the rotation speed at which the resin can be melted by friction heat. The amount of frictional heat is not unique because it depends on the shape of the stirrer, but is preferably 200 to 500 rpm in the stirrer shape of the example. Two
If it is less than 00 rpm, the calorific value is not sufficient and the resin is insufficiently melted to result in insufficient joining, and if it is more than 500 rpm, the frictional heat becomes too large, and the material may escape or soften. Foaming and oxidative decomposition are likely to occur, the surface has an uneven appearance, and the internal quality of the joint cannot be obtained. The advancing angle is also not particularly limited, but is preferably 0.5 to 1.5 °.

【0026】実施例2〜4では第1熱可塑性樹脂部材、
第2熱可塑性樹脂部材とも繊維強化樹脂の場合を示した
が、いずれか一方が繊維強化樹脂であれば同様の効果を
奏する。
In Examples 2 to 4, the first thermoplastic resin member,
Although the case where both the second thermoplastic resin members are fiber reinforced resins is shown, the same effect can be obtained if either one is fiber reinforced resin.

【0027】プローブの材質および表面処理や形状は、
被接合材である樹脂の種類や強化繊維の種類および量と
接合部の厚みなどに関係するため適切に設定すればよ
い。シャフト部、ショルダ部、撹拌子部の形状も用途に
合わせて適切に設定すればよい。シャフト部と撹拌子部
は一体であってもよいし、別体を繋ぎ合わせてもよい。
撹拌子部の撹拌子出代は、接合対象の樹脂の厚さの85
%以下が望ましい。85%より大きい場合は樹脂が溶け
落ちてしまい、撹拌した樹脂を保持できない問題があ
る。
The material, surface treatment and shape of the probe are
It may be appropriately set because it is related to the type and amount of the resin as the material to be joined, the type and amount of the reinforcing fiber, and the thickness of the joined portion. The shapes of the shaft portion, the shoulder portion, and the stirring bar portion may be appropriately set according to the application. The shaft portion and the stirrer portion may be integrated, or separate bodies may be joined together.
The stirrer extension of the stirrer part is 85
% Or less is desirable. If it is more than 85%, the resin will be melted down and the agitated resin cannot be retained.

【0028】実施例では当接面は平面であるが、特に限
定されず、当接部分の断面が逆位相L型、T字とU字の
組み合わせなど、適宜設定できる。また第1熱可塑性樹
脂部材、第2熱可塑性樹脂部材の形状も平板以外にイン
テークマニホールドのような円筒形状など様々な形状に
適用できる。
In the embodiment, the contact surface is a flat surface, but is not particularly limited, and the cross section of the contact portion can be appropriately set such as an antiphase L type, a combination of T-shape and U-shape. Further, the shapes of the first thermoplastic resin member and the second thermoplastic resin member can be applied to various shapes such as a cylindrical shape like an intake manifold other than the flat plate.

【0029】[0029]

【発明の効果】以上のように、本発明は、第1熱可塑性
樹脂部材と第2熱可塑性樹脂部材を当接後、前記第1熱
可塑性樹脂部材と前記第2熱可塑性樹脂部材との表面境
界線の所定部分を含む前記第1熱可塑性樹脂部材と前記
第2熱可塑性樹脂部材の表面部に回転するプローブを押
し当てて前記表面境界線に沿って移動させることを特徴
とする熱可塑性樹脂部材の接合方法または第1熱可塑性
樹脂部材と第2熱可塑性樹脂部材の少なくとも一方が繊
維強化樹脂からなり、前記第1熱可塑性樹脂部材と前記
第2熱可塑性樹脂部材を当接後、前記第1熱可塑性樹脂
部材と前記第2熱可塑性樹脂部材との表面境界線の所定
部分を含む前記第1熱可塑性樹脂部材と前記第2熱可塑
性樹脂部材の表面部に回転するプローブを押し当てて前
記表面境界線に沿って移動させることを特徴とする繊維
強化熱可塑性樹脂部材の接合方であるので、バリの発生
を防止できるし、繊維強化樹脂の接合にあっては接合強
度も大きくできる。
As described above, according to the present invention, the surfaces of the first thermoplastic resin member and the second thermoplastic resin member are brought into contact with each other after the first thermoplastic resin member and the second thermoplastic resin member are brought into contact with each other. A thermoplastic resin, characterized in that a rotating probe is pressed against the surface portions of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined portion of the boundary line and moved along the surface boundary line. At least one of the joining method of the members or the first thermoplastic resin member and the second thermoplastic resin member is made of fiber reinforced resin, and the first thermoplastic resin member and the second thermoplastic resin member are brought into contact with each other, and then the The rotating probe is pressed against the surface portions of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined portion of the surface boundary line between the first thermoplastic resin member and the second thermoplastic resin member. Along the surface border Since moving it towards the junction of the fiber-reinforced thermoplastic resin member, characterized in Te, to be prevented occurrence of burrs, in the joining of the fiber-reinforced resin bonding strength can be increased.

【図面の簡単な説明】[Brief description of drawings]

【図1】接合前の第1繊維強化樹脂部材と第2繊維強化
樹脂部材を当接した状態を上面から見た断面説明図。
FIG. 1 is an explanatory cross-sectional view of a state in which a first fiber-reinforced resin member and a second fiber-reinforced resin member before joining are in contact with each other as viewed from above.

【図2】接合前の第1繊維強化樹脂部材と第2繊維強化
樹脂部材を当接した状態を側面から見た断面説明図。
FIG. 2 is a cross-sectional explanatory view of a state in which a first fiber-reinforced resin member and a second fiber-reinforced resin member before joining are in contact with each other as seen from a side surface.

【図3】接合中の第1繊維強化樹脂部材と第2繊維強化
樹脂部材を当接した状態を上面から見た断面説明図。
FIG. 3 is an explanatory cross-sectional view of a state in which the first fiber-reinforced resin member and the second fiber-reinforced resin member being joined are in contact with each other as viewed from above.

【図4】接合中の第1繊維強化樹脂部材と第2繊維強化
樹脂部材を当接した状態を側面から見た接合完了部分の
断面説明図。
FIG. 4 is an explanatory cross-sectional view of a joint-completed portion, viewed from the side, showing a state in which the first fiber-reinforced resin member and the second fiber-reinforced resin member being joined are in contact.

【図5】実施例に使用したプローブの断面図。FIG. 5 is a cross-sectional view of a probe used in an example.

【図6】接合中のプローブの状態を説明する説明図。FIG. 6 is an explanatory diagram illustrating a state of the probe during joining.

【図7】振動溶着した部分を側面から見た断面説明図。FIG. 7 is an explanatory cross-sectional view of a vibration welded portion viewed from a side surface.

【符号の説明】[Explanation of symbols]

1…第1熱可塑性樹脂部材 2…第2熱可塑性樹脂部材 5、6…ガラス繊維(繊維) 7…当接面 7a…表面境界線 8…プローブ 1 ... First thermoplastic resin member 2 ... Second thermoplastic resin member 5, 6 ... Glass fiber (fiber) 7 ... Contact surface 7a ... surface boundary line 8 ... Probe

フロントページの続き Fターム(参考) 4F211 AA29 AD05 AD16 AD19 TA01 TC08 TD07 TN20 TQ13 Continued front page    F term (reference) 4F211 AA29 AD05 AD16 AD19 TA01                       TC08 TD07 TN20 TQ13

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 第1熱可塑性樹脂部材と第2熱可塑性樹
脂部材を当接後、前記第1熱可塑性樹脂部材と前記第2
熱可塑性樹脂部材との表面境界線の所定部分を含む前記
第1熱可塑性樹脂部材と前記第2熱可塑性樹脂部材の表
面部に回転するプローブを押し当てて前記表面境界線に
沿って移動させることを特徴とする熱可塑性樹脂部材の
接合方法。
1. A first thermoplastic resin member and a second thermoplastic resin member after contacting the first thermoplastic resin member and the second thermoplastic resin member with each other.
Pressing the rotating probe against the surface portions of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined portion of the surface boundary line with the thermoplastic resin member and moving the probe along the surface boundary line. A method for joining thermoplastic resin members, comprising:
【請求項2】 第1熱可塑性樹脂部材と第2熱可塑性樹
脂部材の少なくとも一方が繊維強化樹脂からなり、前記
第1熱可塑性樹脂部材と前記第2熱可塑性樹脂部材を当
接後、前記第1熱可塑性樹脂部材と前記第2熱可塑性樹
脂部材との表面境界線の所定部分を含む前記第1熱可塑
性樹脂部材と前記第2熱可塑性樹脂部材の表面部に回転
するプローブを押し当てて前記表面境界線に沿って移動
させることを特徴とする繊維強化熱可塑性樹脂部材の接
合方法。
2. At least one of the first thermoplastic resin member and the second thermoplastic resin member is made of a fiber reinforced resin, and after contacting the first thermoplastic resin member and the second thermoplastic resin member, The rotating probe is pressed against the surface portions of the first thermoplastic resin member and the second thermoplastic resin member including a predetermined portion of the surface boundary line between the first thermoplastic resin member and the second thermoplastic resin member. A method for joining fiber-reinforced thermoplastic resin members, characterized by moving along a surface boundary line.
JP2001344818A 2001-11-09 2001-11-09 Method for connecting thermoplastic resin member and method for connecting fiber-reinforced thermoplastic resin member Pending JP2003145625A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001344818A JP2003145625A (en) 2001-11-09 2001-11-09 Method for connecting thermoplastic resin member and method for connecting fiber-reinforced thermoplastic resin member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2001344818A JP2003145625A (en) 2001-11-09 2001-11-09 Method for connecting thermoplastic resin member and method for connecting fiber-reinforced thermoplastic resin member

Publications (1)

Publication Number Publication Date
JP2003145625A true JP2003145625A (en) 2003-05-20

Family

ID=19158280

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP2003145625A (en)

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JP2008162280A (en) * 2006-12-29 2008-07-17 General Electric Co <Ge> Fiber-reinforced thermoplastic resin friction stirring joining
WO2009127981A2 (en) * 2008-04-15 2009-10-22 Eads Deutschland Gmbh Object with a welded seam, method for producing an object and a friction stirring tool and a device for friction stirring
WO2010067796A1 (en) * 2008-12-09 2010-06-17 日本軽金属株式会社 Method for joining resin member with metal member, and liquid-cooled jacket manufacturing method
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008162280A (en) * 2006-12-29 2008-07-17 General Electric Co <Ge> Fiber-reinforced thermoplastic resin friction stirring joining
WO2009127981A2 (en) * 2008-04-15 2009-10-22 Eads Deutschland Gmbh Object with a welded seam, method for producing an object and a friction stirring tool and a device for friction stirring
WO2009127981A3 (en) * 2008-04-15 2010-01-28 Eads Deutschland Gmbh Object with a welded seam, method for producing an object and a friction stirring tool and a device for friction stirring
WO2010067796A1 (en) * 2008-12-09 2010-06-17 日本軽金属株式会社 Method for joining resin member with metal member, and liquid-cooled jacket manufacturing method
US9333703B2 (en) 2011-06-27 2016-05-10 Airbus Operations Gmbh Method and device for bonding parts to be joined, as well as component
EP2540476A1 (en) * 2011-06-27 2013-01-02 Airbus Operations GmbH Method and device for bonding parts to be joined, as well as component
US9561617B2 (en) 2011-06-27 2017-02-07 Airbus Operations Gmbh Devices for bonding parts to be joined
JP2015133350A (en) * 2014-01-09 2015-07-23 ダイヤモンド電機株式会社 Ignition coil for internal combustion engine
US10065362B2 (en) 2014-03-27 2018-09-04 Toyota Jidosha Kabushiki Kaisha Joining method
JP2015186869A (en) * 2014-03-27 2015-10-29 トヨタ自動車株式会社 Bonding method
WO2015145251A1 (en) 2014-03-27 2015-10-01 Toyota Jidosha Kabushiki Kaisha Joining method
TWI650228B (en) * 2014-03-27 2019-02-11 豐田自動車股份有限公司 Joining method
EP3034276A1 (en) * 2014-12-19 2016-06-22 Airbus Defence and Space GmbH Component with firmly bonded connection and a joining method
US20160176102A1 (en) * 2014-12-19 2016-06-23 Airbus Defence and Space GmbH Component having an integral bond and a joining method
US10018210B2 (en) 2014-12-19 2018-07-10 Airbus Defence and Space GmbH Component having an integral bond and joining method
US10183446B2 (en) 2014-12-19 2019-01-22 Airbus Defence and Space GmbH Component having an integral bond and a joining method
EP3088163A1 (en) * 2015-04-29 2016-11-02 Airbus Defence and Space GmbH Friction stir welding of thermoplastics
US10456985B2 (en) 2015-04-29 2019-10-29 Airbus Defence and Space GmbH Friction stir welding of thermoplastics
EP4159415A1 (en) * 2021-09-29 2023-04-05 Airbus (S.A.S.) Method for joining fibre reinforced composite parts using friction stir welding along a butt joint, aircraft component and aircraft

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