JPS59174315A - Method of uniting fiber reinforced resin material - Google Patents

Method of uniting fiber reinforced resin material

Info

Publication number
JPS59174315A
JPS59174315A JP4944283A JP4944283A JPS59174315A JP S59174315 A JPS59174315 A JP S59174315A JP 4944283 A JP4944283 A JP 4944283A JP 4944283 A JP4944283 A JP 4944283A JP S59174315 A JPS59174315 A JP S59174315A
Authority
JP
Japan
Prior art keywords
reinforcing fibers
materials
reinforced resin
resin materials
fiber reinforced
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
JP4944283A
Other languages
Japanese (ja)
Other versions
JPS6227661B2 (en
Inventor
Masayoshi Kureishi
暮石　正義
Kazuhiro Nohara
和宏 野原
Shinji Sakahata
坂端　伸治
Shiyouichi Kitagawa
彰一 北側
Yasuo Hirai
靖男 平井
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.)
Hitachi Zosen Corp
Original Assignee
Hitachi Zosen Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Zosen Corp filed Critical Hitachi Zosen Corp
Priority to JP4944283A priority Critical patent/JPS59174315A/en
Publication of JPS59174315A publication Critical patent/JPS59174315A/en
Publication of JPS6227661B2 publication Critical patent/JPS6227661B2/ja
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16—Laser beams
    • B29C65/1629—Laser beams characterised by the way of heating the interface
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16—Laser beams
    • B29C65/1629—Laser beams characterised by the way of heating the interface
    • B29C65/1654—Laser beams characterised by the way of heating the interface scanning at least one of the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16—Laser beams
    • B29C65/1677—Laser beams making use of an absorber or impact modifier
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/70—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/001—Joining in special atmospheres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/001—Joining in special atmospheres
    • B29C66/0012—Joining in special atmospheres characterised by the type of environment
    • B29C66/0014—Gaseous environments
    • B29C66/00141—Protective gases
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114—Single butt joints
    • B29C66/1142—Single butt to butt joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43—Joining a relatively small portion of the surface of said articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/69—General aspects of joining filaments 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72141—Fibres of continuous length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/80—General aspects of machine operations or constructions and parts thereof
    • B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/836—Moving relative to and tangentially to the parts to be joined, e.g. transversely to the displacement of the parts to be joined, e.g. using a X-Y table
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
    • B29K2105/101—Oriented

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

PURPOSE:To improve the strength of the united section of fiber reinforced resin materials, by joining reinforcing fibers projected from the surfaces of the fiber reinforced resin materials, at which the materials are to be united, using a laser beam or a plasma heat source, and then filling the space between said surfaces with a resin. CONSTITUTION:Reinforcing fibers 2 are projected from the surfaces 1A of the fiber reinforced resin materials 1 where they will be united. The fiber reinfored resin materials 1 are opposed to each other with the projected reinforcing fibers 2 from the opposed materials 1 being overlapped. Then the overlapped reinforcing fibers 2 are joined using a laser beam 3 or a plasma heat source. If the materials 1 are thin plates, a microplasma whose arc column in thinner can be used. In this case, an inert gas 4 such as argon or helium is fed adjacent to the sections where uniting is carried out so that said sections can be shielded from the atmosphere. Then after the completion of the joining of the projected reinforcing fibers 2, the space between said surfaces 1A of the reinforced resin materials is filled with a resin to complete the uniting.

Description

【発明の詳細な説明】 本発明は強化繊維樹脂材（Ｅ、Ｒ，Ｐ’）の接合方法に
関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for joining reinforced fiber resin materials (E, R, P').

従来、強化繊維樹脂材どうしの接合方法として、接着剤
による方法、樹脂材間ｌζ樹脂を埋め込む方法等がある
。しかし、いずれの接合方法によっても、接合部の強度
が母材強度に比べてかなり劣るという問題があった。こ
れは、強度を高めるために母材中に配設されている強化
！ａ維どうしが接合部において接合されていないという
理由に基づく。Conventionally, methods of joining reinforcing fiber resin materials include a method using an adhesive, a method of embedding lζ resin between the resin materials, and the like. However, with either joining method, there is a problem in that the strength of the joint is considerably inferior to the strength of the base material. This is reinforced, which is placed in the base material to increase its strength! This is based on the reason that the a fibers are not joined together at the junction.

本発明はこのような問題を解決することを目的とし、強
化繊維樹脂材をその接合面とするところから強化繊維を
突出させた状態で製作し、このように製作した強化繊維
樹脂材を互いの強化繊維の突出部どうしを重ね合せた状
態で対向させ、次に重ね合せた前記強化繊維どうしをレ
ーザ光もしくはプラズマ熱源を用いて接合し、この後強
化繊維樹脂材の接合面間に樹脂の埋め込みを行う構成の
強化繊維樹脂材の接合方法を提供することによって、そ
の目的を達成するものであり、これにより、強化繊維樹
脂材の接合部の強度を従来の方法によるものより高く保
つことができるものである。The purpose of the present invention is to solve these problems by manufacturing reinforced fiber resin materials with reinforcing fibers protruding from their bonding surfaces, and by making the reinforced fiber resin materials manufactured in this way contact each other. The protrusions of the reinforcing fibers are overlapped and faced to each other, and then the overlapped reinforcing fibers are bonded together using a laser beam or a plasma heat source, and then a resin is embedded between the joining surfaces of the reinforcing fiber resin material. This objective is achieved by providing a method for joining reinforced fiber resin materials configured to perform the following steps, and thereby the strength of the joint of reinforced fiber resin materials can be maintained higher than that by conventional methods. It is something.

以下本発明方法の構成を、その一実施例を示す図面に基
づいて詳細に説明する。The configuration of the method of the present invention will be explained in detail below based on the drawings showing one embodiment thereof.

第１図に示すように、先ず、強化繊維樹脂材（１）をそ
の接合面（ＩＡ）とするところから強化繊維（２）を突
出させた状態で製作する。なお、強化繊維樹脂材（１）
の板厚には種々のものがあることは周知の通りで、図は
その一例を示している。As shown in FIG. 1, first, a reinforcing fiber resin material (1) is manufactured with reinforcing fibers (2) protruding from its joint surface (IA). In addition, reinforced fiber resin material (1)
It is well known that there are various plate thicknesses, and the figure shows one example.

次に、第２図に示すように、前記強化繊維樹脂材（１）
を互いの強化繊維（２）の突出部どうしを重ね合せた状
態で対向させる。Next, as shown in FIG. 2, the reinforced fiber resin material (1)
The reinforcing fibers (2) are made to face each other with their protruding parts overlapped with each other.

次に、第８図、第４図（薄板の場合）または第５図、第
６図（厚板の場合）に示すように、重ね合せた強化繊維
（２）の突出部どうしをレーザ光（３）またはプラズマ
熱源（図示せず）を用いて接合する。Next, as shown in Figures 8 and 4 (for thin plates) or Figures 5 and 6 (for thick plates), the protrusions of the overlapped reinforcing fibers (2) are exposed to each other using a laser beam ( 3) or bonding using a plasma heat source (not shown).

薄板の場合はアーク柱の細いマイクロプラズマを用いて
もよい。このとき、アルゴンやヘリウム等の不活性ガス
（４）を接合部近傍に送り込み、大気からシールドする
。なお、第４図はシールドにガラスチャンバー（５）を
用いたところを示しており、係る場合はガラスチャンバ
ー（５）内に不活性ガス（４）を充填しておく。また厚
板の場合は図に示されるように最下１の強化繊維（２）
から順に接合して行くと能率的であり、この場合にもガ
ラスチャンバー（５）を使用してもよいことは明らかで
ある。In the case of thin plates, microplasma with a narrow arc column may be used. At this time, an inert gas (4) such as argon or helium is sent into the vicinity of the joint to shield it from the atmosphere. Note that FIG. 4 shows a glass chamber (5) used as a shield, and in this case, the glass chamber (5) is filled with an inert gas (4). In addition, in the case of a thick plate, as shown in the figure, the bottom 1 reinforcing fiber (2)
It is efficient to join in order from the beginning, and it is clear that the glass chamber (5) may also be used in this case.

このようにして、強化繊維（２）の突出部どうしの接合
を終えると、次に、強化繊維、樹脂材（１）の接合１４
（ＩＡ）間に樹脂の埋め込みを行って作業が完了する。After the protrusions of the reinforcing fibers (2) are joined together in this way, the next step is to join 14 the reinforcing fibers and the resin material (1).
(IA) The work is completed by filling the space with resin.

第７図は、本発明方法に用いると有効なレーザ発振装置
を示す。図において、（６）は接合す之強化繊維樹脂材
（１）の載置台、（７）は該載置台（６）の両側に位置
して設けられたバンク、（８）はバンク（７）上面に沿
って移動自在に構成された一対の第１台車、（９）は第
１台車（８）間にわたって架設されたビーム、ｉｌｌは
ビーム（９）に沿って移動自在に構成された第２台車で
、該第２台車αＯには上下方向に伸縮自在に構成された
集光レンズ移動装置（１１）が取付けられて１）る。な
お、（ロ）は集光レンズ移動装置αυのレーザ光集光レ
ンズである。（至）はビーム（９）の上部に設けられた
レーザ発振器で、該発振器ａ３と前記集光レンズ移動装
置（ロ）との上端部はジャバラ０尋を介して接続されて
いる。FIG. 7 shows a laser oscillation device that is effective when used in the method of the present invention. In the figure, (6) is a mounting table for the reinforced fiber resin material (1) to be joined, (7) is a bank provided on both sides of the mounting table (6), and (8) is a bank (7). A pair of first carts are configured to be movable along the upper surface, (9) is a beam installed between the first carts (8), and ill is a second bogie that is configured to be movable along the beam (9). A condensing lens moving device (11) configured to be vertically expandable and retractable is attached to the second truck αO (1). Note that (b) is the laser beam condensing lens of the condensing lens moving device αυ. (to) is a laser oscillator provided above the beam (9), and the upper end of the oscillator a3 and the condensing lens moving device (b) are connected via a bellows.

係る構成で、レーザ光集光レンズ（２）のＸ方向。With such a configuration, the X direction of the laser beam condensing lens (2).

Ｙ方向、Ｚ方向の三次元移動を、それぞれ、Ｘ方向は第
２台車Ｏｆ３で、Ｙ方向は集光レンズ移動装置ｑ０で、
Ｚ方向は第１台車（８）で行う。このようなレーザ発振
装置を用いれば、前記強化繊維（２）どうしの接合を能
率旧に行うことができる。Three-dimensional movement in the Y direction and Z direction is performed by the second cart Of3 in the X direction and the condensing lens moving device q0 in the Y direction, respectively.
The Z direction is carried out using the first cart (8). If such a laser oscillation device is used, the reinforcing fibers (2) can be joined together efficiently.

以上本発明方法によれば、強化繊維樹脂材の強化繊維ど
うしも接合部において接合するので、接合部の強度を従
来の方法によるものより高く保つことができる。As described above, according to the method of the present invention, since the reinforcing fibers of the reinforcing fiber resin material are bonded to each other at the bonded portions, the strength of the bonded portions can be maintained higher than that by conventional methods.

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

図面は本発明方法の一実施例を示し、第１図は本発明方
法に係る強化繊維樹脂材の斜視図、第２区は第１図の強
化繊維樹脂材を対向させたところの斜視図、第８図〜第
６図は強化繊維樹脂材の接合部側面図、第７図はレーザ
発振装置の全体側面図である。 （１）・・強化繊維樹脂材、（ＩＡ）・・・接合面、（
２）・・・強化繊維、（３）・レーザ光 代理人　介本義弘The drawings show one embodiment of the method of the present invention, and FIG. 1 is a perspective view of the reinforcing fiber resin material according to the method of the present invention, and the second section is a perspective view of the reinforced fiber resin material of FIG. 1 facing each other. 8 to 6 are side views of the joints of the reinforced fiber resin material, and FIG. 7 is a side view of the entire laser oscillation device. (1)...Reinforced fiber resin material, (IA)...Joint surface, (
2) Reinforced fiber, (3) Laser light agent Yoshihiro Keimoto

Claims (1)

【特許請求の範囲】[Claims] １、強化繊維樹脂材をその接合面とするところから強化
繊維を突出させた状態で製作し、このように製作した強
化繊維樹脂材を互いの強化繊維の突出部どうしを重ね合
せた状態で対向させ、次に重ね合せた前記強化繊維どう
しをレーザ光もしくはプラズマ熱源を用いて接合し、こ
の後強化繊維樹脂材の接合面間に樹脂の埋め込みを行う
ことを特徴とする強化繊維樹脂材の接合方法。1. Produce the reinforcing fiber resin material with the reinforcing fibers protruding from the joint surface, and place the reinforcing fiber resin materials produced in this way facing each other with the protruding parts of the reinforcing fibers overlapping each other. and then bonding the superimposed reinforcing fibers to each other using a laser beam or a plasma heat source, and then embedding resin between the joint surfaces of the reinforcing fiber resin materials. Method.
JP4944283A 1983-03-23 1983-03-23 Method of uniting fiber reinforced resin material Granted JPS59174315A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4944283A JPS59174315A (en) 1983-03-23 1983-03-23 Method of uniting fiber reinforced resin material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4944283A JPS59174315A (en) 1983-03-23 1983-03-23 Method of uniting fiber reinforced resin material

Publications (2)

Publication Number Publication Date
JPS59174315A true JPS59174315A (en) 1984-10-02
JPS6227661B2 JPS6227661B2 (en) 1987-06-16

Family

ID=12831232

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4944283A Granted JPS59174315A (en) 1983-03-23 1983-03-23 Method of uniting fiber reinforced resin material

Country Status (1)

Country Link
JP (1) JPS59174315A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2033769A1 (en) * 2007-09-04 2009-03-11 Lm Glasfiber A/S A method of producing a composite structure via intermediate products and a composite structure obtainable by the method
WO2010130438A1 (en) * 2009-05-14 2010-11-18 Lzh Laserzentrum Hannover E.V. Method for joining components

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2033769A1 (en) * 2007-09-04 2009-03-11 Lm Glasfiber A/S A method of producing a composite structure via intermediate products and a composite structure obtainable by the method
WO2009030228A1 (en) * 2007-09-04 2009-03-12 Lm Glasfiber A/S A method of producing a composite structure via intermediate products, the related apparatus and a composite structure obtainable by the method
US9221219B2 (en) 2007-09-04 2015-12-29 Lm Glasfiber A/S Method of producing a composite structure via intermediate products, the related apparatus and a composite structure obtainable by the method
WO2010130438A1 (en) * 2009-05-14 2010-11-18 Lzh Laserzentrum Hannover E.V. Method for joining components
US8591693B2 (en) 2009-05-14 2013-11-26 Lzh Laserzentrum Hannover E.V. Method for joining components

Also Published As

Publication number Publication date
JPS6227661B2 (en) 1987-06-16

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