JPS60225735A - Joining of heterogeneous synthetic resin material - Google Patents
Joining of heterogeneous synthetic resin materialInfo
- Publication number
- JPS60225735A JPS60225735A JP59084613A JP8461384A JPS60225735A JP S60225735 A JPS60225735 A JP S60225735A JP 59084613 A JP59084613 A JP 59084613A JP 8461384 A JP8461384 A JP 8461384A JP S60225735 A JPS60225735 A JP S60225735A
- Authority
- JP
- Japan
- Prior art keywords
- synthetic resin
- resin materials
- joining
- melt
- plate members
- 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
Links
- 239000000463 material Substances 0.000 title claims abstract description 74
- 229920003002 synthetic resin Polymers 0.000 title claims abstract description 67
- 239000000057 synthetic resin Substances 0.000 title claims abstract description 67
- 238000000034 method Methods 0.000 claims abstract description 27
- 239000000155 melt Substances 0.000 claims abstract description 13
- 230000002745 absorbent Effects 0.000 claims 1
- 239000002250 absorbent Substances 0.000 claims 1
- 239000007789 gas Substances 0.000 description 12
- -1 polypropylene Polymers 0.000 description 9
- 239000004743 Polypropylene Substances 0.000 description 8
- 229920001155 polypropylene Polymers 0.000 description 8
- 229920005989 resin Polymers 0.000 description 8
- 239000011347 resin Substances 0.000 description 8
- 239000012768 molten material Substances 0.000 description 6
- 239000000853 adhesive Substances 0.000 description 5
- 230000001070 adhesive effect Effects 0.000 description 5
- 229910052779 Neodymium Inorganic materials 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 4
- 229920002285 poly(styrene-co-acrylonitrile) Polymers 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 3
- 239000013307 optical fiber Substances 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229920013716 polyethylene resin Polymers 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000009751 slip forming Methods 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- CPBQJMYROZQQJC-UHFFFAOYSA-N helium neon Chemical compound [He].[Ne] CPBQJMYROZQQJC-UHFFFAOYSA-N 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 229910052743 krypton Inorganic materials 0.000 description 1
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- SCUZVMOVTVSBLE-UHFFFAOYSA-N prop-2-enenitrile;styrene Chemical compound C=CC#N.C=CC1=CC=CC=C1 SCUZVMOVTVSBLE-UHFFFAOYSA-N 0.000 description 1
- 239000010979 ruby Substances 0.000 description 1
- 229910001750 ruby Inorganic materials 0.000 description 1
- 229920000638 styrene acrylonitrile Polymers 0.000 description 1
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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- 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
-
- 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
- B29C65/1677—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
- B29C65/74—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
- B29C65/747—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using other than mechanical means
- B29C65/7473—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using other than mechanical means using radiation, e.g. laser, for simultaneously welding and severing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0246—Cutting or perforating, e.g. burning away by using a laser or using hot air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined
- B29C66/30325—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the 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
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
-
- 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
- B29C66/82—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps
- B29C66/826—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined
- B29C66/8266—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- 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
- B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
- B29K2023/10—Polymers of propylene
- B29K2023/12—PP, i.e. polypropylene
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Health & Medical Sciences (AREA)
- Electromagnetism (AREA)
- Toxicology (AREA)
- Fluid Mechanics (AREA)
- Thermal Sciences (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、異種の合成樹脂材料を重ね合わせ、その両者
をレーザ光によって接合させる方法に関するものである
。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a method of superimposing different types of synthetic resin materials and bonding them together using a laser beam.
従来、合成樹脂材料と合成樹脂材料とを接合する際には
、熱を加えて溶着する物理的接合方法と接着剤を用いて
接着する化学的接合方法が広く利用されている。Conventionally, when joining synthetic resin materials, a physical joining method in which heat is applied to weld them, and a chemical joining method in which they are joined together using an adhesive have been widely used.
すなわち、前者の物理的接合方法は、接合しようとする
合成樹脂材料の接合面でメタルメソシュ等の発熱体を発
熱させて両者の合成樹脂材料の接合面を溶融さセつつ加
圧・冷却し、両合成樹脂材料を接合する方法である。ま
た、後者の化学的接合方法は、接合しようとする合成樹
脂材料の接合面にホットメルト等の接着剤を介在させ、
一方の合成樹脂材料の表面から高周波または超音波を付
与させて接着剤を加熱・溶融させた後、両者の合成樹脂
材料を加圧しつつ冷却し、両合成樹脂材料を接合する方
法である。In other words, the former physical joining method involves heating a heating element such as a metal mesh on the joint surfaces of the synthetic resin materials to be joined, melting the joining surfaces of both synthetic resin materials, and pressurizing and cooling them. This is a method of joining synthetic resin materials. In addition, the latter chemical bonding method involves interposing an adhesive such as hot melt on the bonding surfaces of the synthetic resin materials to be bonded.
In this method, high frequency or ultrasonic waves are applied to the surface of one synthetic resin material to heat and melt the adhesive, and then both synthetic resin materials are cooled while being pressurized to join both synthetic resin materials.
しかし、前者の物理的接合方法においては、同種の合成
樹脂材料を接合する際には接合しようとする両者の合成
樹脂材料の溶融温度が同一であるとともに、相溶性を有
するので、両合成樹脂材料の接合には適しているが、異
種の合成樹脂材料を接合する際には両者の合成樹脂材料
の溶融温度が異なるとともに、相溶性が悪いことから、
両合成樹脂材料の接合は困難である。また、後者の化学
的接合方法においては、同種の合成樹脂材料を接合する
際には前者の物理的接合方法と同様に適しているが、異
種の合成樹脂材料を接合する際には合成樹脂材料の材質
によって接着剤の接着力が低下し、両合成樹脂材料を強
固に接合することは困難である。However, in the former physical joining method, when joining synthetic resin materials of the same type, both synthetic resin materials have the same melting temperature and are compatible, so both synthetic resin materials are However, when joining different types of synthetic resin materials, the melting temperatures of the two synthetic resin materials are different and the compatibility is poor.
It is difficult to join both synthetic resin materials. In addition, the latter chemical bonding method is as suitable as the former physical bonding method when bonding synthetic resin materials of the same type, but it is suitable for bonding synthetic resin materials of different types. The adhesive force of the adhesive decreases depending on the material of the material, making it difficult to firmly join both synthetic resin materials.
上述のようなことから、異種の合成樹脂材料を接合する
際には、機械的接合方法が多く利用されている。その代
表例を第１図に示すポリプロピレンとポリエチレンの接
合方法によって説明する。For the reasons described above, mechanical joining methods are often used when joining different types of synthetic resin materials. A typical example thereof will be explained using the method of joining polypropylene and polyethylene shown in FIG.
第１図においては、５１はポリプロピレン樹脂からなる
板部材であって、この板部材５１の下部にはポリエチレ
ン樹脂からなる板部材５２が配設されており、このポリ
エチレン樹脂の板部材５２とポリプロピレン樹脂の板部
材５１とは互いに対向する部位に貫通孔５３ａ、５３ｂ
が形成されている。そして、両板部材５１．５２の貫通
孔５３ａ、５３ｂには上方からパツキン５４をを介在し
て螺子５５が螺合され、両板部材５１．５２が接合され
ている。In FIG. 1, 51 is a plate member made of polypropylene resin, and a plate member 52 made of polyethylene resin is disposed at the bottom of this plate member 51, and this plate member 52 of polyethylene resin and polypropylene resin Through-holes 53a and 53b are formed in opposing parts of the plate member 51.
is formed. Further, screws 55 are screwed into the through holes 53a and 53b of both plate members 51 and 52 from above with a gasket 54 interposed therebetween, thereby joining both plate members 51 and 52.
しかしながら、このような機械的接合方法においては、
両板部材５１．５２に貫通孔５３ａ、５３ｂを形成し、
螺子５５を螺合しなければならず、前記の物理的接合方
法および化学的接合方法に比較して接合作業が煩雑とな
ることはもとより、両板部材５１．５２に貫通孔５３ａ
、５３ｂを形成する必要があることから、画板部材５１
．５２の強度が低下する不具合がある。However, in such mechanical joining methods,
Through holes 53a and 53b are formed in both plate members 51 and 52,
The screws 55 must be screwed together, which makes the joining work more complicated than the above-mentioned physical joining method and chemical joining method.
, 53b, the drawing board member 51
．． There is a problem that the strength of 52 is reduced.
本発明は、上記の不具合を解消するためになされたもの
で、その目的は重ね合わされた合成樹脂材料のうち、上
方の合成樹脂材料の前後関係にレーザ光を照射して加熱
・溶融させ、後方のレーザ光で溶融された溶融物に圧縮
気体を吹き付けて両者の合成樹脂材料に連続して形成さ
れた溝に押し込むことにより、両合成樹脂材料の強度を
低下させることなく、容易に接合することができる異種
合成樹脂材料の接合方法を提供することにある。The present invention was made in order to solve the above-mentioned problems, and its purpose is to irradiate a laser beam to the front and back of the upper synthetic resin material of the stacked synthetic resin materials to heat and melt it, and to By blowing compressed gas onto the molten material melted by laser light and pushing it into the grooves continuously formed in both synthetic resin materials, it is possible to easily join both synthetic resin materials without reducing their strength. The object of the present invention is to provide a method for joining dissimilar synthetic resin materials.
上記の目的を達成するために、本発明に係る異種合成樹
脂材料の接合方法の構成は、異種の合成樹脂材料を重ね
合わせてその両者を接合するにあたり、前記異種の合成
樹脂材料をレーザ光に対して吸収性とし、この両者の合
成樹脂材料を重ね合わせ、上部の合成樹脂材料の上方か
ら前後関係にレーザ光を照射し、前方のレーザ光で両者
の合成樹脂材料を溶融せしめて連続した溝を形成すると
ともに、後方のレーザ光で上方の合成樹脂材料を幅広に
溶融せしめ、その溶融部位に圧縮気体を吹き付けてその
溶融物を前記両者の合成樹脂材料に形成された連続した
溝に押し込み、再溶融物を互いに絡み合わせるようにし
たものである。In order to achieve the above object, the structure of the method for joining different types of synthetic resin materials according to the present invention is such that when overlapping different types of synthetic resin materials and joining them, the different types of synthetic resin materials are exposed to laser light. The two synthetic resin materials are superimposed, and a laser beam is irradiated from above the upper synthetic resin material in front and back, and the front laser beam melts both synthetic resin materials to form continuous grooves. At the same time, the upper synthetic resin material is melted in a wide range using a rear laser beam, and compressed gas is blown onto the melted area to force the melted material into continuous grooves formed in both synthetic resin materials. The remelted material is made to intertwine with each other.
そして、重ね合わされるレーザ光に対して吸収性の合成
樹脂材料としては、カーボンブランク等の補助材料が添
加されたポリプロピレン樹脂、ガラス繊維で強化され、
かつカーボンブランクが添加されたスチレン−アクリロ
ニトリル共重合体等を挙げることができる。そして、こ
れらの合成樹脂材料は、上部および下部に配置する組み
合わせにおいて自由に選択して接合させることができる
。The synthetic resin material that absorbs the superimposed laser beams is reinforced with polypropylene resin and glass fiber to which auxiliary materials such as carbon blank are added.
Examples include styrene-acrylonitrile copolymer to which carbon blank is added. These synthetic resin materials can be freely selected and bonded in combinations arranged in the upper and lower parts.
また、異種合成樹脂材料の接合時に使用されるレーザと
しては、ガラス：ネオジウムトレーザ、ＹＡＧ：ネオジ
ウム３“レーザ、ルビーレーザ、ヘリウム−ネオンレー
ザ、クリプトンレーザ、アルゴンレーザ、Ｈ２レーザ、
Ｎ２レーザ等を挙げることができ、このうち、特にＹＡ
Ｃ； ：ネオジウム３゛レーザが最も適している。In addition, lasers used when joining dissimilar synthetic resin materials include glass: neodymium laser, YAG: neodymium 3" laser, ruby laser, helium-neon laser, krypton laser, argon laser, H2 laser,
Examples include N2 laser, among which YA laser
C;: Neodymium 3° laser is most suitable.
また、異種合成樹脂材料の接合時に用いられるレーザの
波長としては、接合する合成樹脂材料に適合した波長が
必要であって１．０６μｍ以下が最も優れており、その
波長が１．０６μｍ以上の場合には異種の合成樹脂材料
を溶融させて接合することは不可能である。また、レー
ザの出力においては、５Ｗないし３０Ｗが適しており、
その出力が５Ｗ以下の場合には異種の合成樹脂材料を溶
融させることができず、３０Ｗ以上の場合には異種の合
成樹脂材料が蒸発したり、変質したりして接合が不可能
である。In addition, the wavelength of the laser used when joining dissimilar synthetic resin materials needs to be compatible with the synthetic resin materials to be joined, and a wavelength of 1.06 μm or less is best; It is impossible to melt and join different types of synthetic resin materials. In addition, 5W to 30W is suitable for the laser output.
If the output is less than 5 W, different types of synthetic resin materials cannot be melted, and if the output is more than 30 W, the different types of synthetic resin materials will evaporate or change in quality, making it impossible to join them.
以下、本発明の一実施例を図面に基づいて詳細に説明す
る。Hereinafter, one embodiment of the present invention will be described in detail based on the drawings.
第２図は本発明に係る異種合成樹脂材料の接合方法を説
明する概略側断面図、第３図は本発明に係る異種合成樹
脂材料の接合方法を説明する概略正断面図を示すもので
ある。FIG. 2 is a schematic side sectional view illustrating the method for joining dissimilar synthetic resin materials according to the present invention, and FIG. 3 is a schematic front sectional view illustrating the method for joining dissimilar synthetic resin materials according to the present invention. .
第２図および第３図の（ａ）ないしくｄ）において、１
はガラス繊維が添加されて強化されたスチレン−アクリ
ロニトリル共重合体からなる板部材であって、この板部
材１の原材料色はカーボンブランクが添加されて黒色と
なっており、１．０６μｍ以下のレーザ光に対して吸収
性の性質を有している。In (a) to d) of Figures 2 and 3, 1
is a plate member made of styrene-acrylonitrile copolymer reinforced by adding glass fiber, and the raw material color of this plate member 1 is black due to the addition of carbon blank. It has the property of absorbing light.
また、板部材１の上部にはポリプロピレン樹脂からなる
板部材２が配設されており、その下面は平坦に形成され
、板部材１の接触面１ａに当接する接触面２ａとなって
いる。そして、この板部材２の原材料色はカーボンブラ
ックが添加されて黒色となっており、１．０６μｍ以下
のレーザ光に対して吸収性の性質を有している。Further, a plate member 2 made of polypropylene resin is arranged on the upper part of the plate member 1, and its lower surface is formed flat and serves as a contact surface 2a that comes into contact with the contact surface 1a of the plate member 1. The raw material color of this plate member 2 is black due to the addition of carbon black, and has the property of absorbing laser light of 1.06 μm or less.
そして、上述のような異種合成樹脂材料からなる板部材
１．２を接合する際には、第３図の（ａ）に示すように
ポリプロピレン樹脂からなる板部材２の接触面２ａをス
チレン−アクリロニトリル共重合体からなる板部材１の
接触面１ａに重ね合わせる。When joining the plate members 1.2 made of different synthetic resin materials as described above, the contact surface 2a of the plate member 2 made of polypropylene resin is coated with styrene-acrylonitrile, as shown in FIG. 3(a). It is superimposed on the contact surface 1a of the plate member 1 made of a copolymer.
次に、第２図に示すように上部の合成樹脂材料の上方に
、ＹＡＧ ：ネオジウム３゛レーザ発振器と（図示せず
）に接続され、しかも、その内部に石英光ファイバ（図
示せず）で接続された二つの照射ノズル３ａ、３ｂを前
後関係に配設する。その際、前方の照射ノズル３ａの先
端を板部材２の表面に可及的に接近させて位置させると
ともに、後方の照射ノズル３ｂの先端を前方の照射ノズ
ル３ａよりも板部材２の表面から離して位置させる。Next, as shown in Fig. 2, above the upper synthetic resin material, a YAG:neodymium 3゜ laser oscillator (not shown) is connected, and a quartz optical fiber (not shown) is installed inside it. Two connected irradiation nozzles 3a and 3b are arranged in front-and-back relationship. At this time, the tip of the front irradiation nozzle 3a is positioned as close as possible to the surface of the plate member 2, and the tip of the rear irradiation nozzle 3b is positioned farther from the surface of the plate member 2 than the front irradiation nozzle 3a. position.
その後、前方の照射ノズル３ａから第３図（ｂ）に示す
ように波長が１．０６μｍ、出力が３０ＷのＹＡＧレー
ザ光４ａを石英光ファイバ内に通過させて照射すると同
時に、後方の照射ノズル３ｂから第３図＜ｃ＞に示すよ
うに波長が１．０６μｍ、出力が８ＷのＹＡＧレーザ光
４ｂを石英光ファイバ内に通過させてレーザ光４ａより
も広範囲に照射しつつ、画板部材１．２の長手方向に移
行させる。Thereafter, as shown in FIG. 3(b), a YAG laser beam 4a with a wavelength of 1.06 μm and an output of 30 W is passed through the quartz optical fiber and irradiated from the front irradiation nozzle 3a, and at the same time, the rear irradiation nozzle 3b As shown in FIG. 3<c>, a YAG laser beam 4b with a wavelength of 1.06 μm and an output of 8W is passed through a quartz optical fiber to irradiate a wider area than the laser beam 4a, while the drawing board member 1.2 Shift in the longitudinal direction.
その際、前方の照射ノズル３ａから照射されるＹＡＧレ
ーザ光４ａはレーザ光４ｂよりも狭い範囲で、両板部材
１．２の照射位置に高いエネルギとして蓄積されるとと
もに、そのエネルギによって画板部材ｌ、２が加熱され
、その部位が溶融される。これによって画板部材１．２
のそれぞれに溶融物１ｂ、２ｂが形成されるとともに、
画板部材１．２に連続した溝５が形成される。一方、後
方の照射ノズル３ｂから照射されるＹＡＧレーザ光４ｂ
は４ａよりも広範囲を照射しエネルギは低出力であり、
主に上部の板部材２の照射位置にエネルギとして蓄積さ
れるとともに、そのエネルギによって上部の板部材２が
加熱され、その部位が溶融されて溶融物２ｃが形成され
る。At this time, the YAG laser beam 4a irradiated from the front irradiation nozzle 3a is accumulated as high energy at the irradiation position of both plate members 1.2 in a narrower range than the laser beam 4b, and the energy is used to , 2 is heated to melt that part. As a result, the drawing board member 1.2
Melts 1b and 2b are formed in each of
A continuous groove 5 is formed in the drawing board member 1.2. On the other hand, YAG laser light 4b irradiated from the rear irradiation nozzle 3b
irradiates a wider area than 4a and has lower energy output,
The energy is mainly accumulated at the irradiation position of the upper plate member 2, and the upper plate member 2 is heated by the energy, and that portion is melted to form a molten material 2c.
また、ＹＡＧレーザ光４ａ、４ｂの照射と同時に、空気
、ガス、空気およびガスの混合気体等からなる圧縮気体
の供給源（図示せず）に接続されている二つのバイブロ
ａ、６ｂを後方の照射ノズル３ｂの両側方に配置させる
とともに、両者のバイブロａ、６ｂの先端を板部材２の
溶融部位の上方に位置させる。その後、各バイブロａ、
６ｂに設けられているバルブ７ａ、７ｂを開放させて圧
縮気体を溶融物２Ｃの上方から吹き付けるとともに、照
射ノズル３ｂに追随して移行させる。Simultaneously with the irradiation of the YAG laser beams 4a and 4b, two vibros a and 6b connected to a compressed gas supply source (not shown) consisting of air, gas, a mixture of air and gas, etc. They are arranged on both sides of the irradiation nozzle 3b, and the tips of both vibros a and 6b are located above the melting part of the plate member 2. After that, each vibro a,
Valves 7a and 7b provided at 6b are opened to blow compressed gas from above the melt 2C, and the gas is caused to follow the irradiation nozzle 3b.
その際、板部材２の溶融物２Ｃが吹き付けられた圧縮気
体によって、両板部材１．２の先に形成される連続した
溝５に押し込まれ、先の溶融物１ｂ、２ｂと互いにぶつ
かり合う。この時、三者の溶融物１ｂ、２ｂ、２Ｃが互
いに押し付は合うとともに、その一部が絡み合う。At this time, the molten material 2C of the plate member 2 is pushed into the continuous groove 5 formed at the ends of both plate members 1.2 by the blown compressed gas, and collides with the previous molten material 1b, 2b. At this time, the three molten materials 1b, 2b, and 2C are pressed against each other, and some of them are intertwined.
そして、画板部材１．２への所望とする長さのＹＡＧレ
ーザ光４ａ、４ｂの照射と圧縮気体の吹き付けが終了し
た後、両照射ノズル３ａ、３ｂからのＹＡＧレーザ光４
ａ、４ｂの照射と両バイブロａ、６ｂからの圧縮気体の
吹き付けを停止するとともに、両照射ノズル３ａ、３ｂ
と両バイブロａ、６ｂを両板部材ｌ、２の上方から後退
させる。After the irradiation of the YAG laser beams 4a, 4b of the desired length to the drawing board member 1.2 and the spraying of the compressed gas are completed, the YAG laser beams 4a and 4b are emitted from both the irradiation nozzles 3a and 3b.
At the same time, the irradiation of the vibros a and 4b and the spraying of compressed gas from both the vibros a and 6b are stopped, and both the irradiation nozzles 3a and 3b are stopped.
and both vibros a and 6b are retreated from above both plate members l and 2.
これにより、第３図の（ｄ）に示すように画板部材１．
２の溶融物１ｂ、２ｂ、２Ｃが連続的なうねりを生じて
互いに絡み合った状態で硬化し、スチレン−アクリロニ
トリル共重合体からなる板部材１とポリプロピレン樹脂
からなる板部材２とが強固に接合される。そして、両板
部材１．２の接合強度は、照射ノズル３ａ、３ｂからの
ＹＡＧレーザ光４ａ、４ｂの単位時間当りの照射面積と
照射ノズル３ａ、３ｂの移行速度によって調整すること
ができる。As a result, as shown in FIG. 3(d), the drawing board member 1.
The melts 1b, 2b, and 2C of 2 are cured in a state in which they form continuous undulations and are intertwined with each other, and the plate member 1 made of styrene-acrylonitrile copolymer and the plate member 2 made of polypropylene resin are firmly joined. Ru. The bonding strength between both plate members 1.2 can be adjusted by the irradiation area per unit time of the YAG laser beams 4a, 4b from the irradiation nozzles 3a, 3b and the transfer speed of the irradiation nozzles 3a, 3b.
Ｃ発明の効果〕
以上説明したように、本発明に係る異種合成樹脂材料の
接合方法においては、重ね合わされた合成樹脂材料のう
ち、上方の合成樹脂材料の前後関係にレーザ光を照射し
て加熱・溶融させ、後方のレーザ光で溶融された溶融部
位に圧縮気体を吹き付けてその溶融物を両者の合成樹脂
材料に連続して形成された溝に押し込むようにしたから
、両者の溶融物が互いに絡み合った状態で硬化するので
、合成樹脂材料の強度を低下させることなく、強固に接
合させることができる効果がある。C. Effects of the Invention] As explained above, in the method for joining dissimilar synthetic resin materials according to the present invention, laser light is irradiated to the front and back of the upper synthetic resin material among the superimposed synthetic resin materials to heat it.・The molten parts were melted and compressed gas was blown onto the molten part melted by the rear laser beam, and the molten material was forced into the grooves continuously formed in both synthetic resin materials, so the molten parts of both materials could not touch each other. Since they are cured in an intertwined state, they have the effect of making it possible to firmly bond the synthetic resin material without reducing its strength.
また、本発明においては、重ね合わされた合成樹脂材料
の上方からレーザ光の照射と圧縮気体の吹き付けを行う
ことによって、再合成樹脂材料が接合されるので、従来
の機械的接合方法に比較して、異種の合成樹脂材料の接
合を容易に行うことができる効果がある。In addition, in the present invention, resynthetic resin materials are joined by irradiating laser light and spraying compressed gas from above the superimposed synthetic resin materials, which is superior to conventional mechanical joining methods. This has the effect that different types of synthetic resin materials can be easily joined.
第１図は従来の異種合成樹脂材料の機械的接合方法を説
明する概略断面図である。
第２図は本発明に係る異種合成樹脂材料の接合方法を説
明する概略側断面図である。
第３図は本発明に係る異種合成樹脂材料の接合方法を説
明する概略正断面図である。
１−−−−−−ガラス繊維で強化されたスチレン−アク
リロニトリル共重合体からなる板部材
１ ａ−−−−一接触面
１ ｂ−−−−一溶融物
２−−−−−ポリプロピレン樹脂からなる板部材２ ａ
−−−−−接触面
２ｂ、２ ｃ −−−−一溶融物
３ａ、３ ｂ−−−−−一照射ノズル
４ ａ 、 ４ ｂ −−−−Ｙ Ａ Ｇ レーザ光５
−−−−−−一連続した溝
６ ａ 、 ６ ｂ−−−−−−−パイプ７ ａ 、
７ ｂ−−−−−バルブ
第１図
第２図
１
（ａ）
ｂ
（Ｃ）
第
（ｂ）
３図FIG. 1 is a schematic cross-sectional view illustrating a conventional mechanical joining method of dissimilar synthetic resin materials. FIG. 2 is a schematic side sectional view illustrating the method of joining different types of synthetic resin materials according to the present invention. FIG. 3 is a schematic front sectional view illustrating the method of joining different synthetic resin materials according to the present invention. 1------Plate member 1 made of styrene-acrylonitrile copolymer reinforced with glass fibers a----1 contact surface 1 b----1 melt 2---- Made of polypropylene resin Plate member 2 a
----Contact surfaces 2b, 2c ----1 Melt 3a, 3 b---1 Irradiation nozzles 4 a, 4b ----Y A G Laser beam 5
--------One continuous groove 6a, 6b------Pipe 7a,
7 b ---- Valve Fig. 1 Fig. 2 Fig. 1 (a) b (C) Fig. (b) 3
Claims (1)
にあたり、前記異種の合成樹脂材料をレーザ光に対して
吸収性とし、この両者の合成樹脂材料を重ね合わせ、上
部の合成樹脂材料の上方から前後関係にレーザ光を照射
し、前方のレーザ光で両者の合成樹脂材料を溶融せしめ
て連続した溝を形成するとともに、後方のレーザ光で上
方の合成樹脂材料を幅広に溶融せしめ、その溶融部位に
圧縮気体を吹き付けてその溶融物を前記両者の合成樹脂
材料に形成された連続した溝に押し込み、両港融物を互
いに絡み合わせるようにしたことを特徴とする異種合成
樹脂材料の接合方法。In the process of overlapping different types of synthetic resin materials and joining them together, the different types of synthetic resin materials are made absorbent to laser light, and both synthetic resin materials are overlapped, and the upper synthetic resin material is placed above the upper synthetic resin material. A laser beam is irradiated from the front to the front, and the front laser beam melts the synthetic resin material on both sides to form a continuous groove, and the rear laser beam melts the upper synthetic resin material in a wide range. A method for joining dissimilar synthetic resin materials, characterized in that compressed gas is sprayed onto the parts and the melt is pushed into continuous grooves formed in both synthetic resin materials, thereby intertwining the two melts with each other. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59084613A JPS60225735A (en) | 1984-04-25 | 1984-04-25 | Joining of heterogeneous synthetic resin material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59084613A JPS60225735A (en) | 1984-04-25 | 1984-04-25 | Joining of heterogeneous synthetic resin material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS60225735A true JPS60225735A (en) | 1985-11-11 |
Family
ID=13835543
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59084613A Pending JPS60225735A (en) | 1984-04-25 | 1984-04-25 | Joining of heterogeneous synthetic resin material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60225735A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2678686A1 (en) * | 1991-07-05 | 1993-01-08 | Lidis Sa | Method for assembly by means of grooving (channelling) |
| JP2020138484A (en) * | 2019-02-28 | 2020-09-03 | 学校法人金沢工業大学 | Laser welding method and laser welding system |
| US11454480B1 (en) | 2019-06-12 | 2022-09-27 | Corvid Technologies LLC | Methods for forming munitions casings and casings and munitions formed thereby |
| DE102018120787B4 (en) | 2017-08-28 | 2023-07-20 | GM Global Technology Operations LLC | Process for laser welding non-permeable composite materials |
-
1984
- 1984-04-25 JP JP59084613A patent/JPS60225735A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2678686A1 (en) * | 1991-07-05 | 1993-01-08 | Lidis Sa | Method for assembly by means of grooving (channelling) |
| DE102018120787B4 (en) | 2017-08-28 | 2023-07-20 | GM Global Technology Operations LLC | Process for laser welding non-permeable composite materials |
| JP2020138484A (en) * | 2019-02-28 | 2020-09-03 | 学校法人金沢工業大学 | Laser welding method and laser welding system |
| US11454480B1 (en) | 2019-06-12 | 2022-09-27 | Corvid Technologies LLC | Methods for forming munitions casings and casings and munitions formed thereby |
| US11747122B1 (en) | 2019-06-12 | 2023-09-05 | Corvid Technologies LLC | Methods for forming munitions casings and casings and munitions formed thereby |
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