JP4487110B2 - Laminated body structure and manufacturing method thereof - Google Patents
Laminated body structure and manufacturing method thereof Download PDFInfo
- Publication number
- JP4487110B2 JP4487110B2 JP2000250990A JP2000250990A JP4487110B2 JP 4487110 B2 JP4487110 B2 JP 4487110B2 JP 2000250990 A JP2000250990 A JP 2000250990A JP 2000250990 A JP2000250990 A JP 2000250990A JP 4487110 B2 JP4487110 B2 JP 4487110B2
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- Prior art keywords
- resin
- buffer layer
- resin material
- laminate
- coated
- 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.)
- Expired - Fee Related
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 229920005989 resin Polymers 0.000 claims description 51
- 239000011347 resin Substances 0.000 claims description 51
- 239000000463 material Substances 0.000 claims description 41
- 239000007769 metal material Substances 0.000 claims description 18
- 229920005992 thermoplastic resin Polymers 0.000 claims description 11
- 239000013013 elastic material Substances 0.000 claims description 9
- 229920001187 thermosetting polymer Polymers 0.000 claims description 9
- 239000002759 woven fabric Substances 0.000 claims description 9
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 7
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 7
- 239000004744 fabric Substances 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 6
- 239000004753 textile Substances 0.000 claims description 6
- 239000000835 fiber Substances 0.000 claims description 5
- 229920001971 elastomer Polymers 0.000 claims description 4
- 239000005060 rubber Substances 0.000 claims description 4
- 238000010030 laminating Methods 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 description 13
- 239000002184 metal Substances 0.000 description 13
- 238000000465 moulding Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920000139 polyethylene terephthalate Polymers 0.000 description 2
- 239000005020 polyethylene terephthalate Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- XQUPVDVFXZDTLT-UHFFFAOYSA-N 1-[4-[[4-(2,5-dioxopyrrol-1-yl)phenyl]methyl]phenyl]pyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C(C=C1)=CC=C1CC1=CC=C(N2C(C=CC2=O)=O)C=C1 XQUPVDVFXZDTLT-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229920002943 EPDM rubber Polymers 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229920000620 organic polymer Polymers 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920003192 poly(bis maleimide) Polymers 0.000 description 1
- 229920006122 polyamide resin Polymers 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- -1 polyethylene terephthalate Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
Images
Landscapes
- Laminated Bodies (AREA)
Description
【0001】
【発明の属する技術分野】
この発明は、積層体の構造及びその製造方法に係わり、更に詳しくは線膨張係数が異なる金属材料と樹脂材料とを積層して一体的に成形する際、樹脂材料の成形後に生ずるクラックの発生を有効に防止した積層体の構造及びその製造方法に関するものである。
【0002】
【従来の技術】
樹脂材料を棒状またはパイプ状の金属材料や板状の金属材料に被覆して成形する場合、金属材料の表面に樹脂材料を直接積層して成形するのが一般的である。
【0003】
しかるに、樹脂材料にて金属材料を全面もしくは一方向のみの面を残して二方向の面を覆うような成形方法(例えば、パイプ、棒状金属の外側に成形し、断面は除く)は同様に成形され、そのまま一体で加熱成形させる。
【0004】
【発明が解決しようとする課題】
すると、有機高分子材料である樹脂材料の線膨張係数は、70×10-6K-1であり、金属材料の線膨張係数の8×10-6K-1に比べて約10倍程大きい。
【0005】
この結果、加熱時に各々膨張した樹脂材料及び金属材料は、マトリックス樹脂の硬化または溶融温度域でその貼合わせ界面で一致するが、冷却が始まるにつれて樹脂材料の方が収縮が大きい(所謂硬化収縮)。これは、硬化または溶融温度の高い樹脂材料ほど収縮度合いが大きくなり、極端な場合、樹脂材料にクラックが生じる。これは、断面寸法が同一のテーパ状になっていない金属形状のものに多い。
【0006】
この発明の目的は、線膨張係数が異なる金属材料と樹脂材料とを積層して一体的に成形する際、貼合わせ界面で成形後に生ずるクラックの発生を有効に防止した積層体の構造及びその製造方法を提供することにある。
【0007】
【課題を解決するための手段】
この発明は上記目的を達成するため、この発明の積層体の構造は、金属材料と樹脂材料との境界面に繊維の織布の少なくとも一方の面をゴム状弾性材料でコートしたゴム引き布とした緩衝層を介在させて一体的に構成したことを要旨とするものである。このように構成することで、貼合わせ界面で成形後に生ずるクラックの発生を有効に防止出来るものである。
【0008】
また、この発明の積層体の製造方法は、金属材料の外表面に、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートした緩衝層を被覆し、この緩衝層の上に樹脂材料を被覆して一体的に成形することを要旨とするものである。
【0009】
この発明は、上記のように構成され、金属材料と樹脂材料との境界面に、繊維の織布の片面または両面をゴム状弾性材料でコートしたゴム引き布を介在させて一体的に構成したことにより、線膨張係数が異なる金属材料と樹脂材料とを積層して一体的に成形する際、貼合わせ界面で成形後に生じるクラックの発生を有効に防止することが出来るものである。
【0010】
【発明の実施の形態】
以下、添付図面に基づき、この発明の実施形態を説明する。
【0011】
図1は、この発明の第1実施形態を示す金属棒に繊維強化プラスチック(FRP)等の樹脂材料を積層した積層体の斜視図を示し、この積層体は、金属棒1と、樹脂材料2との成形界面Xには、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートしたゴム引き布とした緩衝層3を介在させて一体的に構成してある。
【0012】
なお、金属棒1は、図1に示すように中実の丸棒の他、中空パイプ状のものであっても良く、金属材料としては、アルミニウム,鉄,チタン,銅等の他、他の金属材料で形成することも可能である。
【0013】
前記緩衝層3を構成する繊維の織布は、芳香族ポリアミド繊維(アラミド繊維)、ポリエチレンテレフタレート(PET)繊維等からなり、ゴム状弾性材料は、NBR,BR,SBR,NR,IR,EPDM,CRから成る。
【0014】
なお、織布、ゴムの種類及び厚さ等は、成形する物体の寸法、硬化温度等により選定される。
【0015】
更に、前記樹脂材料2は、熱可塑性樹脂または熱硬化性樹脂の単独または熱可塑性樹脂との混合物を使用するか、または前記熱可塑性樹脂または熱硬化性樹脂の単独または熱可塑性樹脂との混合物をマトリックス樹脂とする繊維強化プラスチック材料を使用するものである。
【0016】
前記マトリックス樹脂は、エポキシ樹脂、フェノール樹脂、ビスマレイミド樹脂等の熱硬化性樹脂またはポリエステル樹脂、ポリアミド樹脂、ポリイミド樹脂等の熱可塑性樹脂、またはそれらの混合物とし、特に限定するものではない。
【0017】
また、図2はこの発明の第2実施形態を示す積層体の斜視図を示し、この実施形態は、断面四角形状の金属棒1と、樹脂材料2との成形界面Xには、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートしたゴム引き布とした緩衝層3を介在させたもので、金属棒1は、中実または中空状のものであっても良い。
【0018】
なお、緩衝層3のゴム引き布の構成は、上記第1実施形態と同様である。
【0019】
上記のような棒状の積層体の製造方法は、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートした緩衝層3を、前記金属棒1(金属材料)の外表面に被覆し、この上に樹脂材料2を被覆して、常温硬化、またはオーブン等に入れ加熱硬化させることにより一体的に成形するものである。
【0020】
前記樹脂材料2は、熱可塑性樹脂と熱硬化性樹脂との少なくとも一方を使用するか、または熱可塑性樹脂と熱硬化性樹脂との少なくとも一方をマトリックス樹脂とした繊維強化プラスチック材料を使用する。
【0021】
例えば、直径40mmの金属棒1と、その外周面を覆う厚さ40mmの樹脂材料2との成形界面Xには、0.2 〜0.5 mmの緩衝層3を介在させて一体的に成形する。
【0022】
このように構成することで、金属棒1と樹脂材料2のように、線膨張率が全く異なる二種類の材料を積層させて成形する場合にも、成形界面Xに介在させる緩衝層3の所謂クッション効果により樹脂材料2のクラックの発生を抑えることが出来るものである。
【0023】
【発明の効果】
この発明は、上記のように線膨張率が全く異なる二種類の材料を積層させて成形する場合にも、成形界面に介在させる緩衝層の所謂クッション効果により繊維強化プラスチック等の樹脂材料のクラックの発生を抑えることが出来る効果がある。
【図面の簡単な説明】
【図1】この発明の第1実施形態を示す金属棒に樹脂材料を積層した斜視図である。
【図2】この発明の第2実施形態を示す積層体の斜視図である。
【符号の説明】
1 金属棒
2 樹脂材料
3 緩衝層
X 成形界面[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a structure of a laminate and a manufacturing method thereof, and more specifically, when a metal material and a resin material having different linear expansion coefficients are laminated and integrally molded, generation of cracks generated after molding of the resin material is caused. The present invention relates to a structure of a laminate that is effectively prevented and a manufacturing method thereof.
[0002]
[Prior art]
When a resin material is formed by coating a rod-like or pipe-like metal material or a plate-like metal material, the resin material is generally laminated directly on the surface of the metal material.
[0003]
However, a molding method (for example, forming on the outside of a pipe or rod-shaped metal, excluding the cross section) that forms a metal material with a resin material to cover the entire surface or a surface in only one direction and covering the surface in two directions is similarly formed. Then, it is heat-molded as it is.
[0004]
[Problems to be solved by the invention]
Then, the linear expansion coefficient of the resin material which is an organic polymer material is 70 × 10 −6 K −1, which is about 10 times larger than the linear expansion coefficient of the metal material of 8 × 10 −6 K −1. .
[0005]
As a result, the resin material and the metal material that have expanded during heating coincide with each other at the bonding interface in the curing or melting temperature range of the matrix resin, but the resin material contracts more as the cooling starts (so-called curing shrinkage). . This is because a resin material having a higher curing or melting temperature has a higher degree of shrinkage, and in an extreme case, a crack occurs in the resin material. This is often the case for metal shapes that are not tapered with the same cross-sectional dimension.
[0006]
An object of the present invention is to provide a structure of a laminate that effectively prevents the generation of cracks after molding at the bonding interface when a metal material and a resin material having different linear expansion coefficients are laminated and integrally molded, and its manufacture It is to provide a method.
[0007]
[Means for Solving the Problems]
In order to achieve the above-mentioned object, the structure of the laminate of the present invention includes a rubberized cloth in which at least one surface of a woven fabric of fibers is coated with a rubber-like elastic material on a boundary surface between a metal material and a resin material. The gist is that the buffer layer is integrally formed with the buffer layer interposed. By comprising in this way, generation | occurrence | production of the crack which arises after shaping | molding in a bonding interface can be prevented effectively.
[0008]
A method of manufacturing a laminate of the invention, the external surface surface of the metallic material, coated with a buffer layer coated with a rubber-like elastic material at least one surface of the woven fabric of textiles, on the buffer layer The gist is to cover and integrally mold the resin material.
[0009]
This invention is constructed as described above, the interface between the metal and resin materials, is allowed to integrally formed interposing rubberized fabric coated on one or both sides of the woven textiles with rubber-like elastic material As a result, when a metal material and a resin material having different linear expansion coefficients are laminated and integrally molded, it is possible to effectively prevent the occurrence of cracks after molding at the bonding interface.
[0010]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings.
[0011]
FIG. 1 shows a perspective view of a laminated body in which a resin material such as fiber reinforced plastic (FRP) is laminated on a metal rod showing a first embodiment of the present invention. This laminated body is composed of a metal rod 1 and a
[0012]
The metal rod 1 may be a solid round bar as shown in FIG. 1 or may be a hollow pipe. The metal material may be aluminum, iron, titanium, copper, etc. It is also possible to form with a metal material.
[0013]
The woven fabric of fibers constituting the buffer layer 3 is made of aromatic polyamide fiber (aramid fiber), polyethylene terephthalate (PET) fiber, etc., and the rubber-like elastic material is NBR, BR, SBR, NR, IR, EPDM, Consists of CR.
[0014]
The type and thickness of the woven fabric and rubber are selected depending on the size of the object to be molded, the curing temperature, and the like.
[0015]
Furthermore, the
[0016]
The matrix resin is not particularly limited, and may be a thermosetting resin such as an epoxy resin, a phenol resin, or a bismaleimide resin, or a thermoplastic resin such as a polyester resin, a polyamide resin, or a polyimide resin, or a mixture thereof.
[0017]
Also, FIG. 2 shows a second perspective view of a laminate illustrating an embodiment of the present invention, this embodiment includes a square cross-section shape of the metal rod 1, the molding surface X of the
[0018]
The configuration of the rubberized cloth of the buffer layer 3 is the same as that in the first embodiment.
[0019]
Method for producing a laminate of the rod-shaped as described above, covering at least one surface of the woven fabric textiles buffer layer 3 coated with rubber-like elastic material, the external surface surface of the metal rod 1 (metal material) Then , the
[0020]
As the
[0021]
For example, the metal rod 1 having a diameter of 40 mm and the molding interface X between the
[0022]
With this configuration, when the two types of materials having completely different linear expansion coefficients such as the metal rod 1 and the
[0023]
【The invention's effect】
Even when two types of materials having completely different linear expansion coefficients are laminated and molded as described above, the present invention prevents cracks in resin materials such as fiber reinforced plastics by the so-called cushioning effect of the buffer layer interposed at the molding interface. There is an effect that generation can be suppressed.
[Brief description of the drawings]
FIG. 1 is a perspective view in which a resin material is laminated on a metal bar according to a first embodiment of the present invention.
FIG. 2 is a perspective view of a laminated body showing a second embodiment of the present invention.
[Explanation of symbols]
1
Claims (6)
前記金属材料と前記樹脂材料との境界面に緩衝層を介在させて一体的に構成して成り、前記緩衝層を、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートしたゴム引き布にした積層体の構造。In the structure of the laminate formed by laminating the entire surface of the metal material or the other surface leaving the surface in one direction covered with the resin material,
Rubber by interposing a buffer layer Ri formed by integrally formed, the buffer layer, where the at least one surface of the woven fabric of fibers coated with a rubber-like elastic material at the interface between the metal material and the resin material The structure of a laminate made of a stretch fabric .
前記金属材料の外表面に、繊維の織布の少なくとも一方の面をゴム状弾性材料でコートした緩衝層を被覆し、この緩衝層の上に樹脂材料を被覆して一体的に成形する積層体の製造方法。In the manufacturing method of the laminate, in which the entire surface of the metal material or the other surface is left so as to be covered with the resin material while leaving the surface in one direction,
The external surface surface of the metallic material, coated with a buffer layer coated with a rubber-like elastic material at least one surface of the woven fabric of textiles, integrally molded of resin material is coated on the buffer layer A manufacturing method of a layered product.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2000250990A JP4487110B2 (en) | 2000-08-22 | 2000-08-22 | Laminated body structure and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2000250990A JP4487110B2 (en) | 2000-08-22 | 2000-08-22 | Laminated body structure and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2002059509A JP2002059509A (en) | 2002-02-26 |
| JP4487110B2 true JP4487110B2 (en) | 2010-06-23 |
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| JP2000250990A Expired - Fee Related JP4487110B2 (en) | 2000-08-22 | 2000-08-22 | Laminated body structure and manufacturing method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP2006272656A (en) * | 2005-03-28 | 2006-10-12 | Sankyo Seisakusho:Kk | Metal / resin composite tube and manufacturing method thereof |
| JP5270899B2 (en) * | 2007-10-10 | 2013-08-21 | 美濃工業株式会社 | Molded member |
| JP7810546B2 (en) * | 2021-12-08 | 2026-02-03 | 藤倉コンポジット株式会社 | Composite material and method for manufacturing the same |
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