JPH0358836A - Composite molded product - Google Patents

Composite molded product

Info

Publication number
JPH0358836A
JPH0358836A JP19395789A JP19395789A JPH0358836A JP H0358836 A JPH0358836 A JP H0358836A JP 19395789 A JP19395789 A JP 19395789A JP 19395789 A JP19395789 A JP 19395789A JP H0358836 A JPH0358836 A JP H0358836A
Authority
JP
Japan
Prior art keywords
molded product
metal plate
fiber
thickness
acm
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
JP19395789A
Other languages
Japanese (ja)
Other versions
JP2862138B2 (en
Inventor
Yoshijiro Tate
館 芳士郎
Tadashi Kawamoto
忠 川本
Masaaki Tatara
多々良 正明
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.)
Sumitomo Bakelite Co Ltd
Original Assignee
Sumitomo Bakelite 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 Sumitomo Bakelite Co Ltd filed Critical Sumitomo Bakelite Co Ltd
Priority to JP1193957A priority Critical patent/JP2862138B2/en
Publication of JPH0358836A publication Critical patent/JPH0358836A/en
Application granted granted Critical
Publication of JP2862138B2 publication Critical patent/JP2862138B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To enhance impact resistance by fixing fiber reinforced plastic based on a high strength fiber and containing a thermoplastic resin as a binder to the whole or part of the opposite surface to a side where flying matter impinges of a metal plate or a molded product thereof. CONSTITUTION:High strength fiber reinforced plastic 2 based on a high strength fiber and containing a thermoplastic resin as a binder is fixed to the whole or part of the rear of a metal plate 1 or a molded product thereof by bolts 3 to obtain a desired composite molded product. At this time, the thickness of the metal plate 1 is set to 1 - 30mm and that of the fiber reinforced plastic 2 is set to 0.4 - 25mm.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、金属板又はその成形物の飛来物が当たる側の
反対面(以下、裏面という)に高強度繊維を基材とする
熱可塑性樹脂繊維強化プラスチックを機械的方法又は接
着等の化学的方法により固定することにより、軽量で耐
衝撃性に優れた複合或形物に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] The present invention is directed to a metal plate or a molded product having a thermoplastic material having a high-strength fiber as a base material on the opposite side (hereinafter referred to as the back side) of the side that is hit by flying objects. The present invention relates to a composite shaped article that is lightweight and has excellent impact resistance by fixing resin fiber reinforced plastics by a mechanical method or a chemical method such as adhesion.

〔従来の技術〕[Conventional technology]

高所から落下する物体等の飛来物に対する耐衝撃体は、
鉄あるいはアルミニウム合金等の単一物又はそれらの多
層体、あるいは金属体の間にプラスチック又はセラミッ
クなどの層を設けた複合物が有効である。かかる耐@撃
体は所定の特性を保持するために所要の厚みが必要であ
り、このため重量の軽減がはかれない。
Impact-resistant bodies against flying objects such as objects falling from high places are
A single material such as iron or aluminum alloy, a multi-layered material thereof, or a composite material in which a layer of plastic or ceramic is provided between metal materials are effective. Such an impact-resistant body requires a certain thickness in order to maintain predetermined properties, and therefore weight cannot be reduced.

また、金属体の間に高強度繊維を基材とする繊維強化プ
ラスチックを挿入することも研究されたが、このような
複合物は、両側から金属体で固定されているため、繊維
強化プラスチックのもっているエネルギー吸収特性を生
かしきれない欠点があった。
Research has also been done on inserting fiber-reinforced plastics based on high-strength fibers between metal bodies, but such composites are fixed with metal bodies from both sides, making it difficult to use fiber-reinforced plastics. The drawback was that it could not make full use of its energy absorption properties.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

本発明者は、熱可塑性樹脂をバインダーとし、高強度繊
維を基材とする高強度繊維強化プラスチック(以下、A
CMという)が耐衝撃性に優れているとの知見を得、更
に、これと金属体との複合方法を種々検討した結果、A
CMを金属体の裏面に固定することにより、耐衝撃性の
大きな複合或形物を完戊させるに至ったものである。
The present inventor has developed a high-strength fiber-reinforced plastic (hereinafter referred to as A
We found that CM) has excellent impact resistance, and after investigating various ways to combine it with a metal body, we found that A
By fixing CM to the back surface of a metal body, a composite shaped article with high impact resistance has been completed.

〔課題を解決するための手段〕[Means to solve the problem]

本発明は、金属板又はその成形物の裏面全面又はその一
部に、高強度繊維を基材とし、熱可塑性樹脂をバインダ
ーとする高強度繊維強化プラスチックを固定するするこ
とを特徴とする複合成形物である。
The present invention is a composite molding characterized in that a high-strength fiber-reinforced plastic made of high-strength fiber as a base material and a thermoplastic resin as a binder is fixed to the entire back surface or a part of the back surface of a metal plate or a molded product thereof. It is a thing.

本発明において用いられる高強度繊維とは、引張強度を
密度で割った比引張強度が IOXIO’cm以上であ
り、弾性率を密度で割った比弾性率が2.5XlO’C
m以上のものである。具体的には、高強度ガラス繊維、
カーボン繊維、アラミド繊維、芳香族ポリエステル繊維
、高強度ポリエチレン繊維、ビニロン繊維などである。
The high-strength fiber used in the present invention has a specific tensile strength (tensile strength divided by density) of IOXIO'cm or more, and a specific elastic modulus (modulus of elasticity divided by density) of 2.5XlO'C.
m or more. Specifically, high-strength glass fiber,
These include carbon fiber, aramid fiber, aromatic polyester fiber, high strength polyethylene fiber, and vinylon fiber.

一般のガラス繊維、ナイロン繊維、ポリエステル繊維な
どは該当しない。比引張強度あるいは比弾性率が前記値
以下では、ACMと金属体との複合成形物の耐衝撃性は
必ずしも十分ではない。
General glass fibers, nylon fibers, polyester fibers, etc. are not applicable. If the specific tensile strength or specific modulus is less than the above value, the impact resistance of the composite molded product of ACM and the metal body is not necessarily sufficient.

これらの高強度繊維に塗布ないし含浸する熱可塑性樹脂
としては、ポリエチレン、ポリプロピレンなどのポリオ
レフィン、ポリアミド、ポリエステル、ポリビニルアセ
テート、ポリエーテルサルファイド、ポリフエニルサル
ファイド、ポリエーテルエーテルケトン、熱可塑性ポリ
ウレタン、合成ゴムなどである。
Thermoplastic resins to be applied or impregnated into these high-strength fibers include polyolefins such as polyethylene and polypropylene, polyamides, polyesters, polyvinyl acetates, polyether sulfides, polyphenyl sulfides, polyether ether ketones, thermoplastic polyurethanes, synthetic rubbers, etc. It is.

ACMを得るには、通常高強度繊維に熱可塑性樹脂の溶
液、粉末又はその分教液を含浸又は筺布してプリブレグ
を作威し、このプリプレグを複数枚重ね、加熱加圧する
圧縮成形法を採用する。この際、樹脂の含有率は5〜8
0%(重量%、以下同じ)の範囲であるが、通常は5〜
50%、好ましくは10〜30%である。樹脂の含有率
が小さいほど衝撃力に対するエネルギー吸収力が大きく
なるが、5%以下ではプリブレグを作ることが困難であ
り、80%以上でもプリブレグを作ることが困難であり
、50%耐衝撃性が低下する傾向がある。
To obtain ACM, a compression molding method is usually used, in which high-strength fibers are impregnated or coated with a thermoplastic resin solution, powder, or its dispersion solution to create a prepreg, and multiple sheets of this prepreg are stacked and heated and pressed. adopt. At this time, the resin content is 5 to 8
It is in the range of 0% (wt%, same below), but usually 5-
50%, preferably 10-30%. The smaller the resin content, the greater the energy absorption capacity against impact force, but if it is less than 5%, it is difficult to make a pre-reg, and even if it is more than 80%, it is difficult to make a pre-reg, and the impact resistance is less than 50%. There is a tendency to decrease.

本発明において、金属板の厚みは通常1〜30mmであ
る。1mm以下では金属板を設ける効果が小さく、30
mm以上では軽量化の効果が得られ難い。
In the present invention, the thickness of the metal plate is usually 1 to 30 mm. If the thickness is less than 1 mm, the effect of providing the metal plate is small, and 30
If it is more than mm, it is difficult to obtain the effect of weight reduction.

好ましい厚みは1.5〜5mmである。The preferred thickness is 1.5 to 5 mm.

一方、ACMの厚みは通常0−4−25mmである。0
 . 4 mm以下では衝撃エネルギー吸収効果が小さ
く、25mm以上厚くしても衝撃エネルギー吸収効果は
大差ない。好ましい厚みは1.5〜8mmである。
On the other hand, the thickness of ACM is usually 0-4-25 mm. 0
.. If the thickness is 4 mm or less, the impact energy absorption effect is small, and even if the thickness is 25 mm or more, the impact energy absorption effect does not change much. The preferred thickness is 1.5 to 8 mm.

こうして得られたACMは、金属板又はその成形物の裏
面にボルトやリベットあるいは枠材等を使用して機械的
な方法で固定する、あるいは合或ゴム系等の接着剤で接
着する、などの方法で固定する。なお、固定する際、金
属板とACMの間に間隔を設けてもよい。
The ACM thus obtained can be fixed to the back surface of a metal plate or its molded product by a mechanical method using bolts, rivets, frame materials, etc., or by bonding with a rubber-based adhesive or the like. Fix by method. Note that when fixing, a space may be provided between the metal plate and the ACM.

第1図乃至第3図に構戊例を示す。いずれの場合も飛来
物が当たるのは金属板側である。第1図は金属板とAC
Mをボルトで固定したものである。
Examples of the structure are shown in FIGS. 1 to 3. In either case, it is the metal plate side that is hit by the flying object. Figure 1 shows the metal plate and AC
M is fixed with bolts.

第2図は金属板を二次元加工しACMを接着剤で固定し
たものである。第3図は金属板を三次元加工して半球状
とし、同じく半球状のACMをボルトで固定したもので
ある。
Figure 2 shows a metal plate that has been two-dimensionally processed and an ACM fixed with adhesive. In Figure 3, a metal plate is three-dimensionally processed into a hemispherical shape, and a similarly hemispherical ACM is fixed with bolts.

[実施例] 以下、本発明を実施例により説明する。[Example] The present invention will be explained below with reference to Examples.

実施例l 比引張強度 1 6 X l O ’am,比弾性率3
.2×10”cmの高強度ガラス繊維からなる織布(厚
さ0.45mm,坪量500g/mりにアクリル樹脂の
15%MEK溶液を含浸し、乾燥して樹脂分18%のプ
リプレグ(610g/mQを作製した。このブリブレグ
を4枚重ね、2 8 0 ’0,  1 0 0 Kg
/cm”で加熱加圧して高強度ガラス繊維強化アクリル
樹脂ACM板を得た。
Example l Specific tensile strength 1 6 X l O'am, specific modulus 3
.. A woven fabric (thickness 0.45 mm, basis weight 500 g/m) made of high-strength glass fiber of 2 x 10"cm is impregnated with a 15% MEK solution of acrylic resin and dried to produce a prepreg (610 g) with a resin content of 18%. /mQ was produced.Four sheets of this brev leg were stacked and weighed 2 8 0 '0, 1 0 0 Kg.
/cm" to obtain a high-strength glass fiber reinforced acrylic resin ACM board.

これをサイズ300X 300X 3.5mmの鋼板の
四隅にタップを切り、前記ACM板を鋼板の裏面よりボ
ルトで固定し、第1図に示すような複合板を作製し I
こ。
Taps were cut in the four corners of a steel plate of size 300 x 300 x 3.5 mm, and the ACM plate was fixed with bolts from the back side of the steel plate to produce a composite plate as shown in Figure 1.
child.

実施例2 比引張強度2 0 X l O ’cm,比弾性率4.
9×10’cmの芳香族ポリエステル繊維の織布(厚さ
0.44mm,坪量260g/m”)に6−ナイロンの
微粉末を吹き付けて樹脂分15%のプリプレグ(306
g/m”)を作製した。このブリプレグを6枚重ね、2
20゜Cs 7 0Kg/cm2で加熱加圧して芳香族
ポリエステル繊維強化ナイロンACM板を得た。
Example 2 Specific tensile strength: 20 X l O'cm, specific modulus of elasticity: 4.
A prepreg (306
g/m”) was produced. Six sheets of this Bripreg were stacked and two
An aromatic polyester fiber reinforced nylon ACM board was obtained by heating and pressing at 20°Cs 70Kg/cm2.

これをサイズ300 X 300 X 3.5mmの鋼
板の四隅にタップを切り、前記ACM板を鋼板の裏面よ
りボルトで固定し、第l図に示すような複合板を作製し
 Iこ。
Taps were cut in the four corners of a steel plate measuring 300 x 300 x 3.5 mm, and the ACM plate was fixed with bolts from the back side of the steel plate to produce a composite plate as shown in Figure 1.

比較例I 実施例lで使用したものと同質で厚さ5mmの鋼板をそ
のまま使用しt;。
Comparative Example I A 5 mm thick steel plate of the same quality as that used in Example I was used as it was.

実施例3 比引張強度2 1 X 1 0 ’am,比弾性率6.
4×10’cmのアラミド繊維からなる織布(厚さ0.
45mm,坪量500g/mつにABS樹脂の18%M
EK溶液を含浸し、乾燥して樹脂分20%のプリブレグ
(625g/m’)を作製した。このプリプレグを6枚
重ね、二次曲面をもつ金型の中に入れ、150’O、l
 O OKg/cm”で加熱加圧してアラミド繊維強化
ABS樹脂ACM板を得た。
Example 3 Specific tensile strength 2 1 × 1 0 'am, specific modulus 6.
A 4 x 10'cm woven fabric made of aramid fibers (thickness 0.
45mm, basis weight 500g/m, 18%M of ABS resin
It was impregnated with an EK solution and dried to produce a prepreg (625 g/m') with a resin content of 20%. 6 sheets of this prepreg were stacked and placed in a mold with a quadratic curved surface, 150'O, l
An aramid fiber-reinforced ABS resin ACM board was obtained by heating and pressing at a pressure of 0.0 kg/cm''.

これを同じ曲面を有する厚さ5mmのアルミニウム合金
板の裏面に合戊ゴム系接着剤で接着固定し、第2図に示
すような複合板を作製した。
This was adhered and fixed to the back side of a 5 mm thick aluminum alloy plate having the same curved surface using a synthetic rubber adhesive to produce a composite plate as shown in FIG. 2.

比較例2 実施例3で使用したものと同質で厚さ8mmのアルミニ
ウム合金板をそのまま使用した。
Comparative Example 2 An aluminum alloy plate having the same quality as that used in Example 3 and having a thickness of 8 mm was used as it was.

比較例3 実施例3で得られたアラミド繊維強化ABS樹脂ACM
板を実施例3で使用したアルミニウム合金板の表面側に
前記接着剤で接着固定した。
Comparative Example 3 Aramid fiber reinforced ABS resin ACM obtained in Example 3
The plate was adhesively fixed to the surface side of the aluminum alloy plate used in Example 3 using the adhesive described above.

比較例4 実施例3で得られたアラミド繊維強化ABS樹脂ACM
板を同じ曲面をもつ厚さ2mmと3mmのアルミニウム
合金板の間に挿入し、ボルト・ナットで固定した。なお
、表面側のアルミニウム合金板を2mmとした。
Comparative Example 4 Aramid fiber reinforced ABS resin ACM obtained in Example 3
The plate was inserted between 2 mm and 3 mm thick aluminum alloy plates with the same curved surface and fixed with bolts and nuts. Note that the aluminum alloy plate on the front side was 2 mm thick.

実施例4 実施例lで使用した高強度ガラス繊維の織布にポリブチ
レンテレフタレート(PBT)樹脂の微粉末を吹き付け
て、樹脂分20%のプリブレグ(625g/mりを作製
した。このプリプレグを4枚重ね、半球状の金型に入れ
、l 5 0’OSI O OKg/cm”で加熱加圧
して高強度ガラス繊維強化PBT樹脂ACMtC形物を
得た。
Example 4 Fine powder of polybutylene terephthalate (PBT) resin was sprayed onto the high-strength glass fiber woven fabric used in Example 1 to produce a prepreg (625 g/m2) with a resin content of 20%. The sheets were stacked, placed in a hemispherical mold, and heated and pressed at l 5 0'OSI O OKg/cm'' to obtain a high-strength glass fiber reinforced PBT resin ACMtC shaped article.

これを厚さ1 . 5 mmの半球状鋼鉄或形体の内面
に入れ、球面のリブ状部分をボルト・ナットで固定し、
第−3図に示すような複合成形物を得た。
Thickness 1. Put it into the inner surface of a 5 mm hemispherical steel shape, fix the spherical rib-like part with bolts and nuts,
A composite molded article as shown in FIG. 3 was obtained.

比較例5 実施例4で使用したものと同質で厚さ2 . 5 mm
の半球状鋼鉄威形体をそのまま使用した。
Comparative Example 5 Same material as that used in Example 4, thickness 2. 5mm
The hemispherical steel body was used as is.

各例における複合或形物について、JIS T 813
3に基づく耐衝撃性試験結果、成形物の厚さ及びlm2
あたりの重量を測定し、その結果を第1表に示す。なお
、耐衝撃性試験は成形物の表側に対して衝撃を加えた。
For composite shapes in each example, JIS T 813
Impact resistance test results based on 3, thickness of molded product and lm2
The weight per unit was measured and the results are shown in Table 1. In the impact resistance test, an impact was applied to the front side of the molded product.

第 l 表 実施例1及び2では、金属板の裏面側のみに八〇Mを設
けているので、比較例lの金属板のみの場合に比べて、
耐衝撃性が優れ、軽量化も達成できた・実施例3でも比
較例2と比べて、耐衝撃性に優れ、軽量化も達成できた
。比較例3及び4は実施例3における金属板をACMの
裏面側、あるいは表面側と裏面側に分割して設けたため
、実施例3に比べて、耐衝撃性が劣っている。実施例4
の場合も、比較例5と比べて、耐衝撃性に優れ、軽量化
も達戒できた。
In Examples 1 and 2 of Table 1, 80M is provided only on the back side of the metal plate, so compared to the case of only the metal plate in Comparative Example 1,
Excellent impact resistance and weight reduction achieved - Example 3 also achieved excellent impact resistance and weight reduction compared to Comparative Example 2. In Comparative Examples 3 and 4, the metal plate in Example 3 was provided on the back side of the ACM or divided into the front side and the back side, so the impact resistance was inferior to that in Example 3. Example 4
Also in the case of Comparative Example 5, the impact resistance was excellent and the weight was reduced.

〔発明の効果〕〔Effect of the invention〕

以上の実施例からも明らかなように、本発明の複合成形
物は、従来の耐衝撃性金属体に対して耐衝撃性を同等以
上としたとき、その重量を20〜60%軽減することが
できる。
As is clear from the above examples, the composite molded product of the present invention can reduce the weight by 20 to 60% when the impact resistance is equal to or higher than that of a conventional impact-resistant metal body. can.

ACMを金属体の表面側に設けた場合、又は金属体間に
挿入した場合、ACMの耐衝撃性の効果はかなり小さく
なり、複合板にするメリットは少ない。
If the ACM is provided on the surface side of a metal body or inserted between metal bodies, the impact resistance effect of the ACM will be considerably reduced, and there will be little merit in using a composite plate.

ACMを金属体の裏面側にのみ設けた場合、金属体のみ
の場合や金属体を使用しないACMの場合と比較して、
同一重量で耐衝撃性は25〜50%向上する。
When the ACM is provided only on the back side of the metal body, compared to the case where only the metal body is used or the case where the ACM does not use the metal body,
Impact resistance increases by 25-50% for the same weight.

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

第1図乃至第3図は本発明のACMの構戊例を示すもの
であり、第1図及び第2図は斜視図、第3図は断面図で
ある。
1 to 3 show examples of the structure of the ACM of the present invention, FIGS. 1 and 2 are perspective views, and FIG. 3 is a sectional view.

Claims (3)

【特許請求の範囲】[Claims] (1)高強度繊維を基材とし、熱可塑性樹脂をバインダ
ーとする繊維強化プラスチックを、金属板又はその成形
物の飛来物が当たる側の反対面全面又はその一部に固定
してなることを特徴とする複合成形物。
(1) A fiber-reinforced plastic made of high-strength fiber as a base material and a thermoplastic resin as a binder is fixed to the entire surface or a part of the opposite side of the metal plate or its molded material to the side that is hit by flying objects. Composite molded product with characteristics.
(2)高強度繊維基材に熱可塑性樹脂の溶液、粉末又は
その分散液を含浸又は塗布してなるプリプレグを加熱加
圧成形して得た繊維強化プラスチックを、金属板又はそ
の成形物の、飛来物が当たる側の反対面全面又はその一
部に固定してなることを特徴とする複合成形物。
(2) A fiber-reinforced plastic obtained by heating and press-molding a prepreg obtained by impregnating or coating a high-strength fiber base material with a thermoplastic resin solution, powder, or dispersion thereof, can be used as a metal plate or a molded product thereof. A composite molded article that is fixed to the entire surface or a part of the opposite side to the side that is hit by flying objects.
(3)前記金属板の厚みが1〜30mmであり、前記繊
維強化プラスチックの厚みが0.4〜25mmであるこ
とを特徴とする複合成形物。
(3) A composite molded article, wherein the metal plate has a thickness of 1 to 30 mm, and the fiber reinforced plastic has a thickness of 0.4 to 25 mm.
JP1193957A 1989-07-28 1989-07-28 Composite molding Expired - Fee Related JP2862138B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1193957A JP2862138B2 (en) 1989-07-28 1989-07-28 Composite molding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1193957A JP2862138B2 (en) 1989-07-28 1989-07-28 Composite molding

Publications (2)

Publication Number Publication Date
JPH0358836A true JPH0358836A (en) 1991-03-14
JP2862138B2 JP2862138B2 (en) 1999-02-24

Family

ID=16316574

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1193957A Expired - Fee Related JP2862138B2 (en) 1989-07-28 1989-07-28 Composite molding

Country Status (1)

Country Link
JP (1) JP2862138B2 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0620110A1 (en) * 1992-10-02 1994-10-19 Sumitomo Chemical Company, Limited Multi-layer laminate
US5736254A (en) * 1992-10-02 1998-04-07 Sumitomo Chemical Company, Limited Multilayer laminate
WO2012126923A1 (en) * 2011-03-24 2012-09-27 Thyssenkrupp Steel Europe Ag Composite material and structural component for a motor vehicle
US10137940B2 (en) * 2015-05-27 2018-11-27 Toyota Jidosha Kabushiki Kaisha Vehicle member joining structure and vehicle member joining method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5757654A (en) * 1980-09-24 1982-04-06 Nippon Soken Method of connecting carbon fiber reinforced composite material and metallic material
JPS5770648A (en) * 1980-10-21 1982-05-01 Idemitsu Petrochemical Co Laminate
JPS591250A (en) * 1982-06-28 1984-01-06 横浜ゴム株式会社 Method of pasting fiber reinforced plastic to steel plate

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5757654A (en) * 1980-09-24 1982-04-06 Nippon Soken Method of connecting carbon fiber reinforced composite material and metallic material
JPS5770648A (en) * 1980-10-21 1982-05-01 Idemitsu Petrochemical Co Laminate
JPS591250A (en) * 1982-06-28 1984-01-06 横浜ゴム株式会社 Method of pasting fiber reinforced plastic to steel plate

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0620110A1 (en) * 1992-10-02 1994-10-19 Sumitomo Chemical Company, Limited Multi-layer laminate
EP0620110A4 (en) * 1992-10-02 1995-03-29 Sumitomo Chemical Co Multi-layer laminate.
US5736254A (en) * 1992-10-02 1998-04-07 Sumitomo Chemical Company, Limited Multilayer laminate
WO2012126923A1 (en) * 2011-03-24 2012-09-27 Thyssenkrupp Steel Europe Ag Composite material and structural component for a motor vehicle
US10137940B2 (en) * 2015-05-27 2018-11-27 Toyota Jidosha Kabushiki Kaisha Vehicle member joining structure and vehicle member joining method

Also Published As

Publication number Publication date
JP2862138B2 (en) 1999-02-24

Similar Documents

Publication Publication Date Title
JPH0358836A (en) Composite molded product
JPH08258189A (en) Manufacture of sandwich panel
JP3127947B2 (en) Composite molding
WO2022260186A1 (en) Laminate for pressing, and pressed laminate
JP6360766B2 (en) Damping structure and damping material
JP2740011B2 (en) Composite molding
JPH0576628A (en) Golf club head
JP3179971B2 (en) Composite molding
JPH0358835A (en) Composite molded product
JPH10128896A (en) Fiber reinforced resin laminated molded body
JPH09174765A (en) Composite molding
JP3144671B2 (en) Impact-resistant decorative board
JPH06297417A (en) High strength particle board and production thereof
JPH1134233A (en) Panel
JPH03236943A (en) Composite molded product composed of prepreg and molding material
JPH1061091A (en) Plate material of furniture, etc., and manufacture thereof
JP3124232B2 (en) Impact-resistant decorative board
JP3129606B2 (en) Composite molding
JPH0628946B2 (en) Impact resistant plate
JPH0834095A (en) High strength composite paper
JPH0121792Y2 (en)
JPS6342863A (en) Manufacture of curved-surface stone panel
JPH0788988A (en) Laminated form and manufacture thereof
JPS5852498B2 (en) Reinforced synthetic resin board
JPH10151708A (en) Carbon fiber composite molded product and manufacture thereof

Legal Events

Date Code Title Description
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20071211

Year of fee payment: 9

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20081211

Year of fee payment: 10

LAPS Cancellation because of no payment of annual fees