JPS63303732A - Extremely thin sheet - Google Patents
Extremely thin sheetInfo
- Publication number
- JPS63303732A JPS63303732A JP14052287A JP14052287A JPS63303732A JP S63303732 A JPS63303732 A JP S63303732A JP 14052287 A JP14052287 A JP 14052287A JP 14052287 A JP14052287 A JP 14052287A JP S63303732 A JPS63303732 A JP S63303732A
- Authority
- JP
- Japan
- Prior art keywords
- resin
- sheet
- extremely thin
- prepreg
- carbon
- 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
Links
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 19
- 239000004917 carbon fiber Substances 0.000 claims abstract description 19
- 229920005989 resin Polymers 0.000 claims abstract description 16
- 239000011347 resin Substances 0.000 claims abstract description 16
- 239000000835 fiber Substances 0.000 claims description 18
- 239000000463 material Substances 0.000 claims description 9
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 6
- 238000010030 laminating Methods 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 12
- 229910052799 carbon Inorganic materials 0.000 abstract description 12
- 238000000034 method Methods 0.000 abstract description 5
- 238000010438 heat treatment Methods 0.000 abstract description 2
- 238000010276 construction Methods 0.000 abstract 1
- 238000007796 conventional method Methods 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 229920002239 polyacrylonitrile Polymers 0.000 description 3
- 239000006185 dispersion Substances 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 229920005992 thermoplastic resin Polymers 0.000 description 2
- 229920001187 thermosetting polymer Polymers 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
- 241000252233 Cyprinus carpio Species 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
- 239000004696 Poly ether ether ketone Substances 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- JUPQTSLXMOCDHR-UHFFFAOYSA-N benzene-1,4-diol;bis(4-fluorophenyl)methanone Chemical compound OC1=CC=C(O)C=C1.C1=CC(F)=CC=C1C(=O)C1=CC=C(F)C=C1 JUPQTSLXMOCDHR-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000004922 lacquer Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229920003192 poly(bis maleimide) Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920002530 polyetherether ketone Polymers 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229920001567 vinyl ester resin Polymers 0.000 description 1
Landscapes
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、薄板バネ、X線透過板、ICカード、その他
各種用途に使用品る、優れた平面度を有する炭素繊維強
化極薄板に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a carbon fiber-reinforced ultra-thin plate having excellent flatness and used for thin plate springs, X-ray transmission plates, IC cards, and various other uses.
炭素繊維強化極薄板は、その繰返し曲げ疲労強度の高い
事、軽量で高剛性であること、X線透過性が優れている
こと、導電性、電磁波吸収性があること、等の特性のた
め、各種用途展開が期待されており、その具体例も提案
されている(実開昭60−145050号公報)。しか
し、極薄板の製造に際して、従来公知の炭素長繊維一方
向引揃え樹脂含浸されたプリプレグ(UDプリプレグ)
を積層し、常法によりプレス又はオートクレーブ成形さ
れたものは、表面の波打ち、凹凸、カーyを回避するこ
とは至難であることが判明した。Carbon fiber-reinforced ultra-thin plates have the following characteristics: high repeated bending fatigue strength, light weight and high rigidity, excellent X-ray transparency, electrical conductivity, and electromagnetic wave absorption properties. Various applications are expected, and specific examples thereof have been proposed (Japanese Utility Model Publication No. 145050/1983). However, when manufacturing ultra-thin plates, conventionally known prepreg (UD prepreg) impregnated with resin and unidirectionally aligned carbon long fibers is used.
It has been found that it is extremely difficult to avoid surface undulations, irregularities, and curves in products that are laminated and then pressed or autoclaved using conventional methods.
本発明者らは、波打ち、カー〜のない炭素繊維強化樹脂
極薄板を開発すべく、鋭意検討、を進めた結果、炭素短
繊維を用いた特殊一方向シートプリデレグを使用するこ
とが、波打ち、カールを抑え、かつ高度の物性を発揮し
得ることを見出し本発明に到達した。The inventors of the present invention have carried out intensive studies to develop an ultra-thin carbon fiber reinforced resin plate that is free from waving and curling. As a result, it has been found that the use of special unidirectional sheet Predeleg using short carbon fibers is effective against waving and curling. The present invention was achieved by discovering that it is possible to suppress the physical properties and exhibit high-level physical properties.
本発明の要旨は5〜100■の炭素繊維を一方向に配列
せしめたV−)状物に樹脂を含浸したプリプレグを単独
もしくは、炭素長繊維の一方向引揃えシートの樹脂含浸
プリプレグと併用して積層し加熱・加圧硬化して得られ
るα5冒以下の炭素繊維強化樹脂極薄板にある。The gist of the present invention is to use a prepreg made by impregnating a V-shaped material with 5 to 100 square carbon fibers arranged in one direction alone or in combination with a resin-impregnated prepreg made of a unidirectionally aligned sheet of long carbon fibers. This is an ultra-thin sheet of carbon fiber-reinforced resin with a diameter of α5 or less obtained by laminating the sheets and curing them under heat and pressure.
3〜100■の炭素短繊維の一方向配列シート状プリプ
レグは、例えば特開昭60−199996号公報等に記
載された方法により製造することができ、第1図に示す
ようにシートの長手方向に対して短繊維がほぼ直交配列
している。A unidirectionally arranged sheet-like prepreg of 3 to 100 square carbon short fibers can be produced, for example, by the method described in JP-A-60-199996. The short fibers are arranged almost orthogonally to the
具体的にはポリアクリロニトリル系高強度炭素m維を所
逼の長さに切断しつつ、分散溶媒に分散させ、回転体に
よる遠心力を使用して、連続的にP布に配列させ乾燥し
た後、熱硬化性もしくは熱可塑性樹脂をフィルム状又は
液膜状にて含浸させることにより得られる。Specifically, polyacrylonitrile-based high-strength carbon fibers are cut to a predetermined length, dispersed in a dispersion solvent, and then continuously arranged on a P cloth using the centrifugal force of a rotating body, and then dried. It can be obtained by impregnating a thermosetting or thermoplastic resin in the form of a film or liquid film.
又必要に応じ併用される炭素長繊維一方向引揃えプリプ
レグシートは、連続炭素繊維シート状物に従来公知のホ
ットメルト法、ラッカー法、フィルム含浸法等により製
造したものが使用される。Further, the carbon long fiber unidirectionally aligned prepreg sheet, which is used in combination as necessary, is produced by a conventional method such as a hot melt method, a lacquer method, a film impregnation method, etc. on a continuous carbon fiber sheet.
極薄板の成形は、上記炭素短繊維一方向プリプレグを一
方向又は0/90°、0/+45°/−45゜/906
等、適宜配列角度を組合せて積層する。The ultra-thin plate is formed by using the short carbon fiber unidirectional prepreg in one direction or at 0/90°, 0/+45°/-45°/906
etc., are laminated by combining the arrangement angles as appropriate.
このとき平面度を上げるため上下鏡面対称構成となるよ
う配列して積層することが囁ましい。At this time, in order to increase the flatness, it is recommended that the layers be arranged and stacked so as to have a symmetrical configuration with upper and lower mirror surfaces.
又、併用する炭素長繊維一方向プリプレグを使用すると
きは上記短繊維プリプレグの一部を長繊維で置き替えて
上下鏡面対称となるように配列積層する。When using carbon long fiber unidirectional prepreg, a part of the short fiber prepreg is replaced with long fibers, and the fibers are arranged and laminated in a mirror-symmetrical manner.
このように配列されたプリプレグは、使用樹脂の特性に
合せて加熱されたプレス又はオートクレーブにより加圧
又はバッグ真空下に加圧し本発明の極薄プリプレグとす
る。The prepregs arranged in this manner are pressurized with a heated press or autoclave or under a bag vacuum depending on the characteristics of the resin used to obtain the ultra-thin prepregs of the present invention.
極薄成形品を得るためには既述のプリプレグの厚みは(
LO5mam以下、好ましくはCLO25+m以下の薄
手プリプレグを使用することが望ましい。In order to obtain an ultra-thin molded product, the thickness of the prepreg mentioned above must be (
It is desirable to use a thin prepreg with a LO5mam or less, preferably a CLO25+m or less.
使用するマトリックス樹脂はエポキシ、ビニルエステル
、ポリエステル、フェノール、ビスマレイミド等の熱硬
化性樹脂の他p p S 1PEA。The matrix resins used include thermosetting resins such as epoxy, vinyl ester, polyester, phenol, and bismaleimide, as well as pp S 1PEA.
PEEK、ポリアミド、ポリエステル等の熱可塑性樹脂
を使用することが出来る。Thermoplastic resins such as PEEK, polyamide, polyester, etc. can be used.
又、使用する炭素繊維は、ポリアクリロニトリル、ピッ
チ等を原料とする高強度、高弾性炭素繊維が好ましく使
用出来る。Furthermore, the carbon fibers used are preferably high strength and high elasticity carbon fibers made from polyacrylonitrile, pitch, or the like.
炭素短繊維一方向プリプレグを使用することによシ、加
熱・加圧成形によって繊維と樹脂の成形収縮率の差が吸
収され成形品の歪みがなく、波打ち、反シ、カーpのな
い極薄板を得ることが出来、かつ、一方向材の特性であ
る、高強度、高弾性、高耐久性の特徴が損なわれないた
め、軽量、高剛性、耐久性、X線透過性の要求されるカ
メラ用バネ材その他各種バネ材、X線用ブリード面材、
防護板、ICカード、電卓底バネ〜その他各種用途に使
用することが出来る。By using short carbon fiber unidirectional prepreg, the difference in molding shrinkage rate between the fiber and resin is absorbed by heating and pressure molding, resulting in an ultra-thin plate without distortion of the molded product, and without waving, warping, or carp. It can be used for cameras that require light weight, high rigidity, durability, and X-ray transparency. spring materials and other various spring materials, bleed surface materials for X-rays,
It can be used for various purposes such as protective plates, IC cards, calculator bottom springs, etc.
以下実施例によシ本発明を具体的に説明する。 The present invention will be specifically explained below using examples.
実施例1
ポリアクリロニトリル系高強度炭素繊維(強度S 50
kg7m” 、弾性率24 Ton/’min )を
約6−にカットしつつ、分散溶媒に分散させ、遠心力を
利用して連続的にP布に一方向に配列させ、乾燥し、シ
ート状物とし、エポキシ樹脂フィルムを融着含浸させる
ことにより、1025m厚みの炭素短繊維一方向配列シ
ートプリプレグ囚を得た。Example 1 Polyacrylonitrile-based high-strength carbon fiber (strength S 50
kg7m", elastic modulus 24 Ton/'min), are cut into approximately 6-mm pieces, dispersed in a dispersion solvent, continuously arranged in one direction on a P cloth using centrifugal force, dried, and made into a sheet-like material. By fusing and impregnating an epoxy resin film, a unidirectionally aligned carbon short fiber sheet prepreg having a thickness of 1025 m was obtained.
一方炭素長繊維一方向シートに対し、エポキシ樹脂フィ
ルムを融着含浸させたαD 25m+厚みの炭素長繊維
一方向引揃えシートプリプレグCB)を用意した。On the other hand, a carbon long fiber unidirectional sheet prepreg CB) having an αD of 25 m+thickness and fused and impregnated with an epoxy resin film was prepared for the carbon long fiber unidirectional sheet.
(:)上記短繊維プリプレグ囚を0°/90°10゜の
繊維配向となるよう交互積層し、常法によりオートクレ
ーブ成形することにより、第2図に示すような厚みa0
75mmの平面度の優れた極薄板を得た。(:) The above-mentioned short fiber prepregs are laminated alternately so that the fiber orientation is 0°/90°10°, and by autoclave molding using a conventional method, a thickness a0 as shown in Fig. 2 is obtained.
An ultra-thin plate of 75 mm with excellent flatness was obtained.
この板は強度、弾性率に優れ、X線整波用グリッド面材
として好適であった。This plate had excellent strength and elastic modulus, and was suitable as a grid surface material for X-ray wave regulation.
(11)短繊維プリプレグ囚を中間層に長繊維プリプレ
グ(A))を上下層に積層して、0°790°10゜の
構成を有する厚みαO75mのハイブリッド構成の平面
度の優れた極薄板を得た。(11) An ultra-thin board with excellent flatness of a hybrid structure with a thickness αO of 75 m and a structure of 0°790°10°, by laminating short fiber prepreg in the middle layer and long fiber prepreg (A)) in the upper and lower layers. Obtained.
この平板は0°方向の弾性率、強度が大きく振動耐久性
が大きいため優れたカメラ部品用板バネとして使用する
ことが出来た。This flat plate had a high elastic modulus in the 0° direction, high strength, and high vibration durability, so it could be used as an excellent leaf spring for camera parts.
比較例1
長繊維プリプレグ囚のみを用いて、0°/90”70″
の交互積層を行ない実施例1(1)と同様にして007
5−の極薄板を成形し九ところ、得られた平板は波打ち
と反りが発現した。Comparative Example 1 Using only long fiber prepreg, 0°/90"70"
007 in the same manner as in Example 1 (1) by laminating alternately.
When an extremely thin plate of No. 5 was molded, the obtained flat plate developed waving and warping.
この平板を用いてグリッド用面板、板バネとして使用す
る場合形顔が不安定であり、使用用途が限定された。When this flat plate was used as a face plate for a grid or a leaf spring, the shape was unstable and its usage was limited.
東回面の簡単な説明
第1図は、本発明で使用する炭素短繊維の一方向配列シ
ートの平面図、第2図は本発明で得られる極薄板の一例
を示す斜視図を各示す。Brief Explanation of the Eastern Plane FIG. 1 is a plan view of a unidirectionally arranged sheet of short carbon fibers used in the present invention, and FIG. 2 is a perspective view showing an example of an ultra-thin plate obtained by the present invention.
Claims (1)
たシート状物に樹脂を含浸したプリプレグを積層し、加
熱・加圧硬化して得られる0.3mm以下の炭素繊維強
化樹脂極薄板。 2、繊維長3〜100mmの炭素繊維を一方向に配列せ
しめたシート状物に樹脂を含浸したプリプレグ(A)と
炭素長繊維を一方向に引揃えたシート状物に樹脂を含浸
したプリプレグ(B)を任意の割合で積層し、加熱・加
圧硬化して得られる0.3mm以下の炭素繊維強化樹脂
極薄板。[Claims] 1. Carbon fibers of 0.3 mm or less obtained by laminating resin-impregnated prepreg on a sheet-like material in which short carbon fibers of 1.3 to 100 mm are arranged in one direction, and curing under heat and pressure. Fiber-reinforced resin ultra-thin plate. 2. Prepreg (A), which is a sheet-like material in which carbon fibers with a fiber length of 3 to 100 mm are arranged in one direction and impregnated with resin; and prepreg (A), in which a sheet-like material in which long carbon fibers are arranged in one direction is impregnated with resin. An ultra-thin carbon fiber reinforced resin plate of 0.3 mm or less obtained by laminating B) in an arbitrary ratio and curing under heat and pressure.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62140522A JPH0624726B2 (en) | 1987-06-04 | 1987-06-04 | Ultra thin plate |
JP4055484A JPH05113590A (en) | 1987-06-04 | 1992-03-13 | Spring material for camera |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62140522A JPH0624726B2 (en) | 1987-06-04 | 1987-06-04 | Ultra thin plate |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4055484A Division JPH05113590A (en) | 1987-06-04 | 1992-03-13 | Spring material for camera |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63303732A true JPS63303732A (en) | 1988-12-12 |
JPH0624726B2 JPH0624726B2 (en) | 1994-04-06 |
Family
ID=15270619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62140522A Expired - Lifetime JPH0624726B2 (en) | 1987-06-04 | 1987-06-04 | Ultra thin plate |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0624726B2 (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05113590A (en) * | 1987-06-04 | 1993-05-07 | Mitsubishi Rayon Co Ltd | Spring material for camera |
JP2002069811A (en) * | 2000-04-14 | 2002-03-08 | Tung-Siang Lin | Method for molding carbon fiber layer |
JP2010095208A (en) * | 2008-10-20 | 2010-04-30 | Nsk Ltd | Steering shaft |
JP2011231297A (en) * | 2010-04-30 | 2011-11-17 | Wisukaa Kk | Resin composite material and adhesive |
JP2012036284A (en) * | 2010-08-06 | 2012-02-23 | Panefuri Kogyo Kk | Electroconductive resin sheet |
JP2012051151A (en) * | 2010-08-31 | 2012-03-15 | Toray Ind Inc | Fiber reinforced molding |
JP2012111909A (en) * | 2010-11-26 | 2012-06-14 | Panasonic Corp | Fiber-reinforced plastic flat plate and manufacturing method thereof |
JP2012169347A (en) * | 2011-02-10 | 2012-09-06 | Panasonic Corp | Casing, and electronic apparatus |
JP2014062886A (en) * | 2012-08-30 | 2014-04-10 | Casio Comput Co Ltd | Indicator |
JP2014062915A (en) * | 2012-08-30 | 2014-04-10 | Casio Comput Co Ltd | Indicator |
JP2017057255A (en) * | 2015-09-15 | 2017-03-23 | 本田技研工業株式会社 | Fiber-reinforced resin base material sheet and method for confirming internal flow of fiber-reinforced resin base material sheet |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61229546A (en) * | 1985-04-05 | 1986-10-13 | 三菱レイヨン株式会社 | Fiber reinforced plastic molded shape |
-
1987
- 1987-06-04 JP JP62140522A patent/JPH0624726B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61229546A (en) * | 1985-04-05 | 1986-10-13 | 三菱レイヨン株式会社 | Fiber reinforced plastic molded shape |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05113590A (en) * | 1987-06-04 | 1993-05-07 | Mitsubishi Rayon Co Ltd | Spring material for camera |
JP2002069811A (en) * | 2000-04-14 | 2002-03-08 | Tung-Siang Lin | Method for molding carbon fiber layer |
JP2010095208A (en) * | 2008-10-20 | 2010-04-30 | Nsk Ltd | Steering shaft |
JP2011231297A (en) * | 2010-04-30 | 2011-11-17 | Wisukaa Kk | Resin composite material and adhesive |
JP2012036284A (en) * | 2010-08-06 | 2012-02-23 | Panefuri Kogyo Kk | Electroconductive resin sheet |
JP2012051151A (en) * | 2010-08-31 | 2012-03-15 | Toray Ind Inc | Fiber reinforced molding |
JP2012111909A (en) * | 2010-11-26 | 2012-06-14 | Panasonic Corp | Fiber-reinforced plastic flat plate and manufacturing method thereof |
JP2012169347A (en) * | 2011-02-10 | 2012-09-06 | Panasonic Corp | Casing, and electronic apparatus |
US8913373B2 (en) | 2011-02-10 | 2014-12-16 | Panasonic Corporation | Housing and electronic device |
JP2014062886A (en) * | 2012-08-30 | 2014-04-10 | Casio Comput Co Ltd | Indicator |
JP2014062915A (en) * | 2012-08-30 | 2014-04-10 | Casio Comput Co Ltd | Indicator |
US10061270B2 (en) | 2012-08-30 | 2018-08-28 | Casio Computer Co., Ltd. | Pointer and pointer manufacturing method |
JP2017057255A (en) * | 2015-09-15 | 2017-03-23 | 本田技研工業株式会社 | Fiber-reinforced resin base material sheet and method for confirming internal flow of fiber-reinforced resin base material sheet |
Also Published As
Publication number | Publication date |
---|---|
JPH0624726B2 (en) | 1994-04-06 |
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