JPS59118829A - Method for shaping composite material - Google Patents

Method for shaping composite material

Info

Publication number
JPS59118829A
JPS59118829A JP22664782A JP22664782A JPS59118829A JP S59118829 A JPS59118829 A JP S59118829A JP 22664782 A JP22664782 A JP 22664782A JP 22664782 A JP22664782 A JP 22664782A JP S59118829 A JPS59118829 A JP S59118829A
Authority
JP
Japan
Prior art keywords
shape
composite material
impregnated
temp
core
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
Application number
JP22664782A
Other languages
Japanese (ja)
Inventor
Yoshihiko Kanchiku
寒竹 嘉彦
Shinya Hiyama
樋山 真也
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.)
Mitsubishi Rayon Co Ltd
Original Assignee
Mitsubishi Rayon 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 Mitsubishi Rayon Co Ltd filed Critical Mitsubishi Rayon Co Ltd
Priority to JP22664782A priority Critical patent/JPS59118829A/en
Publication of JPS59118829A publication Critical patent/JPS59118829A/en
Pending legal-status Critical Current

Links

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  • Laminated Bodies (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

PURPOSE:To manufacture easily a shaped composite material of a complex shape at a low cost by laminating reinforcing fiber impregnated with a matrix on a core body made of a shape memory alloy, and shaping them after heating to a temp. above the memorized shape developing temp. CONSTITUTION:A shape memory alloy such as a Ti-Ni alloy is formed into a prescribed shape and drawn to obtain a core body. Reinforcing fiber such as glass fiber is impregnated with a matrix such as epoxy resin or polyamide, and the impregnated fiber is laminated on the core body. They are shaped after heating to a temp. above the memorized shape developing temp. A composite material of a prescribed complex shape is efficiently manufactured.

Description

【発明の詳細な説明】 本発明は形状記憶合金を複合材の成形用芯体として用い
た複合材の成形法に感するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention is directed to a method of forming a composite material using a shape memory alloy as a core for forming the composite material.

ガラス繊維、炭素繊維、芳香族ポリアミド繊維、7ソコ
ンカーバイト繊維の性能向上は近年目覚しいものであり
、これら補強用繊維に、エポキシ樹脂、不飽和ポリエス
テル樹脂、ポリイミド、フェノール樹脂等の熱硬化性樹
脂や、ポリアミド、ポリエステル、ポリカーボネート、
pps、、PPO、ポリエーテルエーテルケトン、AB
S等の熱可塑性樹脂を含浸した複合材は、ゴルフシャフ
ト、釣竿などのスポーツレジャー分野での利用ばかシで
なく、航空機用素材、自動車構造材等の工業用途での利
用が活発になってきている。
The performance of glass fibers, carbon fibers, aromatic polyamide fibers, and 7-carbon carbide fibers has improved dramatically in recent years, and thermosetting resins such as epoxy resins, unsaturated polyester resins, polyimides, and phenolic resins are being used as reinforcing fibers for these fibers. , polyamide, polyester, polycarbonate,
pps, , PPO, polyetheretherketone, AB
Composite materials impregnated with thermoplastic resins such as S are not only used in sports and leisure fields such as golf shafts and fishing rods, but are also increasingly being used in industrial applications such as aircraft materials and automobile structural materials. There is.

これら複合材の成形は平板形状、円柱、角柱形状等の比
較的単純な形状のものでは比較的簡単なのであるが、曲
面を有する成形体、例えばコイルスプリング、トーンア
ーム、ゴルフパターシャフト、ラケットフレーム等への
成形は極めて難しく、複雑で高価な金型の作成なくして
は実施不可能な現況にある。
Molding of these composite materials is relatively easy for relatively simple shapes such as flat plate shapes, cylinders, and prismatic shapes, but molded products with curved surfaces such as coil springs, tone arms, golf putter shafts, racket frames, etc. Molding is extremely difficult and is currently impossible without the creation of complex and expensive molds.

そこで、本発明者等は複合材のより一層改良された成形
法を開発すべく検討中のところ形状記憶合金を芯型に用
いることによって、複雑な形状を有する複合材製成形物
も容易に、かつ、安価に作り得ることを見出し本発明を
完成した。
Therefore, the present inventors are currently considering developing a further improved molding method for composite materials.By using a shape memory alloy for the core mold, molded composite materials with complex shapes can be easily formed. Moreover, they discovered that it can be manufactured at low cost and completed the present invention.

本発明の要旨とするところは形状記憶合金製芯体にマト
リックスを含浸した補強繊維素材を積層し、芯体の記憶
形状詔醐迂社に加温して積層体を付形し成形することを
特徴とする複合材の成形方法にある。
The gist of the present invention is to laminate a reinforcing fiber material impregnated with a matrix on a core made of a shape memory alloy, and shape and mold the laminate by heating the core to form a memory shape. The main feature lies in the method of forming the composite material.

本発明を実施するに際して用いる形状記憶合金の具体例
としては0u−Zn−At系合金、Ti−Ni系合金、
CuZ n −Z n系合金Fe−Pt系合金など種々
(7)4のを用いることができるが、とくに記憶形状発
現〃171度が室温以上で、マトリックスの流動温度以
下なるもの全選定するのがよい。Ni−Tl系合金の形
状発現温度の一例を示すと次の如くなる。
Specific examples of shape memory alloys used in carrying out the present invention include Ou-Zn-At alloy, Ti-Ni alloy,
Various materials (7) 4 can be used, such as CuZ n -Z n alloys, Fe-Pt alloys, etc., but in particular, it is recommended to select all those whose memory shape development is 171 degrees above room temperature and below the flow temperature of the matrix. good. An example of the shape development temperature of Ni--Tl alloy is as follows.

また、形状記憶合金は上述した如き特異な性能を示す他
、その振動減衰性に優れるという%徴も合せ持っておシ
、良好な振動減衰性を要求されるトーンアーム、ゴルフ
ノ4ターシャフト、ラケット、ラケットフレームなどに
於ては芯体を抜くことなく、その捷ま芯体を複合した成
形体として利用するとともできる。
In addition to the above-mentioned unique performance, shape memory alloys also have excellent vibration damping properties, and are used in tone arms, golf players' shafts, and rackets that require good vibration damping properties. In racket frames and the like, the twisted core can be used as a composite molded product without removing the core.

本発明を実施するに際して用いる補強用繊維としては前
述した補強用繊維類を、マトリックスとしては、11J
述した如き熱硬化性樹脂、熱可塑性樹脂類を主体として
用いる。補強用繊維へのマトリックスの含浸は、芯体へ
のこれらの素材の積層前に行なうもの、或いは芯体へこ
れら補強用繊維を積層した後、マトリックス含浸する方
法等を用いることができるが、補強用繊維の引揃えソー
トにマ) l)ツクスを含浸したプリプレグ、或いはス
クリムクロス補強プリプレグ、クロスプリプレグ、ロー
ビング状プリプレグ、シートモールディング材、バルク
モールディング材などの形として用いることもできる。
The reinforcing fibers used in carrying out the present invention are the above-mentioned reinforcing fibers, and the matrix is 11J.
Thermosetting resins and thermoplastic resins as mentioned above are mainly used. The reinforcing fibers can be impregnated with the matrix before these materials are laminated to the core, or the reinforcing fibers are laminated to the core and then impregnated with the matrix. It can also be used in the form of prepreg impregnated with tux, scrim cloth reinforced prepreg, cloth prepreg, roving-like prepreg, sheet molding material, bulk molding material, etc.

又、本発明による複合材の成形は、熱収縮性グラスチッ
クやゴムの管体を被包して成形する方法、熱収縮性テー
プを用いる方法の他、金型を補助的に用いる方法、オー
トクレーブを用いる方法などによって成形することがで
きる。
In addition, the composite material according to the present invention can be molded by encapsulating and molding a heat-shrinkable glass or rubber tube, by using a heat-shrinkable tape, by using a mold as an auxiliary method, and by using an autoclave. It can be molded by a method such as using

本発明の複合材の成形法は従来開発されてきた方法に比
べ特に複雑な形状を有するものの成形法として、極めて
効率的な方法である。
The method for molding a composite material of the present invention is an extremely efficient method for molding materials having particularly complex shapes compared to conventionally developed methods.

以下実施例により本発明を更に詳細に説明する。The present invention will be explained in more detail with reference to Examples below.

実施例1 形状発現温度90CのNi−Ti系合金で径1航なるコ
イルスプリングを作シ、このものを引伸ばしてコイルス
プリング成形芯体とした、この芯体にエポキシ樹脂を含
浸した炭素繊維補強ストランドをフィラメントワインデ
ィング法にて糸角度が±4()度になるように巻き付け
た后、熱収縮性シリコンチューブで被包し、90C以上
に加温したところ、コイルスプリングの記憶形状にもど
った。
Example 1 A coil spring with a diameter of 1 was made from a Ni-Ti alloy with a shape development temperature of 90C, and this was stretched to form a coil spring core.This core was reinforced with carbon fibers impregnated with epoxy resin. After the strand was wound using a filament winding method so that the thread angle was ±4 () degrees, it was wrapped in a heat-shrinkable silicone tube and heated to 90C or higher, and it returned to the memorized shape of a coil spring.

この時のエポキシ樹脂は十分な流動性を有していた。コ
イルスプリング形状となった複合材を、内径保持のだめ
の補助材を挿入し、オートクレーブ中で加熱し、エポキ
シ樹脂の硬化を行った后、補助拐を抜き、シリコンチュ
ーブを除いたところ、炭素繊維の配向角がスプリング軸
に対し、はソ±45度になった炭素繊維強化樹脂製コイ
ルスプリングが得られた。
The epoxy resin at this time had sufficient fluidity. The composite material in the shape of a coil spring was inserted with an auxiliary material to hold the inner diameter, heated in an autoclave to cure the epoxy resin, and then the auxiliary material was removed and the silicone tube was removed. A carbon fiber reinforced resin coil spring with an orientation angle of ±45 degrees with respect to the spring axis was obtained.

実施例11 実施例1で用いた合金にて記憶形状がくの字型の中空状
の芯体を作シ、このものを引伸ばしてはソ直すぐな円筒
体を用意した。この円筒体に炭素繊維引揃えノートにエ
ポキシ樹脂を含浸したプリプレグにガラススクリムクロ
スで補強したものを炭素繊維軸が前記円筒体とはヌ平行
となるようにチプライ巻付け、シリコン樹脂チューブを
被包し、90C以上の温度に加温したところ、くの字型
の形状に変形した。更に、このものをオートクレーブ中
にて加熱し、樹脂を硬化した后、シリコン樹脂チューブ
を除去したところ、くの字型の炭素繊維強化複合材製曲
管が得られた。
Example 11 A hollow core body with a memory shape of a dogleg shape was made from the alloy used in Example 1, and this core body was stretched to prepare a straight cylindrical body. A prepreg made of epoxy resin-impregnated carbon fiber notebook and reinforced with glass scrim cloth is wrapped around this cylinder so that the carbon fiber axis is parallel to the cylinder, and a silicone resin tube is encapsulated. However, when it was heated to a temperature of 90C or higher, it deformed into a dogleg shape. Furthermore, this product was heated in an autoclave to cure the resin, and then the silicone resin tube was removed to obtain a dogleg-shaped bent pipe made of carbon fiber reinforced composite material.

実施例■ 実施例1で用いた合金にて半円弧状板状体を記憶形状と
する平板を作り、炭素繊維織物にエポキシ樹脂を含浸し
たクロスプリプレグを前記平板の両面に貼りつけた后、
9(1”以上に加温したところ、記憶形状を発現した。
Example ■ A flat plate having a memorized shape of a semicircular arc plate was made from the alloy used in Example 1, and a cross prepreg made of carbon fiber fabric impregnated with epoxy resin was attached to both sides of the flat plate.
9 (When heated to 1" or higher, a memorized shape was developed.

このとき、クロスプリプレグは、記憶形状に良好に追随
した。このものを型金に入れ加熱硬化することによって
半円弧状の炭素繊維強化複合材製板状体が得られた。
At this time, the cross prepreg followed the memorized shape well. This material was placed in a mold and heated to harden to obtain a semicircular arc-shaped plate made of carbon fiber reinforced composite material.

特許出願人 三菱レイヨン株式会社 代理人 弁理士 1)村 武 敏 手  続  補  正  書 く方式)昭和58年4月
10? 日 特許庁長官  若  杉  和  夫  殿1、事件の
表示 昭和57年特許願第226647号 2、発明の名称 複合制の成形法 3、補正をする者 事(’lとの関係 特許出願人 東京都中央区京橋二丁目3番19号 (603)三菱レイヨン株式会社 取締役社長  金 澤 脩 三 4、代理人 東以都港区虎ノ門二丁目8番1号
Patent Applicant Mitsubishi Rayon Co., Ltd. Agent Patent Attorney 1) Toshite Mura (Continuation Amendment Writing Method) April 10, 1982? Kazuo Wakasugi, Commissioner of the Japan Patent Office1, Indication of the case, Patent Application No. 226647 of 1982,2 Forming method for compound title of invention3, Person making the amendment (relationship with 'l) Patent applicant Tokyo 2-3-19 Kyobashi, Chuo-ku (603) Osamu Kanazawa, President and Director of Mitsubishi Rayon Co., Ltd., 34, Agent 2-8-1 Toranomon, Higashiito Minato-ku

Claims (1)

【特許請求の範囲】[Claims] 形状記憶合金製芯体にマトリックス含浸補強繊維を積層
し、記憶形状発現温度以上に加温して付形し成形するこ
とを特徴とする複合材の成形法。
A method for forming a composite material, which is characterized by laminating matrix-impregnated reinforcing fibers on a core made of a shape memory alloy, and shaping and molding the core by heating it to a temperature above the memory shape development temperature.
JP22664782A 1982-12-27 1982-12-27 Method for shaping composite material Pending JPS59118829A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22664782A JPS59118829A (en) 1982-12-27 1982-12-27 Method for shaping composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22664782A JPS59118829A (en) 1982-12-27 1982-12-27 Method for shaping composite material

Publications (1)

Publication Number Publication Date
JPS59118829A true JPS59118829A (en) 1984-07-09

Family

ID=16848453

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22664782A Pending JPS59118829A (en) 1982-12-27 1982-12-27 Method for shaping composite material

Country Status (1)

Country Link
JP (1) JPS59118829A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020051461A (en) * 2000-12-22 2002-06-29 신현준 Fabrication method of metal matrix composite using shape memory alloys as reinforcing agent
KR100431828B1 (en) * 2001-12-22 2004-05-17 재단법인 포항산업과학연구원 Fabrication method of metal metrix composite reinforced by shape memory alloy
JP2014075431A (en) * 2012-10-03 2014-04-24 Fujitsu Ltd Apparatus case and manufacturing method therefor
US9603288B2 (en) 2012-04-23 2017-03-21 Hyundai Motor Company Electronic/electrical component housing with strips of metal plate and shape memory material forming a heat transfer path

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020051461A (en) * 2000-12-22 2002-06-29 신현준 Fabrication method of metal matrix composite using shape memory alloys as reinforcing agent
KR100431828B1 (en) * 2001-12-22 2004-05-17 재단법인 포항산업과학연구원 Fabrication method of metal metrix composite reinforced by shape memory alloy
US9603288B2 (en) 2012-04-23 2017-03-21 Hyundai Motor Company Electronic/electrical component housing with strips of metal plate and shape memory material forming a heat transfer path
US10375858B2 (en) 2012-04-23 2019-08-06 Hyundai Motor Company Electronic/electrical component housing with strips of metal plate and shape memory material forming a heat transfer path
JP2014075431A (en) * 2012-10-03 2014-04-24 Fujitsu Ltd Apparatus case and manufacturing method therefor

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