JPH0761688B2 - Repair method of carbon fiber reinforced carbon composite material - Google Patents

Repair method of carbon fiber reinforced carbon composite material

Info

Publication number
JPH0761688B2
JPH0761688B2 JP62136488A JP13648887A JPH0761688B2 JP H0761688 B2 JPH0761688 B2 JP H0761688B2 JP 62136488 A JP62136488 A JP 62136488A JP 13648887 A JP13648887 A JP 13648887A JP H0761688 B2 JPH0761688 B2 JP H0761688B2
Authority
JP
Japan
Prior art keywords
composite material
carbon fiber
carbon
fiber reinforced
carrier
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 - Lifetime
Application number
JP62136488A
Other languages
Japanese (ja)
Other versions
JPS63297031A (en
Inventor
正剛 阪上
幸一 岩田
幸典 山下
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 Electric Industries Ltd
Original Assignee
Sumitomo Electric Industries 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 Electric Industries Ltd filed Critical Sumitomo Electric Industries Ltd
Priority to JP62136488A priority Critical patent/JPH0761688B2/en
Publication of JPS63297031A publication Critical patent/JPS63297031A/en
Publication of JPH0761688B2 publication Critical patent/JPH0761688B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は、炭素繊維強化炭素複合材料の補修方法に関す
る。
TECHNICAL FIELD The present invention relates to a method for repairing a carbon fiber reinforced carbon composite material.

[従来技術と問題点] 現在、炭素繊維強化炭素複合材料の接合技術がないた
め、摩擦・摩耗あるいは消耗した複合材料は、廃却する
ほかなかった。この種複合材料は非常に高価であるた
め、経済的に大きな損失である。
[Prior Art and Problems] At present, since there is no bonding technology for carbon fiber reinforced carbon composite materials, the composite materials that have been rubbed, worn or consumed have to be discarded. Since this kind of composite material is very expensive, it is a great economical loss.

このような炭素繊維強化炭素複合材料は、例えば自動車
ディスクブレーキ用パッドに使用されている。
Such carbon fiber reinforced carbon composite materials are used, for example, in automobile disc brake pads.

[発明の構成] 本発明は、摩擦・摩耗、もしくは消耗、または板厚の薄
い炭素繊維強化炭素複合材料の補修を目的としてなされ
たものであって、炭素繊維強化炭素複合材料の表面に電
着法を用いて炭素質粉末および担体を析出させ、次に同
じく電着法により炭素繊維に炭素質粉末および担体を析
出させた被覆物を前記炭素繊維強化炭素複合材料に重
ね、もしくは、炭素繊維強化炭素複合材料の表面に電着
法を用いて炭素質粉末および担体を析出させたもの同志
を重ね、加圧・加熱により一体化したのち焼成する炭素
繊維強化炭素複合材料を補修する方法である。
[Structure of the Invention] The present invention has been made for the purpose of repairing a carbon fiber reinforced carbon composite material having a thin plate thickness such as friction, wear, or wear, and electrodeposition is performed on the surface of the carbon fiber reinforced carbon composite material. Method to deposit carbonaceous powder and carrier, and then deposit carbonaceous powder and carrier on carbon fiber by the same electrodeposition method. This is a method of repairing a carbon fiber reinforced carbon composite material in which carbonaceous powder and a carrier are deposited on the surface of a carbon composite material by using an electrodeposition method, and the carbon fiber reinforced carbon composite material is fired after being integrated by pressing and heating.

このような補修方法は、炭素繊維およびその複合材料に
導電性があるため、電着法の適用に着目してなされたも
のである。
Such a repairing method is made by paying attention to the application of the electrodeposition method because the carbon fiber and the composite material thereof have conductivity.

本発明の方法は次のとおりである。すなわち、炭素質の
微粉末に、液体中でイオン化しうる担体を吸着させたの
ち、液体中に分散させる。
The method of the present invention is as follows. That is, a carrier which can be ionized in a liquid is adsorbed to the carbonaceous fine powder and then dispersed in the liquid.

その後、摩擦・摩耗もしくは消耗によって板厚が減少し
たあるいは、元々板厚の薄い炭素繊維強化炭素複合材料
と対向電極とを、前記の分散液に浸漬し、前記複合材料
と対向電極との間に直流電圧を印加して炭素質微粉末お
よび担体を前記複合材料表面に析出させる。
Thereafter, the plate thickness is reduced by friction, wear, or consumption, or the carbon fiber-reinforced carbon composite material originally having a thin plate thickness and the counter electrode are immersed in the dispersion liquid, and the composite material and the counter electrode are placed between the composite material and the counter electrode. A DC voltage is applied to deposit the carbonaceous fine powder and the carrier on the surface of the composite material.

他方、前記分散液に炭素繊維基材を浸漬し、炭素繊維基
材と対向電極との間に直流電圧を印加し、炭素粉末およ
び担体を炭素繊維基材表面に析出させて被覆物を得る。
On the other hand, a carbon fiber base material is immersed in the dispersion liquid, a direct current voltage is applied between the carbon fiber base material and the counter electrode, and carbon powder and a carrier are deposited on the surface of the carbon fiber base material to obtain a coating.

このように被覆された炭素繊維強化複合材料と炭素繊維
基材を乾燥し、重ねて加圧・加熱成形により一体化した
のち、炭化焼成を行う。
The carbon fiber reinforced composite material and the carbon fiber base material coated in this manner are dried, overlapped and integrated by pressure / heat molding, and then carbonized and fired.

炭素繊維強化炭素複合材料は導電性があるため、液体中
でイオン化しうる担体を用いることで、炭素質粉末や樹
脂を強固に密着させることができ、そのため炭素粉末や
樹脂を被覆させた炭素繊維強化複合材料と被覆炭素繊維
を加圧・加熱により一体化成形後焼成すると300〜900℃
間で炭素質粉末が軟化し、界面のぬれおよび化学反応に
よって焼成物は一体化された炭素繊維強化複合材料とな
るのである。
Since the carbon fiber reinforced carbon composite material has conductivity, it is possible to firmly adhere the carbonaceous powder and the resin by using the carrier that can be ionized in the liquid, and therefore the carbon fiber coated with the carbon powder or the resin is used. 300-900 ℃ when reinforced composite material and coated carbon fiber are integrally molded by pressure and heating and then fired
The carbonaceous powder softens in the meantime, and the fired product becomes an integrated carbon fiber reinforced composite material due to the wetting of the interface and the chemical reaction.

なお、炭素繊維基材としては、単繊維を束ねたひも状の
もの、織布、ペーパー状不織布を用いることができ、担
体はポリアクリロニトリル樹脂誘導体もしくは、熱硬化
性樹脂誘導体を改質して電着可能な樹脂としたものを用
いる。
As the carbon fiber base material, a string-like material obtained by bundling single fibers, a woven fabric, or a paper-like non-woven fabric can be used, and the carrier is modified by modifying a polyacrylonitrile resin derivative or a thermosetting resin derivative. A resin that can be attached is used.

以下実施例について説明する。Examples will be described below.

[実施例1] (1)摩擦・摩耗した炭素繊維強化複合材料の表面を平
面研削して表面の平行度を出した。(形状φ250×t7m
m) (2)その後、電着しやすいように表面を適当に荒らし
た。
[Example 1] (1) The surface of the carbon fiber reinforced composite material that was rubbed and worn was surface-ground to obtain the parallelism of the surface. (Shape φ250 × t7m
m) (2) After that, the surface was appropriately roughened so as to facilitate electrodeposition.

(3)この炭素繊維強化複合材料に、自己焼結性炭素質
粉末と担体樹脂が重量比で1対1の電着被覆を形成させ
た。
(3) On this carbon fiber reinforced composite material, a self-sintering carbonaceous powder and a carrier resin formed an electrodeposition coating in a weight ratio of 1: 1.

(4)また、重量比で自己焼結性炭素粉末と担体樹脂と
炭素繊維布が1対1対1のφ250の被覆物を電着法で80
枚作成し、被覆された炭素繊維強化炭素複合材料と一緒
に成形した。温度200℃、加圧力20kg/cm2、10分間加熱
による。
(4) Also, a self-sintering carbon powder, a carrier resin, and a carbon fiber cloth in a weight ratio of 1: 250 with a diameter of 250 are applied by electrodeposition.
Sheets were made and molded with the coated carbon fiber reinforced carbon composite material. By heating at a temperature of 200 ℃ and a pressure of 20kg / cm 2 for 10 minutes.

(5)これらの成形体を3メッシュの金網でクランプし
ながら大気中で250℃、280℃の各温度でそれぞれ3時間
加熱し、熱処理を行った。
(5) These compacts were heated in the atmosphere at 250 ° C. and 280 ° C. for 3 hours, respectively, while being clamped with a 3-mesh wire net, to perform heat treatment.

(6)この熱処理体を不活性雰囲気中で500kg/cm2で面
圧下で30℃/時の昇温温度で2000℃まで昇温して炭素繊
維強化炭素複合材料を焼成した。
(6) The heat-treated body was heated in an inert atmosphere at 500 kg / cm 2 under surface pressure to 2000 ° C. at a temperature rising rate of 30 ° C./hour to fire a carbon fiber-reinforced carbon composite material.

[実施例2] (1)実施例1の(3)項で作製した炭素繊維強化炭素
複合材料の電着体を2枚重ね実施例1の(4)項の条件
で一体成形した。
[Example 2] (1) Two sheets of the electrodeposited carbon fiber reinforced carbon composite material produced in item (3) of example 1 were stacked and integrally molded under the conditions of item (4) of example 1.

(2)以下実施例1と同じ条件で熱処理加圧焼成を行っ
た。
(2) Then, heat treatment and pressure firing were performed under the same conditions as in Example 1.

[比較例] (1)前記実施例で用いた自己焼結性炭素粉末、担体樹
脂、炭素繊維織布を使用して、重量比で1対1対1とな
るφ250の被覆物を150枚作成した。
[Comparative Example] (1) Using the self-sintering carbon powder, the carrier resin, and the carbon fiber woven cloth used in the above examples, 150 sheets of φ250 coating having a weight ratio of 1: 1 were prepared. did.

(2)これらを実施例と同じ条件で、加圧・加熱による
成形、熱処理、加圧焼成を行い、炭素繊維強化炭素複合
材料を得た。
(2) Under the same conditions as in the examples, molding by pressure / heating, heat treatment, and pressure firing were performed to obtain a carbon fiber-reinforced carbon composite material.

実施例と比較例で得られた材料の物性値を表1に示す。Table 1 shows the physical property values of the materials obtained in Examples and Comparative Examples.

表1より明らかなように、補修を行ってももとの複合材
料とその特性で若干劣るが実用上差支えない。
As is clear from Table 1, even if repair is performed, the composite material is slightly inferior to the original composite material, but there is no practical problem.

[発明の効果] 本発明により、摩擦・摩耗もしくは消耗した炭素繊維強
化炭素複合材料の再利用した場合、曲げ強度、シャルピ
衝撃値がやや劣るものの、実用上問題はなく、今まで廃
却していた炭素繊維強化炭素複合材料の再使用が可能と
なり、経済的に非常に有効である。
[Advantages of the Invention] According to the present invention, when a carbon fiber reinforced carbon composite material that has been rubbed, worn or exhausted is reused, the bending strength and the Charpy impact value are slightly inferior, but there is no problem in practical use and they have been discarded until now. The carbon fiber reinforced carbon composite material can be reused, which is economically very effective.

フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 D06M 11/00 B Continuation of the front page (51) Int.Cl. 6 Identification number Office reference number FI technical display location D06M 11/00 B

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】摩擦・摩耗、もしくは消耗、あるいは板厚
の薄い炭素繊維強化炭素複合材料の表面に電着法を用い
て炭素質粉末および担体を析出させ、これに電着法によ
り炭素繊維に炭素質粉末および担体を析出させた被覆物
を重ね、加圧、加熱により一体化したのち焼成すること
を特徴とする炭素繊維強化炭素複合材料の補修方法。
1. A carbonaceous powder and a carrier are deposited on the surface of a carbon fiber-reinforced carbon composite material having a thin plate thickness by friction, wear, or consumption, or a thin plate, and carbon fibers are deposited on the carbon fiber powder and the carrier by the electrodeposition method. A method for repairing a carbon fiber reinforced carbon composite material, which comprises stacking a coating material on which a carbonaceous powder and a carrier are deposited, integrating them by pressurizing and heating, and then firing.
【請求項2】摩擦・摩耗、もしくは消耗あるいは板厚の
薄い炭素繊維強化炭素複合材料の表面に電着法を用いて
炭素質粉末および担体を析出させたもの同志を重ね、加
圧・加熱により一体化したのち焼成することを特徴とす
る炭素繊維強化炭素複合材料の補修方法。
2. A carbon fiber reinforced carbon composite material having a thin plate thickness, which is frictional, worn, or worn, or has a thin plate on which carbonaceous powder and a carrier are deposited by an electrodeposition method. A method for repairing a carbon fiber-reinforced carbon composite material, which comprises firing after being integrated.
JP62136488A 1987-05-29 1987-05-29 Repair method of carbon fiber reinforced carbon composite material Expired - Lifetime JPH0761688B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62136488A JPH0761688B2 (en) 1987-05-29 1987-05-29 Repair method of carbon fiber reinforced carbon composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62136488A JPH0761688B2 (en) 1987-05-29 1987-05-29 Repair method of carbon fiber reinforced carbon composite material

Publications (2)

Publication Number Publication Date
JPS63297031A JPS63297031A (en) 1988-12-05
JPH0761688B2 true JPH0761688B2 (en) 1995-07-05

Family

ID=15176317

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62136488A Expired - Lifetime JPH0761688B2 (en) 1987-05-29 1987-05-29 Repair method of carbon fiber reinforced carbon composite material

Country Status (1)

Country Link
JP (1) JPH0761688B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20150142187A (en) * 2014-06-11 2015-12-22 이범희 Apparatus for repairing carbon composite meterial frame and method for repairing the same

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2689919B1 (en) 2012-07-24 2020-04-08 Airbus Operations GmbH Process for selective isolation of CFRP parts by electrodeposition coatings
CN103409985B (en) * 2013-08-07 2015-04-22 常州大学 Preparation method of carbon nano tube loaded carbon fiber
CN107839260B (en) * 2017-10-25 2019-07-16 南京航空航天大学 The injury repair technique and its device of the super hybrid composite manner laminate of fibre reinforced thermoplasticity
CN113085229B (en) * 2021-04-22 2022-02-15 同济大学 Device and method for repairing layered damage of carbon fiber reinforced thermosetting resin-based composite material

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20150142187A (en) * 2014-06-11 2015-12-22 이범희 Apparatus for repairing carbon composite meterial frame and method for repairing the same

Also Published As

Publication number Publication date
JPS63297031A (en) 1988-12-05

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