JPH01259931A - Repairing method for composite material structure - Google Patents

Repairing method for composite material structure

Info

Publication number
JPH01259931A
JPH01259931A JP8865088A JP8865088A JPH01259931A JP H01259931 A JPH01259931 A JP H01259931A JP 8865088 A JP8865088 A JP 8865088A JP 8865088 A JP8865088 A JP 8865088A JP H01259931 A JPH01259931 A JP H01259931A
Authority
JP
Japan
Prior art keywords
composite material
damaged section
material structure
tool
cutting tool
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
JP8865088A
Other languages
Japanese (ja)
Other versions
JP2541620B2 (en
Inventor
Katsumi Kamei
亀井 克美
Takayuki Kamiyama
神山 隆之
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.)
Subaru Corp
Original Assignee
Fuji Heavy 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 Fuji Heavy Industries Ltd filed Critical Fuji Heavy Industries Ltd
Priority to JP63088650A priority Critical patent/JP2541620B2/en
Publication of JPH01259931A publication Critical patent/JPH01259931A/en
Application granted granted Critical
Publication of JP2541620B2 publication Critical patent/JP2541620B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To prevent a whetstone from getting clogged and also a shaved surface from peeling off by shaving damaged section of a composite material by means of a cutting tool provided radiately a plurality of helical cutting blades of diamond abrasive grains on a conical surface of a tool body and filling a patching agent of similar quality of said damaged section. CONSTITUTION:A cutting tool 3 is provided with a conical tool main body 4, and a plurality of helical cutting blade sections 6 constituted of sintered diamond abrasive grains are disposed radiately on said conical surface, while chip pockets 7 are formed between respective adjacent cutting blade sections 6. A cutting tool 3 is positioned right above the damaged section 2, and the damaged section 2 of a composite material structure 1 is shaved off to form a patching hole 9. A filler 10 of same quality as the composite material structure 1 is filled to complete patching. As swarfs are discharged out of the chip pocket 7, a whetstone never gets clogged, and the damaged section can be scooped out and patched without the generation of heat or peeling.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は複合材構造物の修理方法に係り、特に複合材の
表面に存在する損傷部をダイヤモンド砥粒で削りとつっ
てその部分に補修剤を充填するようにした複合材構造物
の補修方法に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a method of repairing a composite material structure, and in particular, a method of repairing a damaged part existing on the surface of a composite material by scraping away the damaged part with diamond abrasive grains. The present invention relates to a method for repairing a composite structure by filling it with a compound.

〔従来の技術〕[Conventional technology]

一般に繊維強化プラスチック(FRP)の構造物の表面
もしくは内部に亀裂や損傷部が存在すると材料強度が低
下することから、その部分を補修する必要がある。その
ために、従来はハンドグラインダに豆砥石を取付け、損
傷部を台形状に削りとり、その部分に構造物と同質の材
料を充填して補修していた(特開昭55−63620お
よび特開昭60−89338号公報参照)。
Generally, when cracks or damaged parts exist on the surface or inside of a fiber-reinforced plastic (FRP) structure, the strength of the material decreases, so it is necessary to repair the parts. For this purpose, in the past, a grindstone was attached to a hand grinder, the damaged part was cut into a trapezoidal shape, and the damaged part was filled with a material of the same quality as the structure to repair it (Japanese Patent Application Laid-Open No. 55-63620 and 60-89338).

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

しかしながら、上述した従来技術によると、被切削材料
がプラスチックの複合材料であるために砥石が目ずまり
をおこしやすく、削りとった面が凹凸となって剥離を生
じ、そのために接着性が良くなく空洞が生じるという問
題があった。
However, according to the above-mentioned conventional technology, since the material to be cut is a plastic composite material, the grinding wheel tends to clog, and the cut surface becomes uneven and peels, resulting in poor adhesion. There was a problem that cavities were formed.

そこで、本発明は上記従来技術が有する問題点を解消し
、砥石が目つまりを起こすことなく、シかも削りとった
面に剥離を起こさないようにした複合材構造物の修理方
法を提供することにある。
SUMMARY OF THE INVENTION Therefore, the present invention solves the problems of the above-mentioned prior art and provides a method for repairing a composite material structure that does not cause clogging of the grindstone and does not cause peeling on the ground surface. It is in.

〔課題を解決するための手段〕   。[Means for solving problems].

上記課題を解決するために、本発明による複合材構造物
の修理方法は、工具本体の円すい面上にダイヤモンド砥
粒によるヘリカル状の切れ刃部の複数個が放射状に設け
られた切削工具を複合材の損傷部に押しあてて損傷部を
削りとり、その後に複合材構造物と同質の補修剤を充填
したことを特徴とするものである。
In order to solve the above problems, the method for repairing a composite material structure according to the present invention is a composite cutting tool in which a plurality of helical cutting edges made of diamond abrasive grains are radially provided on the conical surface of the tool body. It is characterized in that it is pressed against the damaged part of the material to scrape off the damaged part, and then filled with a repair agent of the same quality as the composite material structure.

また、本発明による切削工具は、工具本体の円すい面上
にダイヤモンド砥粒によるヘリカル状の切れ刃部の複数
個を放射状に配置したことを特徴とするものである。
Further, the cutting tool according to the present invention is characterized in that a plurality of helical cutting edges made of diamond abrasive grains are arranged radially on the conical surface of the tool body.

〔実施例〕〔Example〕

以下本発明による複合材構造物の修理方法を図面を参照
して説明する。
Hereinafter, a method for repairing a composite material structure according to the present invention will be explained with reference to the drawings.

第1図(a)(b)(c)(d)は、本発明による複合
材構造物の修理方法の各工程を示しており、第1図(a
)は、複合材構造物1の表面近くにfM(M部2が存在
していることを示している。この損傷部2を除去するた
めに、本発明による切削工具3が使用される。この切削
工具3は、第2図および第3図に示したように、円すい
状の工具本体4を有し、この本体4の円すい面5にはダ
イヤモンド砥粒を焼結してなるヘリカル状の切れ刃部6
の複数個が放射状に配置されている。これらの隣接する
切れ刃部6の間にはチップポケット7が形成されている
。このような切削工具3は駆動軸8がエアーツール等の
回転駆動工具に接続され、回転力を与えられる。第1図
(b)に示したように、上記切削工具3が損傷部2の直
ぐ上に位置され、切削工具3を使って損傷部2が削りと
られる。
1(a), (b), (c), and (d) show each step of the method for repairing a composite material structure according to the present invention, and FIG.
) indicates the presence of fM (M section 2) near the surface of the composite structure 1. In order to remove this damaged section 2, the cutting tool 3 according to the invention is used. As shown in FIGS. 2 and 3, the cutting tool 3 has a conical tool body 4, and a helical cut formed by sintering diamond abrasive grains is formed on the conical surface 5 of the body 4. Blade part 6
A plurality of these are arranged radially. A chip pocket 7 is formed between these adjacent cutting edges 6. The cutting tool 3 has a drive shaft 8 connected to a rotary drive tool such as an air tool, and is given rotational force. As shown in FIG. 1(b), the cutting tool 3 is positioned directly above the damaged part 2, and the damaged part 2 is scraped off using the cutting tool 3.

次いで、第1図(c)に示したように、補修穴9が形成
され、この穴内に複合材構造物と同質の充填材10が充
填され、補修が完了する。
Next, as shown in FIG. 1(c), a repair hole 9 is formed, and the hole is filled with a filler 10 of the same quality as the composite material structure, thereby completing the repair.

〔発明の効果〕〔Effect of the invention〕

以上の説明から明らかなように、本発明によれば、ダイ
ヤモンド砥粒の切れ刃部のチップポケット7から切屑が
排出されるために、砥石が目づまりを起こすことなく、
かつ発熱や剥離なく損傷部をえぐりとることができ、そ
の後に同質の材料を充填して補修することができる。
As is clear from the above description, according to the present invention, chips are discharged from the chip pocket 7 of the cutting edge of the diamond abrasive grain, so that the grinding wheel does not become clogged.
Moreover, the damaged part can be scooped out without heat generation or peeling, and then repaired by filling with the same material.

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

第1図(a)(b)(c)(d)は本発明による補修方
法の工程を示した図、第2図は切削工具を示した正面図
、第3図は同切削工具の側面図である。 1・・・複合材構造物、2・・・損傷部、3・・・切削
工具、6・・・切れ刃部、7・・・チップポケット、出
願人代理人  佐  藤  −雄 (a)               (b)(c) 
              (d)第1 図
Figures 1 (a), (b), (c) and (d) are diagrams showing the steps of the repair method according to the present invention, Figure 2 is a front view of the cutting tool, and Figure 3 is a side view of the same cutting tool. It is. DESCRIPTION OF SYMBOLS 1... Composite material structure, 2... Damaged part, 3... Cutting tool, 6... Cutting edge part, 7... Chip pocket, Applicant's representative Sato-Yu (a) ( b)(c)
(d) Figure 1

Claims (1)

【特許請求の範囲】 1、工具本体の円すい面上にダイヤモンド砥粒によるヘ
リカル状の切れ刃部の複数個が放射状に設けられた切削
工具を複合材の損傷部に押しあてて損傷部を削りとり、
その後に複合材構造物と同質の補修剤を充填したことを
特徴とする複合材構造物の修理方法。 2、工具本体の円すい面上にダイヤモンド砥粒によるヘ
リカル状の切れ刃部の複数個を放射状に配置してなる切
削工具。
[Claims] 1. A cutting tool having a plurality of helical cutting edges made of diamond abrasive radially provided on the conical surface of the tool body is pressed against the damaged part of the composite material to scrape the damaged part. bird,
A method for repairing a composite material structure, characterized in that a repair agent of the same quality as the composite material structure is then filled. 2. A cutting tool in which a plurality of helical cutting edges made of diamond abrasive grains are arranged radially on the conical surface of the tool body.
JP63088650A 1988-04-11 1988-04-11 How to repair composite structures Expired - Fee Related JP2541620B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63088650A JP2541620B2 (en) 1988-04-11 1988-04-11 How to repair composite structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63088650A JP2541620B2 (en) 1988-04-11 1988-04-11 How to repair composite structures

Publications (2)

Publication Number Publication Date
JPH01259931A true JPH01259931A (en) 1989-10-17
JP2541620B2 JP2541620B2 (en) 1996-10-09

Family

ID=13948693

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63088650A Expired - Fee Related JP2541620B2 (en) 1988-04-11 1988-04-11 How to repair composite structures

Country Status (1)

Country Link
JP (1) JP2541620B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5142828A (en) * 1990-06-25 1992-09-01 Microelectronics And Computer Technology Corporation Correcting a defective metallization layer on an electronic component by polishing
JP2015068096A (en) * 2013-09-30 2015-04-13 Jfeエンジニアリング株式会社 Repairing method of deteriorated layer of fiber-reinforced plastic molded article surface and repaired fiber-reinforced plastic molded article

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2540485B1 (en) 2010-02-26 2020-05-06 Mitsubishi Heavy Industries, Ltd. Composite material repair method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5142828A (en) * 1990-06-25 1992-09-01 Microelectronics And Computer Technology Corporation Correcting a defective metallization layer on an electronic component by polishing
JP2015068096A (en) * 2013-09-30 2015-04-13 Jfeエンジニアリング株式会社 Repairing method of deteriorated layer of fiber-reinforced plastic molded article surface and repaired fiber-reinforced plastic molded article

Also Published As

Publication number Publication date
JP2541620B2 (en) 1996-10-09

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