JP2541620B2 - How to repair composite structures - Google Patents

How to repair composite structures

Info

Publication number
JP2541620B2
JP2541620B2 JP63088650A JP8865088A JP2541620B2 JP 2541620 B2 JP2541620 B2 JP 2541620B2 JP 63088650 A JP63088650 A JP 63088650A JP 8865088 A JP8865088 A JP 8865088A JP 2541620 B2 JP2541620 B2 JP 2541620B2
Authority
JP
Japan
Prior art keywords
composite material
damaged portion
cutting tool
tool
material structure
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 - Fee Related
Application number
JP63088650A
Other languages
Japanese (ja)
Other versions
JPH01259931A (en
Inventor
克美 亀井
隆之 神山
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

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モンド砥粒で削りとっつ
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。
Description: TECHNICAL FIELD The present invention relates to a method for repairing a composite material structure, and in particular, repairs a damaged portion existing on the surface of the composite material by shaving the damaged portion with a diamond abrasive grain. The present invention relates to a method for repairing a composite material structure that is filled with a material.

〔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56−63620および特
開昭60−89338号公報参照)。
Generally, if there are cracks or damaged parts on the surface or inside of the structure of the fiber reinforced plastic (FRP), the material strength decreases, so that part needs to be repaired. For this purpose, a hand grinder was conventionally attached to a hand grinder, the damaged portion was ground into a trapezoidal shape, and the portion was filled with a material of the same quality as the structure for repair (JP-A-56-63620 and JP-A-SHO-63620) 60-89338).

〔発明が解決しようとする問題点〕[Problems to be solved by the invention]

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、消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 technique, since the material to be cut is a composite material of plastic, the grindstone easily causes clogging, and the erased surface becomes uneven and peels off, which results in good adhesiveness. There was a problem that a cavity was created without it.

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、しかも削りとっ
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。
Therefore, the present invention provides a method for repairing a composite material structure that solves the problems of the above-mentioned conventional techniques and that does not cause clogging of the grindstone and does not cause peeling on the ground surface. is there.

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

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, a 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 formed by diamond abrasive grains are radially provided on a conical surface of a tool body. It is characterized in that it is pressed against the damaged portion of the material to scrape off the damaged portion, and then the repair material of the same quality as the composite material structure is filled.

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 formed by diamond abrasive grains are radially arranged 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。
A method for repairing a composite material structure according to the present invention will be described below 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の表面近くに損傷部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、回転力に与えられる。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. 1 (a) shows the surface of the composite material structure 1. This indicates that the damaged portion 2 is present in the vicinity. A cutting tool 3 according to the present invention is used to remove this damaged portion 2. As shown in FIGS. 2 and 3, this cutting tool 3 has a conical tool body 4, and the conical surface 5 of this body 4 has a helical shape formed by sintering diamond abrasive grains. Cutting edge 6
Are radially arranged. A chip pocket 7 is formed between these adjacent cutting edge portions 6. In such a cutting tool 3, the drive shaft 8 is connected to a rotary drive tool such as an air tool and is given a rotational force. First
As shown in FIG. 2B, the cutting tool 3 is located immediately above the damaged portion 2, and the damaged portion 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 a filling material 10 of the same quality as the composite material structure is filled in this hole, and the repair is completed.

〔発明の効果〕〔The invention's effect〕

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, since chips are discharged from the chip pocket 7 of the cutting edge portion of the diamond abrasive grains, the grindstone does not cause clogging, and the damaged portion does not generate heat or peel off. Can be removed and then repaired by filling with homogeneous material.

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

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、
1 (a), (b), (c), and (d) are diagrams showing steps of the repair method according to the present invention, FIG. 2 is a front view showing a cutting tool, and FIG. 3 is a side view of the cutting tool. Is. 1 ... Composite structure, 2 ... Damaged part, 3 ... Cutting tool,
6 ... Cutting edge part, 7 ... Tip pocket,

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項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。
1. A cutting tool in which a plurality of helical cutting edges formed by diamond abrasive grains are radially provided on a conical surface of a tool body is pressed against a damaged portion of a composite material to scrape the damaged portion, and thereafter. A repair method for a composite material structure, characterized in that a repair agent of the same quality as that of the composite material structure is filled in.
【請求項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。
2. A cutting tool in which a plurality of helical cutting edges formed by diamond abrasive grains are radially arranged on a conical surface of a 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 JPH01259931A (en) 1989-10-17
JP2541620B2 true 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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011105540A1 (en) 2010-02-26 2011-09-01 三菱重工業株式会社 Composite material repair method, and composite material using same

Families Citing this family (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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011105540A1 (en) 2010-02-26 2011-09-01 三菱重工業株式会社 Composite material repair method, and composite material using same
US9993983B2 (en) 2010-02-26 2018-06-12 Mitsubishi Heavy Industries, Ltd. Repairing method for composite material and composite material using the same

Also Published As

Publication number Publication date
JPH01259931A (en) 1989-10-17

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