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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0157279 (1988-02-17) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 30 인용 특허 : 8 |
A bolted repair for curved surfaces of an aircraft structure includes a plurality of relatively thin, flexible plates that are bent to conform to the surface, either individually or as a group. After the plates have been bent to conform to the surface, layers of adhesive are applied between adjacent
A method of repairing a damaged airframe structure, comprising: preparing a plurality of relatively thin plates having a shape configured to at least overlap the damaged area of said structure; bending said plates against said structure, either individually or in groups, so that said plates progress
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