항공기 복합재 솔리드 적층판의 본드 플러시 패치 수리 방법에 관한 연구

• 영문명: A Study on the Bonded Flush Patch Repair Method for Aircraft Composite Solid Laminates
• 발행기관: 한국산업기술융합학회(구. 산업기술교육훈련학회)
• 저자명: 김형래(Hyoung-Rae Kim) 이병우(Byung-Woo Lee)
• 간행물 정보: 『산업기술연구논문지』산업기술연구논문지 제26권 3호, 37~43쪽, 전체 7쪽
• 주제분류: 공학 > 공학일반
• 파일형태: PDF
• 발행일자: 2021.09.30

영문 초록

An evaluation was performed by applying repair technology of composite solid laminates to airframe composite structures. Damage and defects in the composite laminate structure of an aircraft are caused by events occurring during vehicle movement, such as lightning, tide collisions, and runway collisions during takeoff and landing along with damage caused during aircraft movement and maintenance, fuel injection, and cargo loading. After the damaged part was removed, the damaged composite solid laminated structure was repaired using the bonded flush patch repair method. In the bonded flush patch repair method, the molded patch is joined to the base material using an adhesive. To determine the damage caused by external impact, the test results of the repaired specimen and those of the specimen before damage were compared.

목차

Ⅰ. 서 론

Ⅱ. 실 험

Ⅲ. 실험결과 및 고찰

Ⅳ. 결 론

참고문헌

키워드

복합재 적층판 구조 수리 손상 가압장비 본드 플러시 패치 Composite Laminate Structure Repair Damage Autoclave Bonded Flush Patch