항공기 복합재 구조물 전용 토크 치구 개발에 관한 연구

• 영문명: A Study on the Development of Safety Torque Tool for Aircraft Composite Structure
• 발행기관: 한국산업기술융합학회(구. 산업기술교육훈련학회)
• 저자명: 김형래(Hyoung-Rae Kim)
• 간행물 정보: 『산업기술연구논문지』산업기술교육훈련논문지 제22권 3호, 61~66쪽, 전체 6쪽
• 주제분류: 공학 > 공학일반
• 파일형태: PDF
• 발행일자: 2017.09.30

영문 초록

In this paper, we performed the design of safety torque tool for high torque value required on the composite material structure. We surveyed the characteristic of composite materials and application case in aerospace industries. Also, we reviewed the assembly sequence of the composite skin assembly for tool design. The safety torque tool is designed in accordance with the drawing & process specification requirement of the Boeing company. The torque tools are designed by solid modelling of CATIA. As a result, the safety torque tools are composed base plate assembly, strap clamp assembly and handle assembly. Engineering requirement and tools designed for the hi-torque application process are introduced in this paper.

목차

Ⅰ. 서 론

Ⅱ. 항공기 복합재 조립체 생산 공정 분석

III. Safety Torque Tool 개발

Ⅳ. 결 론

키워드

Composite(복합재) CFRP(Carbon Fiber-Reinforced Plastic,탄소섬유강화 복합재료) Torque Wrench(토크 렌치) Tool(치공구) Concept Design(개념설계) Detail Design(상세설계)