항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제14권3호
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  • Pages.60-68
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  • 2020
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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블레이드 파편 봉쇄를 위한 컨테인먼트 케이스 연구 동향

Research Survey of the Containment Case for Damage Protection from Blade Fragments

  • 채승호 (한국항공대학교 항공우주 및 기계공학부) ;
  • 안상현 (한국항공대학교 항공우주 및 기계공학부) ;
  • 이수용 (한국항공대학교 항공우주 및 기계공학부) ;
  • 노진호 (한국항공대학교 항공우주 및 기계공학부)
  • Chae, Seungho (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Ahn, Sanghyeon (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Lee, Soo-Yong (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Roh, Jin-Ho (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
  • 투고 : 2019.12.10
  • 심사 : 2020.05.17
  • 발행 : 2020.06.30
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초록

항공기 엔진 내의 파손된 블레이드가 케이스를 관통하여 외부로 나가게 되면, 동체에 부딪혀 승객의 안전을 위협하게 된다. 따라서 엔진 케이스 설계 시 항공청의 안전성 평가 인증을 받아야한다. 본 논문에서는 국내의 독자적인 엔진 개발을 위해 필요한 엔진 케이스의 컨테인먼트 인증 요구조건과 개발 기술에 대하여 조사하였다. 미국과 유럽의 항공청에서 제시하는 컨테인먼트 안전성 요구 조건을 정리하고 이 인증에 부합하는 케이스의 파편 봉쇄를 검증하는 실험적/해석적 방법에 대하여 확인하였다. 컨테인먼트 케이스에 대한 최근의 연구를 분석하여 케이스 개발 시 검증 방법을 제시하고자 한다.

If a broken blade in the aircraft engine penetrates the casing and ejects outside the aircraft, it will impact the fuselage, threatening the safety of the passengers. Thus, the development of a engine case should be certified for stability evaluation by the Aviation Administration. In this paper, we investigated the requirements and development technology for the containment certification of the engine casing necessary for the independent engine development in the country. An experimental/analytical method has been identified to summarize the contact safety requirements presented by the U.S. and European aviation agencies to verify the containment of debris in the casing corresponding to this certification. Also, we analyzed recent research on the containment casing and verification methods in casing development.

키워드

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