A Study on the Compliance Evaluation for Design of an Aircraft Generator

항공기용 발전기의 설계 적합성 평가에 관한 연구

  • 김유광 (한국항공우주연구원 품질인증센터) ;
  • 박근영 (한국항공우주연구원 품질인증센터) ;
  • 이강이 (한국항공우주연구원 품질인증센터) ;
  • 진영권 (한국항공우주연구원 품질인증센터)
  • Published : 2003.12.13

Abstract

In this paper, the design data of an aircraft generator have been reviewed to evaluate the compliance with the airworthiness standards, and the technical procedure to ensure safety and reliability of an alternate-current generator by the tests and computations have been developed.

Keywords