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A Study on the Elevator Spar Improvement for the Operating Aircraft

장기 운영항공기 승강타 날개보 구조개선 연구

  • Shim, Daisung (Sacheon Center, Defense Agency for Technology and Quality) ;
  • Kim, Mantae (Sacheon Center, Defense Agency for Technology and Quality) ;
  • Yeom, Hyowon (Sacheon Center, Defense Agency for Technology and Quality) ;
  • Im, Dongmin (Sacheon Center, Defense Agency for Technology and Quality) ;
  • Kim, Youngjin (Sacheon Center, Defense Agency for Technology and Quality) ;
  • Uhm, Wonseop (Airframe Analysis Team, Korea Aerospace Industries, Ltd.)
  • 심대성 (국방기술품질원 사천센터) ;
  • 김만태 (국방기술품질원 사천센터) ;
  • 염효원 (국방기술품질원 사천센터) ;
  • 임동민 (국방기술품질원 사천센터) ;
  • 김영진 (국방기술품질원 사천센터) ;
  • 엄원섭 (한국항공우주산업(주) 고정익해석팀)
  • Received : 2016.05.04
  • Accepted : 2016.11.04
  • Published : 2016.12.05

Abstract

This is a study for the improvement of the defected elevator spar in operating aircraft. The elevator spar web holes were analyzed to find out the cause of the cracks. The fatigue striations were observed and the cracks occurred by the repetitive stresses during the elevator works. Also the outboard connection structure of the elevator and horizontal stabilizer was more weak shape than the inboard. The design changes were recommended and the analyses were performed to verify the improvement of the changed shapes.

Keywords

References

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