A Study on Reliability Assessment of Aircraft Structural Parts

항공기 동적 부분품에 대한 신뢰성 평가

  • 김은정 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 원준호 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 최주호 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김태곤 (대한항공 항공우주 사업본부)
  • Received : 2010.12.15
  • Accepted : 2010.12.21
  • Published : 2010.12.31

Abstract

A continuing challenge in the aviation industry is how to safely keep aircraft in service longer with limited maintenance budgets. Therefore, all the advanced countries in aircraft technologies put great efforts in prediction of failure rate in parts and system, but in the domestic aircraft industry is lack of theoretical and experimental research. Prediction of failure rate provides a rational basis for design decisions such as the choice of part quality levels and derating factors to be applied. For these reasons, analytic prediction of failure rate is essential process in developing aircraft structure. In this paper, a procedure for prediction of failure rate for aircraft structural parts is presented. Cargo door kinematic parts are taken to illustrate the process, in which the failure rate for Hook part is computed by using Monte Carlo Simulation along with Response Surface Model, and system failure rate is obtained afterwards.

Keywords

References

  1. SAE ARP 4761, Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne System and Equipment, 1996.
  2. Naval Surface Warfare Center, NSWC-98/LE1, Handbook of reliability prediction procedures for mechanical equipment, Washington, USA, 1998.
  3. Reliability Information Analysis Center, NPRD-95, Nonelectronic parts reliability data , Utica, USA, 1995.
  4. Serhan Ozsoy, Mehmet Celik, F. Suat Kadıoğlu, "An Accelerated Life Test Approach for Aerospace Structural Components", Engineering Failure Analysis Journal, Vol. 15, Oct. 2008, pp.946-957. https://doi.org/10.1016/j.engfailanal.2007.10.015
  5. SD Durham, WJ Padgett, "Estimation for a Probabilitic Stress-Strength Model", IEEE Transaction Reliability, Vol. 39(2), June 1990, pp.199-203. https://doi.org/10.1109/24.55882
  6. MIL-Handbook 17, Department of Defence, Washington, USA, 1996.
  7. C. G. Bucher, U. Bourgund, "A fast and efficient response surface approach for structural reliability problems", Structural Safety, Vol. 7(1), 1990, pp. 57-66. https://doi.org/10.1016/0167-4730(90)90012-E
  8. Yu Chee Tong, Literature Review on Aircraft Structural Risk and Reliability Analysis, Defence Science & Technology Organization Aeronautical and Maritime Research and Laboratory Technical Report, 2001.