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Study on Vibration Characteristic Improvement of Aircraft Landing Gear Handle

항공기용 착륙장치 핸들의 진동 특성 개선에 관한 연구

  • Received : 2018.01.16
  • Accepted : 2018.04.18
  • Published : 2018.04.30

Abstract

The landing gear (L/G) handle of an aircraft is an essential piece of equipment for aircraft take-off and landing. The bracket in the landing gear handle was fractured during a vibration test when developing the landing gear handle. This paper summarizes the vibration test procedures performed during landing gear handle development. A cause analysis, design improvements, and verification results of the fault in the vibration test are also provided.

항공기 구성품인 착륙장치 핸들은 항공기 이 착륙 시 착륙장치 작동을 위한 핵심적인 장비이다. 착륙장치 핸들의 개발을 위한 진동시험 중 착륙장치 핸들 내부의 브라켓 파손 현상이 발생하였다. 따라서 본 논문에서는 착륙장치 핸들 개발 시 수행한 진동시험 절차와 진동시험 중 발생한 결함사항에 대한 원인 분석, 설계 개선사항 그리고 검증 결과를 함께 기술하였다.

Keywords

References

  1. USAF, "MIL-STD-810 Environmental Test Methods for Aerospace and Ground Equipment", Department of the Air Force, Jun 1962
  2. RTCA, "DO-160 Environmental Conditions and Test Procedures for Airborne Equipment", Radio Technical Commission for Aeronautics, Feb 1975
  3. H. J. Yoo. and K. H. Byun. and K. Y. Park., "The Ground Vibration Test on an Aircraft and FE Model Update," Journal of KSNVE, vol. 8, no. 4, pp. 690-699, Aug 1998
  4. K. H. Byun. and C. Y. Park. and J. H. Kim., "Ground Vibration Test of KF-16D," Journal of The Korean Society for Aeronautical and Space Sciences, vol. 33, no. 5, pp. 41-49. May 2005 https://doi.org/10.5139/JKSAS.2005.33.5.041
  5. D. H. Cho. and C. Y. Park. and J. H. Kim., "Evaluation of Vibration Test Severity by FDS and ERS,," Proceedings of ISMA, pp. 1725-1735. 2010