Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Impact Dynamic Analysis for the Wheel-Type Landing Gear System of Helicopter

헬리콥터 휠타입 착륙장치 충돌특성 연구

  • 박효근 (국립경상대학교 기계항공공학부) ;
  • 김동만 (국립경상대학교 기계항공공학부) ;
  • 김동현 (국립경상대학교 기계항공공학부 및 항공기부품기술 연구소) ;
  • 조윤모 (한국항공우주산업 KHP사업부 KHP계통종합팀) ;
  • 정재훈 (한국항공우주산업 KHP사업부 KHP계통종합팀)
  • Published : 2008.10.31
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Abstract

In this study, the dynamic characteristics for the wheel-type landing gear system of helicopter have been analyzed. Nonlinear multi-body dynamic models of the landing gear system are constructed and the equations of motion, kinematics and internal forces of shock strut are considered. In addition, flexibility effect of the wheel axle with equivalent beam element is taken into account. General purpose commercial finite code, SAMCEF which includes MECANO module is applied. The results of dynamic simulation for various landing and weight conditions are presented and compared with each other. Based on the results, characteristics of impact dynamic behaviors of the landing gear system are practically investigated.

Keywords

References

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