Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Research on Dynamics of Helicopter Leg Landing Gear Mechanism
Author:
Affiliation:

1.National Key Laboratory Strength and Structural Integrity,Aircraft Strength Research Insitute of China,Xi’an 710065;2.China

Clc Number:

V226;TP23

Fund Project:

Aeronautical Science Foundation of China

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    Multipurpose, intelligent, and strong terrain adaptability are important trends in the development of helicopters in the future. The landing gear is a key component to ensure the safety of helicopter takeoff and landing. Due to the poor terrain adapt-ability of the traditional landing gear, a leg landing gear system is designed using the bionics design concept to solve the problem of the helicopter"s smooth land observation in complex terrain environment. Starting from the design require-ments of leg landing gear, the landing architecture was analyzed and the leg structure design was completed. Then, based on the designed leg mechanism, the kinematics analysis and dynamics analysis are completed, and the relevant models are established as the basis for the motion control of the leg landing gear. Finally, motion testing of the leg landing gear was completed in the laboratory, proving the rationality of the structural design and the accuracy of the control algorithm.

    Reference
    Related
    Cited by
Get Citation

LIU Haolin, LIU Xiaochuan, REN Jia, WANG Jizhen. Research on Dynamics of Helicopter Leg Landing Gear Mechanism[J]. Advances in Aeronautical Science and Engineering,2024,15(3):157-166

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:November 08,2023
  • Revised:May 14,2024
  • Adopted:May 17,2024
  • Online: May 21,2024
  • Published: