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
Study on stiffness and shimmy stability of strut-type nose landing gear system
Author:
Affiliation:

1.Central South University;2.AVIC Landing-gear Advanced Manufacturing Corp

Clc Number:

V226+.1

Fund Project:

The civil aircraft special project of the MIIT (Grant No. JZ025-XY-003) ; The Postgraduate Scientific Research Innovation Project of Hunan Province (Grant No. CX20210221)

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

    System stiffness (longitudinal, lateral, and torsional stiffness) is a meaningful index for strut nose landing gear design. It arises from profound significance to explore the influence law of system stiffness on shimmy stability for the anti-shimmy design of landing gear. By changing the initial gas pressure of the buffer, the influence of buffer stroke on the system stiffness is analyzed, and the influence of the system stiffness on the initial torsion angle, convergence time, convergence ratio, and stability area of the strut nose landing gear shimmy is studied. Results show that increasing the stiffness of the strut-type nose gear system can improve the anti-shimmy performance, but increase the initial torsional angle and shimmy convergence time, and reduce the ability of the landing gear to resist external disturbances. Therefore, the stiffness of the strut-type nose landing gear system cannot be excessively increased, which provides a guiding significance for its anti-shimmy design.

    Reference
    Related
    Cited by
Get Citation

fengguan, xiangzongwei, jiangyiyao, jinjun, yuhaowen, jiangbingyan. Study on stiffness and shimmy stability of strut-type nose landing gear system[J]. Advances in Aeronautical Science and Engineering,2023,14(1):65-72

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:March 14,2022
  • Revised:June 10,2022
  • Adopted:June 21,2022
  • Online: December 15,2022
  • Published: