主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
支柱式前起落架系统刚度与摆振稳定性研究
作者:
作者单位:

1.中南大学;2.中航飞机起落架有限责任公司;3.中南大学机电工程学院高性能复杂制造国家重点实验室

作者简介:

通讯作者:

中图分类号:

V226+.1

基金项目:

工信部民机专项(JZ025-XY-003) ;湖南省研究生科研创新项目资助(CX20210221)


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

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)

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    系统刚度(航向、侧向和扭转刚度)是支柱式前起落架设计的重要指标,探明系统刚度对摆振稳定性的影响规律,对起落架的防摆设计具有重要意义。采用改变缓冲器初始气体压力的方式,分析缓冲器行程对系统刚度的影响规律,研究系统刚度对支柱式前起落架摆振的初始扭转角、收敛时间、收敛比例和稳定区域的影响。结果表明:增大支柱式前起落架系统刚度,可提升防摆性能,但同时会造成初始扭转角和摆振收敛时间的增加,这会降低起落架抵御外界干扰的能力,因此,不能过度增加支柱式前起落架系统刚度。

    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.

    参考文献
    相似文献
    引证文献
引用本文

冯广,向宗威,姜义尧,金军,余好文,蒋炳炎.支柱式前起落架系统刚度与摆振稳定性研究[J].航空工程进展,2023,14(1):65-72

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2022-03-14
  • 最后修改日期:2022-06-10
  • 录用日期:2022-06-21
  • 在线发布日期: 2022-12-15
  • 出版日期: