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
某型飞机主起落架收放系统性能分析与试验验证
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1.航空工业第一飞机设计研究院 结构设计研究所;2.南京航空航天大学 机械结构力学及控制国家重点实验室

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V226

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Performance analysis and experimental verification of the main landing gear retraction system of a certain type of aircraft
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Structure Design and Research Institute,AVIC The First Aircraft Design Institute,Xi’an

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    摘要:

    起落架收放系统是一个集合了机械、电气、液压的混合复杂系统,随着仿真技术的发展,通过计算机仿真的方式进行收放系统性能研究既直观快捷,又可以降低成本。但是,目前利用单个软件对起落架收放系统这类复杂系统进行仿真较难实现,针对该问题,提出一种结合理论分析、多学科仿真技术分析的方法,首先依据起落架模型收放原理,建立收放系统机械动力学模型;然后依据液压原理建立液压系统仿真模型,在此基础上构建二者结合的多学科协同仿真模型;最后将多种工况设置下进行的联合仿真结果与试验结果比对,验证了联合仿真技术在起落架收放系统分析中应用的准确性和便利性。

    Abstract:

    Landing gear retracting system is a complex system integrating mechanical, electrical and hydraulic. With the development of simulation technology, it is convenient and fast to study the performance of retracting and retracting system by computer simulation. Aiming at the present situation that the single software simulation method is difficult to realize this kind of complex system, a method combining theoretical analysis and multidisciplinary simulation technology analysis is proposed, which provides a more accurate analysis means for the landing gear retracting system. In this paper, the mechanical dynamics model of the retraction system is established according to the retraction principle of the landing gear model, and then the simulation model of the hydraulic system is established according to the hydraulic principle. On this basis, a multidisciplinary co-simulation model combining the two is completed. Finally, the results of co-simulation under various operating conditions are compared with the experimental results, and the accuracy and convenience of co-simulation technology in the analysis of landing gear retracting system are verified.

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历史
  • 收稿日期:2024-01-25
  • 最后修改日期:2024-04-18
  • 录用日期:2024-05-29
  • 在线发布日期: 2025-03-06
  • 出版日期: