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飞行器折叠舵展开及锁紧过程动力学仿真研究

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飞行器折叠舵的展开及锁紧过程是多载荷综合作用的动态过程.对该动态过程进行仿真研究,建立了考虑气动载荷和摩擦作用的动力学仿真模型,通过对不同气动载荷工况下的模型进行动力学仿真,分析了气动载荷作用对展开及锁紧过程的影响;并通过空载展开试验,验证了动力学仿真模型的准确性.基于该模型,从载荷和能量维度分别应用角加速度法和角速度法,对不同气动载荷工况下摩擦做功进行了辨识.研究结果表明,摩擦力矩受气动载荷影响;摩擦做功随气动促进作用的增大而增大;角加速度法和角速度法辨识摩擦做功均合理.此次研究为飞行器折叠舵的设计与分析提供了理论参考.
Research on Simulation of Expansion and Locking Process of Aircraft Folding Rudder
The expansion and locking process of aircraft folding rudder is a dynamic process of multi-load synthesis.The dynamic process is studied by simulation.The dynamic simulation model is established,considering aerodynamic load and friction action in the whole dynamic process.The influence of different aerodynamic load on dynamic process is analyzed by dynamically simulating the condition of obstruction,no-load and promoting aerodynamic load.By comparing the result of no-load expansion test with the simulation result of no-load condition,the accuracy of the dynamic simulation model is verified.Based on this dynamic simulation model,the friction work under different aerodynamic load condition is identified by using angular acceleration method and angular velocity method respectively from load and energy dimensions.The result of the study shows that the friction torque is affected by aerodynamic load.The friction work increases with the increase of aerodynamic promotion.The angular acceleration method and angular velocity method are both reasonable to identify the friction work.The research provides theoretical reference for engineering design and analysis of aircraft folding rudder.

aircraft folding rudderthe process of expansion and lockingdynamic simulationaerodynamic loadidentification of friction work

陈克、吴佳奕、金玲、卞亚东、徐倩

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北京宇航系统工程研究所,北京,100076

中国运载火箭技术研究院,北京,100076

飞行器折叠舵 展开及锁紧过程 动力学仿真 气动载荷 摩擦做功辨识

2024

导弹与航天运载技术
中国运载火箭技术研究院

导弹与航天运载技术

CSTPCD北大核心
影响因子:0.238
ISSN:1004-7182
年,卷(期):2024.(3)