首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Design and dynamic analysis of landing gear system in vertical takeoff and vertical landing reusable launch vehicle
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Design and dynamic analysis of landing gear system in vertical takeoff and vertical landing reusable launch vehicle

机译:垂直起飞和垂直着陆可重复使用运载火箭起落架系统的设计和动力学分析

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摘要

Landing gear system is a key part of the implementation of reusable vertical takeoff and vertical landing launch vehicle, where its buffing performance is directly related to the vehicle whether it can land safely or stably. According to the reusable launch vehicle general scheme, outrigger landing legs are designed, and the hydraulic absorber is used for the landing gear system. Meanwhile, a scaling principle prototype of landing gear system is developed, and the landing impact test is carried out. A dynamic simulation model of the landing vehicle has been set up, researching the influence of parameters, such as the horizontal velocity, initial inclination, surface friction coefficient, and pitch angular velocity on the landing performance. Four kinds of extreme conditions are identified, and dynamic response characteristics of landing system under each extreme condition are conducted. The simulation results are in good agreement with the experimental data. The buffing performance of the vehicle meets the design requirements, which provides a reference for the design of landing gear system of the vehicle.
机译:起落架系统是可重复使用的垂直起降和垂直着陆发射飞行器实施过程中的关键部分,无论其能否安全着陆或稳定降落,其抛光性能都与飞行器直接相关。根据可重复使用的运载火箭总体方案,设计了支腿式起落架,液压吸收器用于起落架系统。同时,开发了起落架系统的定标原理样机,并进行了起落架冲击试验。建立了起落架动力学仿真模型,研究了水平速度,初始倾角,表面摩擦系数,俯仰角速度等参数对着陆性能的影响。确定了四种极端条件,并对每种极端条件下的着陆系统进行了动力响应分析。仿真结果与实验数据吻合良好。车辆的抛光性能满足设计要求,为车辆起落架系统的设计提供了参考。

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