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航天器推进系统水击及其抑制方法

晏政 彭小辉 程玉强 吴建军

晏政, 彭小辉, 程玉强, 吴建军. 航天器推进系统水击及其抑制方法[J]. 航空动力学报, 2012, 27(9): 2028-2034.
引用本文: 晏政, 彭小辉, 程玉强, 吴建军. 航天器推进系统水击及其抑制方法[J]. 航空动力学报, 2012, 27(9): 2028-2034.
YAN Zheng, PENG Xiao-hui, CHENG Yu-qiang, WU Jian-jun. Research of water hammer and its suppression methods for spacecraft propulsion system[J]. Journal of Aerospace Power, 2012, 27(9): 2028-2034.
Citation: YAN Zheng, PENG Xiao-hui, CHENG Yu-qiang, WU Jian-jun. Research of water hammer and its suppression methods for spacecraft propulsion system[J]. Journal of Aerospace Power, 2012, 27(9): 2028-2034.

航天器推进系统水击及其抑制方法

Research of water hammer and its suppression methods for spacecraft propulsion system

  • 摘要: 针对航天器推进系统充填和关机过程水击这一动力学问题,基于已建立的航天器推进系统仿真模型,开展了某型推进系统的仿真研究,并重点分析了节流孔、弯管对推进剂供应管路水击的抑制作用.研究结果表明:①在推进系统充填和关机过程中,其不同位置均出现了明显的水击现象,充填过程水击频率较低,而关机过程水击频率较高,关机过程的水击峰值压力显著高于充填过程;②节流孔可显著削弱充填过程中的压力和流量振荡,关机过程的水击需要由较小的节流孔才能有效抑制;③弯管可明显削弱充填过程中的压力和流量振荡,对流量振荡的抑制效果尤为显著,但弯管对关机过程水击的抑制效果不明显.

     

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出版历程
  • 收稿日期:  2012-03-28
  • 刊出日期:  2012-09-28

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