冲压式翼伞滑布控制开伞技术研究  被引量:1

Research on Slider-reefed Control Technology of Ram-air Parafoil

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作  者:张宇晨 胡雪鹏 张红英[1] 缪玉文 ZHANG Yuchen;HU Xuepeng;ZHANG Hongying;MIAO Yuwen(College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;AVIC Aerospace Life-support Industries Ltd.,Xiangyang 441003,China)

机构地区:[1]南京航空航天大学航空学院,南京210016 [2]航空工业航宇救生装备有限公司,襄阳441003

出  处:《航天返回与遥感》2023年第2期14-23,共10页Spacecraft Recovery & Remote Sensing

基  金:航空科学基金(20200029052004)。

摘  要:为了研究滑布收口控制对冲压式翼伞开伞动载的影响,文章应用结构化任意拉格朗日-欧拉(Structured Arbitrary Lagrange-Euler,S-ALE)方法对翼伞系统在无滑布收口控制和有滑布收口控制两种情况下进行了开伞过程的流固耦合仿真计算,分析了滑布收口对翼伞开伞过程的影响。结果表明:滑布收口控制可以有效降低冲压式翼伞的充气速度、伞衣应力和开伞动载,开伞动载可以降低33%。但有滑布收口控制时,翼伞的气室饱满程度有所下降,边缘气室饱满程度的下降更明显;由于滑布在开伞过程中对翼伞前后缘伞绳受力的影响有差别,使得某些伞绳出现松弛现象,这会对冲压式翼伞俯仰稳定性有一定影响。通过研究滑布收口控制对冲压式翼伞开伞动载的影响,可以为冲压式翼伞收口技术的设计与应用提供参考。In order to study the influence of the slider-reefed control on the dynamic load of the parafoil opening,the simulation calculation was carried out for the parafoil opening process in two cases,without slider-reefed control and with slider-reefed control.The simulation calculation uses the structured arbitrary Lagrange-Euler(S-ALE)method.The influence of the slider-reefed control on the parafoil opening process was analyzed.The results show that the slider-reefed control can effectively reduce the inflation rate of the parafoil,the stress of the canopy and the dynamic load of the parafoil.The dynamic load of the parafoil can be reduced by 33%.However,the fullness of cells is decreased,and the decrease of the fullness of the edge cells is more obvious when the slider-reefed control is used;Due to the difference in the influence of the slider on the force of the paracord in the previous and the paracord in the back during the opening process,it causes that some of the paracords to sag,so that the pitching stability of parafoil is affected.By studying the influence of slider reefed control on the dynamic load of the parafoil opening,it can provide a reference for the design and application of parafoil reefed technology.

关 键 词:冲压式翼伞 开伞动载 滑布收口 流固耦合 结构化任意拉格朗日-欧拉 

分 类 号:V244.21[航空宇航科学与技术—飞行器设计]

 

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