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一种浮动锁销式柔性气浮组件的承载特性测试及分析
引用本文:陈飞飞,王宏,许红亮,黄利强,肖杰.一种浮动锁销式柔性气浮组件的承载特性测试及分析[J].航天器环境工程,2017,34(6):631-635.
作者姓名:陈飞飞  王宏  许红亮  黄利强  肖杰
作者单位:上海宇航系统工程研究所, 上海 201109
基金项目:上海航天技术研究院材料与工艺自主研发项目“平面SAR天线多环闭环链机构装配精度预测及调整技术研究”(编号:Z13065)
摘    要:为在空间机构产品集成与测试中合理使用气浮组件,采用刚度试验台模拟加载的方案对一种浮动锁销式柔性气浮组件的承载特性进行测试。试验结果表明:浮动锁销式柔性气浮组件在未预压缩状态下,承载特性近似为线性弹簧压缩模型;在预压缩状态下,初始承载特性近似为刚体,承载力超过气浮组件的保持力后承载特性近似为线性弹簧压缩模型。因此,为避免气浮组件在承载过程中表现出的作用力与位移变化等特性对空间机构产品的运动特性、系统性能造成显著的附加影响,气浮组件在使用前应根据产品重力调节弹簧预压缩量,并严格控制4组可调弹簧支撑组件的制造误差;同时,在产品重力完全被卸载之前需要借助压紧释放机构或刚性支撑工装对产品进行约束。

关 键 词:空间机构  微重力模拟  柔性气浮组件  承载特性  测试试验
收稿时间:2017/5/10 0:00:00
修稿时间:2017/11/22 0:00:00

Experimental analysis of the bearing characteristics of a floating lockpin type flexible flotation device
CHEN Feifei,WANG Hong,XU Hongliang,HUANG Liqiang,XIAO Jie.Experimental analysis of the bearing characteristics of a floating lockpin type flexible flotation device[J].Spacecraft Environment Engineering,2017,34(6):631-635.
Authors:CHEN Feifei  WANG Hong  XU Hongliang  HUANG Liqiang  XIAO Jie
Institution:Shanghai Institute of Aerospace Systems Engineering, Shanghai 201109, China
Abstract:In order to use the flotation device reasonably in the product integration and the test of the space mechanism, the bearing characteristics of a floating lockpin type flexible flotation device are tested by using a stiffness test bed under an analog loading. The results show that the bearing characteristics of the flotation device can be approximated by a linear spring compression model for the flotation device not being pre-compressed. When the flotation device is pre-compressed, the bearing characteristics of the flotation device can be approximated by a rigid body in the initial stage. As the bearing capacity exceeds the holding force of the flotation device, the bearing characteristics of the flotation device can be approximated by a linear spring compression model. In order to avoid the serious influence of the change of force and displacement in the loading process of the flotation device on the motion characteristics and the system performance of the space mechanism, the spring pre-compression of the flotation device should be adjusted according to the gravity product before the flotation device is used. In addition, the manufacturing errors of four groups of adjustable spring support assemblies should be strictly controlled. Moreover, the product should be constrained by using a release mechanism or a rigid support device before the gravity of the product is completely balanced.
Keywords:space mechanism  microgravity simulation  flexible flotation device  bearing characteristics  measurement and test
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