首页> 外国专利> ZERO GRAVITY SIMULATION DEVICE FOR SATELLITE DEPLOYABLE ANTENNA ASSEMBLY AND TEST

ZERO GRAVITY SIMULATION DEVICE FOR SATELLITE DEPLOYABLE ANTENNA ASSEMBLY AND TEST

机译:卫星可分解天线组装与测试的零重力模拟装置

摘要

PURPOSE: A zero gravity simulation device for assembling and testing a deployable satellite antenna is provided to precisely measure and correct alignment while offsetting self-load due to the earth gravity of a deployable satellite antenna. CONSTITUTION: A zero gravity simulation device for assembling and testing a deployable satellite antenna comprises a triangular shaped frame(210), a first centroid moving unit(220), a second centroid moving unit(230), a third centroid moving unit(240), a connection frame(250), and a helium balloon(260). The frame is coupled with a satellite antenna. The first centroid moving unit is installed in one side of the frame to vary the centroid while slidingly moving along the side. The second centroid moving unit is installed in the first centroid moving unit to vary the centroid while slidingly moving to a direction vertical to the first centroid moving unit. The third centroid moving unit is installed at an angular point of the frame facing with one side of the frame where the first centroid moving unit is installed and varies the centroid while slidingly moving to the first centroid moving unit. One side of the connection frame is connected to the third centroid moving unit.
机译:目的:提供一种用于组装和测试可部署卫星天线的零重力仿真设备,以精确测量和校正对准,同时抵消由于可部署卫星天线的地球引力引起的自负载。组成:用于组装和测试可展开卫星天线的零重力模拟设备,包括三角形框架(210),第一质心移动单元(220),第二质心移动单元(230),第三质心移动单元(240) ,连接框架(250)和氦气球(260)。框架与卫星天线耦合。第一质心移动单元安装在框架的一侧,以在沿该侧滑动时改变质心。第二质心移动单元安装在第一质心移动单元中,以在向垂直于第一质心移动单元的方向滑动的同时改变质心。第三质心移动单元安装在框架的与安装有第一质心移动单元的框架的一侧相对的角点处,并且在向第一质心移动单元滑动移动的同时改变质心。连接框架的一侧连接到第三质心移动单元。

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