| 卫星真空热试验倾斜姿态模拟装置的设计 |
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| 引用本文： | 李日华,袁伟峰,高庆华,裴一飞.卫星真空热试验倾斜姿态模拟装置的设计[J].航天器环境工程,2015,32(5):554-559. |
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| 作者姓名： | 李日华 袁伟峰 高庆华 裴一飞 |
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| 作者单位： | 北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094;北京卫星环境工程研究所, 北京 100094 |
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| 摘 要： | 为验证月球地形表面坡度以及重力环境对探测器及设备性能的影响,设计了一种探测器倾斜姿态模拟装置。该装置采用双曲柄摇块机构,主要由步进电机、螺旋升降机、转动平台(连架杆)、底框等组成。针对10-4 Pa的高真空和100 K低温的使用环境以及大尺寸、重负载和高精度的使用要求,讨论了探测器倾斜姿态模拟装置设计时所面临的系列问题及解决方法。该装置已成功应用于"嫦娥三号"以及"嫦娥五号"的真空热试验,满足试验对装置提出的各项指标要求。
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| 关 键 词： | 真空热试验 倾角机构 模拟装置 真空低温环境 |
| 收稿时间： | 2015/2/27 0:00:00 |
| 修稿时间： | 2015/10/9 0:00:00 |
Design of simulation device for spacecraft inclined posture in thermal vacuum test |
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| Li Rihu,Yuan Weifeng,Gao Qinghua and Pei Yifei.Design of simulation device for spacecraft inclined posture in thermal vacuum test[J].Spacecraft Environment Engineering,2015,32(5):554-559. |
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| Authors: | Li Rihu Yuan Weifeng Gao Qinghua and Pei Yifei |
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| Institution: | Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China |
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| Abstract: | In order to verify the influence of the surface slope and the gravity environment on the performance of the lunar probe and the related equipment, a device for simulating the inclined posture of probe is designed. The device is a double crank rocker mechanism, including the stepper motor, the spiral elevator, the rotating platform and the frame. In the environment of high vacuum and ultralow temperature, and with the requirements of large size, over loading and high precision, the related difficulties in the course of designing are discussed. The mechanism is successfully applied to the Chang''e-3 and Chang''e-5 thermal vacuum tests, with all requirements satisfied. |
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| Keywords: | vacuum thermal test inclined angle adjuster simulation device vacuum and cryogenic environment |
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