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系外行星成像星冕仪振动夹具设计与试验分析

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为设计满足巡天空间望远镜系外行星成像星冕仪振动试验要求的夹具,对初步设计的振动夹具进行模态仿真分析.根据分析结果,识别夹具薄弱环节,并对振动夹具进行改进设计.通过分析计算,改进后的夹具满足设计固有频率要求.并对其进行正弦振动和随机振动动力学分析.将夹具在振动台上进行正弦扫频试验,验证设计合理性.夹具的仿真一阶模态结果342.6 Hz,其振动试验结果一阶模态为329 Hz.振动夹具一阶固有频率的试验结果与仿真计算误差约为4%,误差合理.试验验证了仿真计算结果的正确性.实现了振动夹具的基频大于试验件3倍的目标,振动夹具设计合理.满足巡天空间望远镜系外行星成像星冕仪力学环境试验使用.
Design and Experiment Analysis of Vibration Fixture for Cool Planet Imaging Coronagraph
The vibration fixture is designed to meet the vibration test requirements of cool planet imaging coronagraph in space survey telescope.Firstly,the modal simulation calculation was carried out for the preliminary design of the vibration fixture.According to the modal analysis results,the weaknesses were identified and the design of vibration fixture was improved.By analysis calculation,the fixture after design improvement can meet the design requirement of frequency.Then the sinusoidal vibration and random vibration dynamics were analyzed.Sinusoidal sweep test of the fixture was carried out on the shaking table in order to verify the rationality of the design.The first-order mode simulation result of fixture is 342.6 Hz,and the first-order mode of vibration test analysis is 329 Hz.There was an error of 4%between the natural frequency test result of the fixture and simulation calculation.The simulation results are verified by experiments.The objective is attained for the fundamental frequency of the vibration fixture is 3 times greater than the tested object,and the design of vibration fixture is reasonable.The fixture can meet the requirements of mechanical environment test of the cool planet imaging coronagraph for space survey telescope.

fixture designmodal analysissinusoidal vibrationrandom vibrationvibration test

郭伟、许明明、孔令一、窦江培

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中国科学院南京天文光学技术研究所,南京 210042

中国科学院天文光学技术重点实验室(南京天文光学技术研究所),南京 210042

夹具设计 模态分析 正弦振动 随机振动 振动试验

国家自然科学基金项目国家自然科学基金项目中国空间站工程项目

12103073U2031210201906

2024

环境技术
广州电器科学研究院有限公司

环境技术

CSTPCD
影响因子:0.995
ISSN:1004-7204
年,卷(期):2024.42(1)
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