| 黏弹阻尼技术在航天器上的应用与展望 |
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| 引用本文： | 张少辉,柴洪友,马海全,钱志英.黏弹阻尼技术在航天器上的应用与展望[J].航天器工程,2011,20(1):120-128. |
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| 作者姓名： | 张少辉 柴洪友 马海全 钱志英 |
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| 作者单位： | 北京空间飞行器总体设计部,北京,100094 |
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| 摘 要： | 黏弹阻尼技术作为一种被动振动控制技术,可有效改善航天器的载荷环境.文章对黏弹阻尼技术在航天领域的应用(包括航天器发射段和在轨段)进行了综述,指出了航天黏弹阻尼技术发展的薄弱环节,提出了有针对性的4项建议,涵盖了建模、空间环境试验、优化技术和试验验证方面的内容,并对未来技术的发展作了展望.
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| 关 键 词： | 航天器 黏弹阻尼 结构 |
Progress and Perspect on Viscoelastic Damping Technology for Spacecraft Application |
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| ZHANG Shaohui,CHAI Hongyou,MA Haiquan,QIAN Zhiying.Progress and Perspect on Viscoelastic Damping Technology for Spacecraft Application[J].Spacecraft Engineering,2011,20(1):120-128. |
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| Authors: | ZHANG Shaohui CHAI Hongyou MA Haiquan QIAN Zhiying |
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| Institution: | ZHANG Shaohui CHAI Hongyou MA Haiquan QIAN Zhiying(Beijing Institute of Spacecraft System Engineering,Beijing 100094,China) |
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| Abstract: | Viscoelastic damping technology,as a main passive vibration control technology,can improve the dynamic load environment of a spacecraft.The status of research on viscoelastic damping technology for spacecraft structures is reviewed,including space launch and in-orbit applications.The restraint factors on the development of viscoelastic damping technology are analyzed.The needed research field is also proposed to promote the development of viscoelastic damping technology,including modeling method,space envir... |
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| Keywords: | spacecraft viscoelastic damping structure |
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