发明名称 |
Uncoupled vibrion attenuation/isolation devices |
摘要 |
The present invention relates to a vibration attenuation/isolation device. An implementation of the invention provides an improved whole-spacecraft vibration attenuation/isolation by separating the vibration load on the spacecraft that arise from the launch vehicle and fairing into longitudinal and lateral components, and effectively attenuates and/or isolates those components. The invention also provides a general method for reducing vibrations in an assembly by using a vibration control device that separates the vibrational forces into perpendicular components that can be separately damped or attenuated.
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申请公布号 |
US2008048069(A1) |
申请公布日期 |
2008.02.28 |
申请号 |
US20060601547 |
申请日期 |
2006.11.16 |
申请人 |
ZHENG GANGTIE;LIU LIKUN;LIANG LU;HE LING |
发明人 |
ZHENG GANGTIE;LIU LIKUN;LIANG LU;HE LING |
分类号 |
B64G1/52;F16F7/10 |
主分类号 |
B64G1/52 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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