发明名称 |
PASSIVE, MULTI-AXIS, HIGHLY DAMPED, SHOCK ISOLATION MOUNTS |
摘要 |
A passive, multi-axis, highly damped, shock load isolation mount which can serve as a complete one-piece mount, particularly of a spacecraft to its launch vehicle or launch vehicle adaptor structure, or can serve in multiplicity as necessary to provide a complete shock load isolation mounting system. When used as a one-piece mount or used in multitude as a system, the invention provides substantial reduction in the shock load transmission to a payload from its support base for both axial load and lateral loads. The unique multi-layered, opposed beam, contorted load path flexure design combined with a shear wall type constrained layer damping treatment provides substantial shock load isolation in a durable, reliable, lightweight, and compact form.
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申请公布号 |
WO0170573(A2) |
申请公布日期 |
2001.09.27 |
申请号 |
WO2001US08777 |
申请日期 |
2001.03.19 |
申请人 |
CSA ENGINEERING, INC. |
发明人 |
WILKE, PAUL, S.;JOHNSON, CONOR, D.;PENDLETON, SCOTT, C. |
分类号 |
B64G1/00;B64G1/64;F16F1/02;F16F3/12;F16F15/08;(IPC1-7):B64G/ |
主分类号 |
B64G1/00 |
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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