发明名称 |
ATMOSPHERIC TURBULENCE ISOLATION SYSTEM AND METHOD |
摘要 |
A vibration isolation assembly for an aerodynamic object comprises a viscoelastic inner layer disposed on the aerodynamic object and being configured to attenuate vibration. The vibration isolation assembly further comprises a rigid or stiff outer layer disposed on an inner layer. The vibration isolation assembly may attenuate the transmission of aerodynamically-induced vibration to components contained or mounted to the aerodynamic object.
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申请公布号 |
US2010078863(A1) |
申请公布日期 |
2010.04.01 |
申请号 |
US20080240754 |
申请日期 |
2008.09.29 |
申请人 |
THE BOEING COMPANY |
发明人 |
ULLMAN ALAN Z.;GRIFFIN STEVEN F. |
分类号 |
F16M1/08;B64C23/00;F16F1/00 |
主分类号 |
F16M1/08 |
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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