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.
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
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