DYNAMIC SHAPE MAINTENANCE OF AEROSPACE SUBSYSTEMS USING TUNED MASS DAMPERS

申请号 US14699283 申请日 2015-04-29 公开(公告)号 US20160319895A1 公开(公告)日 2016-11-03
申请人 The Boeing Company; 发明人 Steven F. Griffin; Guy D. Granger;
摘要 A vibration damping system employs a component having a directionally sensitive element thereon, mounted to an aircraft, which experiences dynamic excitation that induces bending deflection in the component that will reorient the directionally sensitive element. At least one tuned mass damper is mounted on the component in an orientation in which an internal mass of the tuned mass damper is moveable such that the tuned massed damper absorbs and attenuates at least a portion of the deflective motion, to thereby suppress bending deflection of the component in the particular axial direction and generally maintain the linearity of the directionally sensitive element.
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