发明名称 DUAL-FREQUENCY ACTIVE VIBRATION CONTROL
摘要 A system for active vibration control includes an actuator configured to reduce the impact of a vibratory load imposed on an airframe of a rotorcraft to an amount that is less than a threshold; and a controller configured to determine the vibratory load based on the data, and set an eccentric rotational speed of an actuator at a first frequency and modulate the eccentric rotational speed by a second frequency based on the vibratory load. Also a method includes obtaining, by the controller, data; determining, by the controller, a vibratory load based on the data; and setting, by the controller, an eccentric rotational speed of an actuator at a first frequency and modulating the eccentric rotational speed by a second frequency based on the vibratory load.
申请公布号 US2015097074(A1) 申请公布日期 2015.04.09
申请号 US201314045140 申请日期 2013.10.03
申请人 Sikorsky Aircraft Corporation 发明人 Andrews Joseph John;Millott Thomas A.
分类号 B64C27/00 主分类号 B64C27/00
代理机构 代理人
主权项 1. A method comprising: obtaining, by a controller comprising a processor, data; determining, by the controller, a vibratory load based on the data; and setting, by the controller, an eccentric rotational speed of an actuator at a first frequency and modulating the eccentric rotational speed by a second frequency based on the vibratory load.
地址 Stratford CT US