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 |