发明名称 |
ACTIVE VIBRATION CONTROL DEVICES, SYSTEMS, AND METHODS |
摘要 |
Improved active vibration control (AVC) devices, systems, and related methods are provided herein. An AVC device includes a controller adapted to receive real-time aircraft information and adjust at least one control parameter as a function of the real-time aircraft information is provided. An AVC device is adapted to detect changes in real-time aircraft information, as the aircraft moves from a steady state to transient performance, low and high air speeds, or vice versa. An AVC system (e.g., AVCS) includes one or more sensors, one or more actuators, and a controller adapted to receive real-time aircraft information and adjust at least one control parameter. In some aspects, a method of controlling vibration within an aircraft includes receiving vibration information from at least one sensor, receiving real-time aircraft information from an avionics system, adjusting at least one control parameter used in a control algorithm, and generating a force command. |
申请公布号 |
WO2014168664(A2) |
申请公布日期 |
2014.10.16 |
申请号 |
WO2014US11959 |
申请日期 |
2014.01.17 |
申请人 |
LORD CORPORATION;SWANSON, DOUG A.;BLACK, PAUL R.;RYU, JIHAN;SOUTHWARD, STEVE C.;PEDERSEN, DOUG G. |
发明人 |
SWANSON, DOUG A.;BLACK, PAUL R.;RYU, JIHAN;SOUTHWARD, STEVE C.;PEDERSEN, DOUG G. |
分类号 |
B64C27/00 |
主分类号 |
B64C27/00 |
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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