发明名称 |
Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
摘要 |
A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration control system rotating with the rotating rotary wing hub driven to rotate about a rotating hub center Z axis by a gear box transmission. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating about the rotating hub center Z axis relative to the nonrotating body, a first nonrotating body vibration sensor outputting first nonrotating body vibration sensor data correlating to vibrations. |
申请公布号 |
US8267652(B2) |
申请公布日期 |
2012.09.18 |
申请号 |
US20100771153 |
申请日期 |
2010.04.30 |
申请人 |
JOLLY MARK R.;BLACK PAUL;LORD CORPORATION |
发明人 |
JOLLY MARK R.;BLACK PAUL |
分类号 |
F04D29/26;B64C11/00;F01D5/26 |
主分类号 |
F04D29/26 |
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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