| 发明名称 |
DISTRIBUTED ACTIVE VIBRATION CONTROL SYSTEMS AND ROTARY WING AIRCRAFT WITH SUPPRESSED VIBRATIONS |
| 摘要 |
A method and system is disclosed for controlling problematic vibrations in an aircraft having. The method and system have the ability to cancel problematic rotary wing helicopter vibrations using independent active force generator power and with distributed communications therebetween. |
| 申请公布号 |
US2012158217(A1) |
申请公布日期 |
2012.06.21 |
| 申请号 |
US201113333196 |
申请日期 |
2011.12.21 |
| 申请人 |
JOLLY MARK R.;BADRE-ALAM ASKARI;ALTIERI RUSSELL E.;MEYERS ANDREW D. |
发明人 |
JOLLY MARK R.;BADRE-ALAM ASKARI;ALTIERI RUSSELL E.;MEYERS ANDREW D. |
| 分类号 |
G05D1/00;H02K15/00 |
主分类号 |
G05D1/00 |
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