| 发明名称 |
CONSTANT-VELOCITY DRIVE SYSTEM FOR GIMBALED ROTOR HUBS |
| 摘要 |
A constant-velocity drive system for a rotary-wing aircraft rotor compris ing a differential torque-splitting mechanism and a gimbal mechanism is disc losed. A rotary-wing aircraft having a rotary-wing aircraft rotor comprising a differential torque- splitting mechanism and a gimbal mechanism is disclo sed.
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| 申请公布号 |
CA2652777(A1) |
申请公布日期 |
2008.04.17 |
| 申请号 |
CA20062652777 |
申请日期 |
2006.05.19 |
| 申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
STAMPS, FRANK B.;RAUBER, RICHARD;BRASWELL, JAMES LEE JR. |
| 分类号 |
B64C27/28;B64C27/35;B64C27/58;B64C29/00 |
主分类号 |
B64C27/28 |
| 代理机构 |
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