CONSTANT-VELOCITY DRIVE SYSTEM FOR GIMBALED ROTOR HUBS
摘要
<p>A constant-velocity drive system for a rotary-wing aircraft rotor comprising a differential torque-splitting mechanism and a gimbal mechanism is disclosed. A rotary-wing aircraft having a rotary-wing aircraft rotor comprising a differential torque-splitting mechanism and a gimbal mechanism is disclosed.</p>
申请公布号
EP2018319(A2)
申请公布日期
2009.01.28
申请号
EP20060851645
申请日期
2006.05.19
申请人
BELL HELICOPTER TEXTRON INC.
发明人
RAUBER, RICHARD;STAMPS, FRANK, B.;BRASWELL, JAMES, LEE, JR.
