-
公开(公告)号:US20090184209A1
公开(公告)日:2009-07-23
申请号:US12301191
申请日:2006-05-19
CPC分类号: B64C27/41 , B64C27/52 , B64C29/0033 , F16C1/04
摘要: 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.
摘要翻译: 公开了一种用于旋转翼飞行器转子的恒速驱动系统,其包括差动转矩分解机构和万向架机构。 公开了具有旋转翼飞行器转子的旋转翼飞机,其包括差速扭矩分离机构和万向架机构。