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Rotorcraft rotor with constant velocity joint and a torque-splitting differential
Rotorcraft rotor with constant velocity joint and a torque-splitting differential
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机译:具有等速万向节和扭矩分离差速器的旋翼飞机旋翼
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摘要
The rotor engagement system has a rotor shaft (7) and shaft connections. There are two blade retainers. There is a differential mechanism separating static coupling and authorizing relative movement perpendicular to the shaft axis between two units (40,41) of the drive unit. the differential mechanism is made up of three discs (9,10,11) superimposed and coaxial around the shaft axis.
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