Constant-velocity drive system for gimbaled rotor hubs

Details Constant-velocity drive system for gimbaled rotor hubs Constant-velocity drive system for gimbaled rotor hubs

B - Operations, Transporting

64

C

B64C 27/28 (2006.01) B64C 27/35 (2006.01) B64C 27/58 (2006.01) B64C 29/00 (2006.01)

Patent

CA 2652777

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.

L'invention concerne un système d'entraînement homocinétique pour un rotor d'aéronef à voilure tournante, comprenant un mécanisme différentiel à répartition de couple et un mécanisme à cardan. L'invention concerne également un aéronef à voilure tournante présentant un rotor d'aéronef à voilure tournante comprenant un mécanisme différentiel à répartition de couple et un mécanisme à cardan.

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