Integrated engine and transmission units for rotary wing...

Details Integrated engine and transmission units for rotary wing... Integrated engine and transmission units for rotary wing...

B - Operations, Transporting

64

C

B64C 27/14 (2006.01)

Patent

CA 2379568

A power plant and transmission arrangement (100) for a helicopter wherein the helicopter engine (102) is integrated to the helicopter transmission (106) to form therewith a single unit rigidly mounted to the helicopter frame (110). By so integrating the engine to the helicopter transmission the center of gravity of the engine can be placed closer to the rotor mast (112) of the helicopter, thereby enhancing the stability and the handling characteristics of the helicopter.

L'invention concerne un dispositif (100) de groupe propulseur et de transmission destiné à un hélicoptère. Le moteur (102) de l'hélicoptère est intégré à la transmission (106) de l'hélicoptère de manière à former une seule unité solidement montée au cadre (110) de l'hélicoptère. Grâce à l'intégration du moteur dans la transmission de l'hélicoptère, le centre de gravité dudit moteur peut être placé plus près du mât rotor (112) de l'hélicoptère, ce qui permet d'améliorer la stabilité ainsi que les caractéristiques de comportement et de pilotage de l'hélicoptère.

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