Single rotor helicopter with mixed anti-torque and method to...

Details Single rotor helicopter with mixed anti-torque and method to... Single rotor helicopter with mixed anti-torque and method to...

B - Operations, Transporting

64

C

B64C 27/82 (2006.01) B64C 13/16 (2006.01) G05D 1/08 (2006.01)

Patent

CA 2093701

Hélicoptère comportant : - un unique rotor principal d'avance et de sustentation; et - un système anticouple comprenant : - un rotor auxiliaire anticouple entraîné en rotation à partir des moyens moteurs dudit rotor principal et exerçant une poussée latérale anticouple commandable; et - au moins une surface aérodynamique de direction (14), commandable en orientation et engendrant une portance transversale anticouple. - Selon l'invention, cet hélicoptère comporte des moyens (18, 19) pour commander automatiquement l'angle de braquage de ladite surface aérodynamique de direction (14) en fonction de l'angle de pas collectif dudit rotor principal et de la vitesse d'avance (V) dudit hélicoptère.

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