Multi-mode tiltrotor nacelle control system with integrated...

Details Multi-mode tiltrotor nacelle control system with integrated... Multi-mode tiltrotor nacelle control system with integrated...

B - Operations, Transporting

64

C

B64C 29/00 (2006.01)

Patent

CA 2392734

A tiltrotor aircraft (11) has a multi-mode tiltrotor nacelle control system with integrated envelope protection (13). The tiltrotor aircraft (11) has a fuselage (15), a tail section (17), a left wing member (21a), a right wing member (21b), a right engine nacelle (23b), a left engine nacelle (23a), a left proprotor (25a), and a right proprotor (25b). Activation of the nacelle control system causes preselected rotational movement of the tiltrotor assembly.

L'invention concerne un système de commande multimode de nacelle de rotor basculant avec protection d'enveloppe intégrée (13) utilisé sur un avion à rotors basculants (11). L'avion à rotors basculants (11) possède un fuselage (15), une queue (17), une aile gauche (21a), une aile droite (21b), une nacelle de rotor gauche (23a), une nacelle de rotor droite (23b), un rotor orientable gauche (25a) et un rotor orientable droit (25b). L'activation du système de commande de nacelle entraîne le mouvement de rotation présélectionné de l'ensemble des rotors basculants.

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