Ice management system for tiltrotor aircraft

Details Ice management system for tiltrotor aircraft Ice management system for tiltrotor aircraft

H - Electricity

05

B

H05B 1/02 (2006.01)

Patent

CA 2597483

An ice management system is configured for an aircraft having at least one rotor (11), each rotor having a plurality of blades. The system has an alternating current (AC) electrical power supply for supplying AC power (13), the AC power supply being adapted to be carried by the aircraft remote from the rotor (11). A converter converts the AC power to direct-current (DC) power. At least one ice protection device is carried by the rotor and operated using the DC power.

Système de gestion de glace pour un aéronef ayant au moins un rotor (11), chaque rotor ayant une pluralité de lames. Le système a une alimentation électrique par courant alternatif (CA) pour fournir une alimentation CA (13), l~alimentation électrique CA étant apte à être transportée par l~avion à l~écart du rotor (11). Un convertisseur convertit l~alimentation CA en une alimentation par courant continu (CC). Au moins un dispositif de protection contre la glace est transporté par le rotor et fonctionne à l~aide de l~alimentation CC.

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