Ice management system for tiltrotor aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 15/12 (2006.01)

Patent

CA 2586094

An ice management system is configured for an aircraft having at least one rotor, each rotor having a plurality of blades. The system has an electrical power supply adapted to be carried by the aircraft remote from the rotor, and at least one heater is carried by the rotor for heating at least a portion of the rotor. A solid-state control relay is carried by the rotor and conductively coupled between the power supply and each heater for selectively controlling the flow of electrical power from the power supply to each heater. In addition, the system may incorporate a solid-state feed relay carried by the aircraft remote from the rotor and conductively coupled between the power supply and the control relay for selectively controlling the flow of electrical power to the control relay.

La présente invention concerne un système de gestion de la glace qui est configuré pour un avion ayant au moins un rotor, chaque rotor ayant une pluralité de pales. Le système possède une alimentation électrique adaptée pour être transportée par l~avion à distance du rotor et au moins un dispositif de chauffage est transporté par le rotor pour chauffer au moins une partie du rotor. Un relais de commande à semi-conducteurs est transporté par le rotor et couple de manière conductrice entre l~alimentation électrique et chaque dispositif de chauffage pour réguler de manière sélective l~écoulement d~énergie électrique de l~alimentation électrique à chaque dispositif de chauffage. De plus, le système peut incorporer un relais d~alimentation à semi-conducteurs transporté par l~avion à distance du rotor et couplé de manière conductrice entre l~alimentation électrique et le relais de commande pour réguler de manière sélective l~écoulement d~énergie électrique vers ledit relais de commande.

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