Sikorsky Aircraft Corporation

Matthew Fogarty

Mark P Eisenhauer

Frederick L Bourne

Robert F Longley, Jr

A rotor ice protection system (RIPS) apparatus for an aircraft to heat aircraft rotor blades is provided. The RIPS apparatus includes circuitry disposed to transmit electrical loads associated with RIPS operations, an indicator unit disposed to alert a pilot of the aircraft to a RIPS condition indicating an operating status of the RIPS operations, a controller configured to actuate the RIPS operations in accordance with current conditions and to issue a command to the indicator unit to alert the pilot to the RIPS operations according to the actuation and a sensor system disposed to sense whether the circuitry is transmitting the electrical loads and to provide a sensing result to the indicator unit. The indicator unit additionally alerts the pilot to the RIPS operations according to the sensing result.

Rotor ice protection system

A method of operating an electrical system of an aircraft is provided. The method includes initiating a cross-start action for cross-starting a non-operative engine using a generator of an operative engine, entering a power limiting mode of a generator control unit (GCU) of the operative engine, remaining in the power limiting mode for a duration of the cross-start action and returning to the non-power limiting mode of the GCU of the operative engine upon completion of the cross-start action.

Growing community of inventors

Monroe, CT, United States of America

Matthew Fogarty