Gas turbine engine fixed collective takeoff compensation...

Details Gas turbine engine fixed collective takeoff compensation... Gas turbine engine fixed collective takeoff compensation...

B - Operations, Transporting

64

D

B64D 31/06 (2006.01) B64C 19/00 (2006.01) B64C 19/02 (2006.01) F01D 15/00 (2006.01) F01D 21/14 (2006.01) F02C 9/00 (2006.01)

Patent

CA 2654810

A system and method of controlling a gas turbine engine controller in a rotorwing aircraft includes determining when a fixed collective takeoff (FCTO) of the rotorwing aircraft is being conducted. A control loop gain of the gas turbine engine controller is at least selectively varied when the FCTO is being conducted.

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