Gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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60/151

F02C 9/54 (2006.01)

Patent

CA 1136433

ABSTRACT A method of operating a control system for a gas turbine engine which includes provisions for adjusting fuel flow in relation to gas generator speed, and for adjusting guide vane position in relation to power turbine speed.

382561

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