Gas turbine engine fuel control

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

Patent

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60/151

F02C 9/54 (2006.01) F02C 6/20 (2006.01) F02C 9/26 (2006.01) F02B 1/04 (2006.01)

Patent

CA 1134153

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

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