Gas turbine engine fuel control

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

Patent

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341/95, 341/38.1

F02C 9/26 (2006.01) F02C 9/28 (2006.01)

Patent

CA 1193694

GAS TURBINE ENGINE FUEL CONTROL Abstract of the Disclosure: The ability of a gas turbine engine to recover from surge is enhanced by implementing a closed loop control mode wherein fuel flow is varied as a function of the ratio of the rate of change of engine gas generator speed to compressor discharge pressure.

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