Electronic fuel control system for a gas turbine engine

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

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341/38.12

F02C 9/28 (2006.01)

Patent

CA 1157126

ELECTRONIC FUEL CONTROL SYSTEM FOR A GAS TURBINE ENGINE ABSTRACT An electronic fuel control system for con- trolling the rate at which fuel is supplied to a gas turbine engine which controls turbine speed, accelera- tion, and combustor temperature as a function of ambient temperature and turbine speed. A predetermined fuel schedule controls the maximum and minimum amount of fuel supplied to the gas turbine engine during transient and steady-state operation, and sequences operation from a starting fuel schedule to a running fuel schedule. A transient fuel boosting function temporarily overrides the temperature limit control when a speed increase is called for.

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