Fuel control method and apparatus

Details Fuel control method and apparatus Fuel control method and apparatus

F - Mech Eng,Light,Heat,Weapons

02

C

60/181, 341/38.1

F02C 9/26 (2006.01) F02C 9/28 (2006.01) F02C 9/36 (2006.01) F02M 51/02 (2006.01)

Patent

CA 1172729

FUEL CONTROL METHOD AND APPARATUS Abstract A fuel control for a gas turbine engine has a positive displacement pump (10) which directs fuel to a constant flow regulator (14) which generates a constant flow of fuel. A flow diverter (16) includes a dividing device which divides the constant flow of fuel between a discharge conduit (18) connected to the burner nozzles of the engine and a bypass conduit (20) connected to the inlet side of the pump. A computer (22) which is adapted to sense various engine parameters; and calculate fuel flow controls the flow dividing device in order to apportion the flow so that the calculated fuel flow is delivered to the engine.

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