Fuel control system for gas turbine engine

Details Fuel control system for gas turbine engine Fuel control system for gas turbine engine

1974-07-18

1976-01-06

Gordon, Clarence R.

Power plants

Combustion products used as motive fluid

Different fluids

60 3928R, F02C 726

Patent

active

039303659

ABSTRACT:
A fuel control system for a gas turbine engine includes a metering device having a sleeve which is movable to vary fuel flow to the engine. A stop cooperates with the sleeve to define a minimum fuel flow. The stop is movable between a first, normal running position and a second, engine starting position, the second position corresponding to a smaller minimum flow through the metering arrangement.

REFERENCES:
patent: 3173468 (1965-03-01), McCombs
patent: 3427804 (1969-02-01), Lawrence
patent: 3514947 (1970-06-01), Bloom
patent: 3530666 (1970-09-01), Cross
patent: 3557552 (1971-01-01), Yates
patent: 3768249 (1973-10-01), Lewis

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