Gas turbine engine fuel supply control

Power plants – Combustion products used as motive fluid – Different fluids

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F02C 726

Patent

active

039628639

ABSTRACT:
Fuel supply control means is operatively connected to an electromagnetic flow control valve applying thereto a fuel control signal for controlling fuel flow supplied through the electromagnetic flow control valve to the combustion chamber of a gas turbine engine. The control signal increases gradually or exponentially from a low value such as corresponds to fuel flow required at engine hot start to a high value corresponds to fuel flow required at engine cold start.

REFERENCES:
patent: 2880790 (1959-04-01), Mock
patent: 3059427 (1962-10-01), Thorpe et al.
patent: 3469395 (1969-09-01), Spitsbergen et al.
patent: 3834158 (1974-09-01), Oppmann

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