Gas turbine fuel control system

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

Patent

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Details

60 3928R, F02C 932

Patent

active

043376150

ABSTRACT:
An electronic fuel control system for varying the fuel flow to a gas turbine engine during the engine's acceleration. The reference speed set point of the engine's fuel controlling governor is increased as a function of the elapsed time from engine start-up and the engine characteristics so that the engine accelerates substantially along its "required to run line."

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patent: 4044554 (1977-08-01), West
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