Fuel control system

Power plants – Combustion products used as motive fluid

Patent

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Details

60 3914R, 60 3928R, F02C 726, F02C 932

Patent

active

042815096

ABSTRACT:
A gas turbine fuel control system for controlling the acceleration of an engine during start-up which permits the engine to accelerate substantially along its required-to-run line. Fuel flow to the engine is controlled by a speed governor, and means are included to gradually increase the speed set point of the governor in relation to elapsed time of the start-up period.

REFERENCES:
patent: 3075350 (1963-01-01), McCombs et al.
patent: 4010605 (1977-03-01), Uram
Casamassa et al. Jet Aircraft Power Systems N.Y., McGraw Hill Inc., 1957, pp. 92 & 94.

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