Gas turbine engine fuel control

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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Details

60 3925, 60 3928R, 192 0084, F02C 904

Patent

active

042664012

ABSTRACT:
A control system for a gas turbine engine includes provisions for adjusting fuel flow in relation to gas generator speed, and for adjusting guide vane position in relation to power turbine speed.

REFERENCES:
patent: 3252686 (1966-05-01), Chadwick
patent: 3283503 (1966-11-01), Cowles
patent: 3521446 (1970-07-01), Maljanian
patent: 3686859 (1972-08-01), White
patent: 3814537 (1974-06-01), Stoltman

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