Gas turbine fuel control having fuel viscosity compensation to p

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

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60 3928R, F02C 926

Patent

active

042803233

ABSTRACT:
An arrangement is provided for resetting the fuel inlet pressure to the throttle valve in response to sensed changes in nozzle fuel pressure to compensate for variations in the fuel viscosity resulting from changes in fuel temperature. The fuel nozzle pressure is automatically maintained at a fixed value during the ignition sequence to assure reliable ignition without overfueling throughout the range of site ambient temperature variation.

REFERENCES:
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patent: 3022425 (1962-02-01), Rockstead
patent: 3056259 (1962-10-01), Jubb et al.
patent: 3259037 (1973-09-01), Kiseaden
patent: 3282323 (1966-11-01), Katz et al.
patent: 3566900 (1971-03-01), Black
patent: 3686859 (1972-08-01), White
patent: 3688495 (1972-09-01), Fehler et al.
patent: 3913314 (1975-10-01), Yannone et al.

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