Fuel control system for gas turbine engine operated on gaseous f

Details Fuel control system for gas turbine engine operated on gaseous f Fuel control system for gas turbine engine operated on gaseous f

1976-07-21

1978-05-09

Gordon, Clarence R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3946G, F02C 908

Patent

active

040879615

ABSTRACT:
A gas turbine engine is operated from a gaseous fuel supply whose pressure may occasionally drop from a normal and comparatively high value. The acceleration limit schedule for the engine is established as a function of compressor discharge pressure but this schedule is modified as a function of fuel supply pressure so that, when lower than normal supply pressures exist, the engine may develop substantially the maximum power which is possible at the lower supply pressures.

REFERENCES:
patent: 3279169 (1966-10-01), Bayard
patent: 3413806 (1968-12-01), Belke
patent: 3488948 (1970-01-01), Cornett
patent: 3688495 (1972-09-01), Fehler
patent: 3759037 (1973-09-01), Kiscaden
patent: 3832846 (1974-09-01), Leeson

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