Control system for a gas turbine

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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F02C 908

Patent

active

040117170

ABSTRACT:
A control system for a gas turbine, which control system comprises a fuel pressurizing pump and two fuel flow restrictors supplied with fuel at different pressures from the pump, said restrictors being in communication with a common fuel pipe line, and there being electrically actuated means, e.g. a rotenoid, for varying the fuel pressure in the common fuel pipe line whereby said varying fuel pressure can be used for controlling the output of the gas turbine.

REFERENCES:
patent: 2940394 (1960-06-01), Mosure
patent: 3043367 (1962-07-01), Abraham
patent: 3514948 (1970-06-01), Wayne
patent: 3713290 (1973-01-01), Gold
patent: 3780527 (1973-12-01), Lewis

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