Gaseous fuel compression and control system for gas turbine engi

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

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60 39465, 417 45, F02C 930

Patent

active

056068530

ABSTRACT:
A gaseous fuel compression and control system for gas turbine engine (30) comprises a screw compressor (10) driven by an electric motor (11) for feeding gaseous fuel to the gas turbine engine, and a modulating device (12) for modulating the rotational speed of the motor by controlling the frequency of electric power to the motor in response to sensed output power of the gas turbine engine.

REFERENCES:
patent: 3693601 (1972-09-01), Sauder
patent: 4815278 (1989-03-01), White
patent: 4922710 (1990-05-01), Rowen et al.
patent: 4971522 (1990-11-01), Butlin
patent: 5103629 (1992-04-01), Mumford et al.

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