Control means for a gas turbine engine

Rotary kinetic fluid motors or pumps – Method of operation

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Details

415 47, 415175, 415178, F01D 2508

Patent

active

043380611

ABSTRACT:
Clearance control means is provided for a gas turbine engine. In one embodiment relating to compressor blade clearance, means is provided for developing a first signal representative of the actual compressor casing temperature, a second signal representative of compressor inlet gas temperature, and a third signal representative of compressor speed. Schedule means is provided for receiving the gas temperature and compressor speed signals and developing a schedule output signal. The schedule output signal is representative of a reference casing temperature at which a predetermined compressor blade stabilized clearance is provided. Means is provided for comparing the actual compressor casing temperature signal and the reference casing temperature signal and developing a clearance control signal representative of the difference therebetween. The clearance control signal is coupled to a control valve which controls a flow of air to the compressor casing to control the clearance between the compressor blades and the compressor casing. Means is provided for modification of the clearance control signal to accommodate transient characteristics. Other embodiments are disclosed.

REFERENCES:
patent: 2994472 (1961-08-01), Botje
patent: 3736751 (1973-06-01), Fuller
patent: 3966354 (1976-06-01), Patterson
patent: 3975901 (1976-08-01), Hallinger et al.
patent: 3986720 (1976-10-01), Knudsen et al.
patent: 4005946 (1977-02-01), Brown et al.
patent: 4019320 (1977-04-01), Redinger et al.
patent: 4069662 (1978-01-01), Redinger et al.
patent: 4230436 (1980-10-01), Davison
patent: 4230439 (1980-10-01), Smith et al.
patent: 4242042 (1980-12-01), Schwartz

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