Closed cycle gas turbine system

Details Closed cycle gas turbine system Closed cycle gas turbine system

1975-01-27

1977-01-04

Ostrager, Allen M.

Power plants

Motive fluid energized by externally applied heat

Heating motive fluid by nuclear energy

60682, 60690, 60652, F01K 2510, F02C 712, F02C 900

Patent

active

040006174

ABSTRACT:
A closed cycle gas turbine system is described employing a precooler for cooling the gas prior to compression. A closed loop coolant circuit for the precooler employs a heat exchanger. A storage tank is provided for storing a supply of coolant at a temperature substantially lower than the temperature of coolant in the coolant circuit at the discharge side of the heat exchanger. Means selectively circulate the coolant in the storage tank through the precooler to provide a power increase, when needed, in the gas turbine system.

REFERENCES:
patent: 3220191 (1965-11-01), Berchtold
patent: 3377800 (1968-04-01), Spillmann
patent: 3512358 (1970-05-01), Schmidt
patent: 3699681 (1972-10-01), Frutschi
patent: 3867811 (1975-02-01), Waeselynck

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