Method of cooling the coolant of a gas turbine, and apparatus pe

Power plants – Combustion products used as motive fluid

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60 39182, 60728, F02C 600

Patent

active

058732349

ABSTRACT:
Adequate cooling of the coolant of a gas turbine of a gas and steam turbine system is assured under all operating conditions, and especially in peak-load operation. The coolant of the gas turbine is cooled by heat exchange with a medium circulating in a separate evaporator loop connected to the steam drum. The cooling capacity is adapted to the operating state of the gas and steam turbine system. An injector connection is provided between a feedwater delivery pipe and the separate evaporator loop.

REFERENCES:
patent: 3686867 (1972-08-01), Hull
patent: 4445325 (1984-05-01), Tratz
patent: 5285627 (1994-02-01), Losel et al.
patent: 5404708 (1995-04-01), Sigling et al.
patent: 5491971 (1996-02-01), Tomlinson et al.

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