Gas turbine combined cycle system

Power plants – Combustion products used as motive fluid

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Details

60 39182, 122 7R, F02C 618, F02C 700

Patent

active

054675910

ABSTRACT:
An improved gas turbine combined cycle system having a diffuser duct between the gas turbine and steam generator. The diffuser duct has boundary layer suction to prevent gas jet separation, thereby reducing pressure loss and improving gas velocity profiles in the duct, while eliminating the need for internal flow controls. The gas turbine combined cycle system can be vertically oriented to reduce the plan area of the system and provide for convenient use of a symmetrical diffuser duct and the use of forced circulation on the water side of the steam generator.

REFERENCES:
patent: 2926493 (1960-03-01), Poole et al.
patent: 3442324 (1969-05-01), Clay et al.
patent: 3561405 (1971-02-01), Tramuta
Chang, Paul K. Control of Flow Separation McGraw-Hill, New York, 1976. pp. 6-7.

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