Gas turbine combined cycle system

Details Gas turbine combined cycle system Gas turbine combined cycle system

F - Mech Eng,Light,Heat,Weapons

02

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F02G 5/00 (2006.01) F01D 25/30 (2006.01) F02C 6/18 (2006.01) F22B 1/18 (2006.01)

Patent

CA 2134738

ABSTRACT OF THE DISCLOSURE 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.

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