Gas turbine combustor transition

Details Gas turbine combustor transition Gas turbine combustor transition

1997-02-21

1999-05-25

Freay, Charles G.

Power plants

Combustion products used as motive fluid

60752, 60 3937, F02G 300

Patent

active

059060930

ABSTRACT:
A method of converting a steam cooled transition to an air cooled transition in a gas turbine having a compressor in fluid communication with a combustor, a turbine section in fluid communication with the combustor, the transition disposed in a combustor shell and having a cooling circuit connecting a steam outlet and a steam inlet and wherein hot gas flows from the combustor through the transition and to the turbine section, includes forming an air outlet in the transition in fluid communication with the cooling circuit and providing for an air inlet in the transition in fluid communication with the cooling circuit.

REFERENCES:
patent: 4719748 (1988-01-01), Davis, Jr. et al.
patent: 5027604 (1991-07-01), Krueger
patent: 5226278 (1993-07-01), Meylan et al.
patent: 5237813 (1993-08-01), Harris et al.
patent: 5351474 (1994-10-01), Slocum et al.
patent: 5685158 (1997-11-01), Lenahan et al.

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