Integral aft frame mount for a gas turbine combustor transition

Power plants – Combustion products used as motive fluid – Combustion products generator

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F02C 100

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active

054149991

ABSTRACT:
A transition piece (110) for a gas turbine comprising a tubular body having an upstream end (112) and a downstream end (114), the downstream end (114) formed with an integral frame (116) surrounding an opening at the downstream end; and an aft mount connector 126) adapted to connect the transition piece (110) to a first stage nozzle of the gas turbine, the aft mount connector (126) formed integrally with the frame (116).

REFERENCES:
patent: 2547619 (1951-04-01), Buckland
patent: 2594808 (1952-04-01), Rubbra
patent: 2608057 (1952-08-01), Boyd et al.
patent: 3609968 (1972-10-01), Mierley, Sr. et al.
patent: 3657882 (1972-04-01), Hugoson
patent: 3759038 (1973-09-01), Scalzo et al.
patent: 4191011 (1980-03-01), Sweeny et al.
patent: 4195474 (1980-04-01), Bintz et al.
patent: 4232527 (1980-11-01), Reider
patent: 4297843 (1981-11-01), Sato et al.
patent: 4422288 (1983-12-01), Steber
patent: 5190245 (1993-03-01), Debeneix
patent: 5265412 (1993-11-01), Bagepalli

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