Gas turbine

Power plants – Combustion products used as motive fluid – With addition of steam and/or water

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Details

60728, F02C 700

Patent

active

046140832

ABSTRACT:
A gas turbine is disclosed, in which a portion of compressed air from a compressor of the turbine is cooled by water and the cooled compressed air is utilized for cooling a region at or about the turbine inlet, and in which the interior of a combustor chamber into which the compressed air from the compressor is introduced is divided by a partition wall into a combustor part and a transition piece part and air cooling pipes are provided through the partition wall, each air cooling pipe being provided with nozzles through which to jet water to positively and effectively cool the compressed air while it passes through the air cooling pipe.

REFERENCES:
patent: 2592060 (1952-04-01), Oulianoff
patent: 3280555 (1966-10-01), Charpentier et al.
patent: 3418810 (1968-12-01), Cresswell et al.
patent: 3657884 (1972-04-01), Hugoson
patent: 3842597 (1974-10-01), Ehrich
patent: 3949549 (1976-04-01), Holl
patent: 3978658 (1976-09-01), Forbes et al.
patent: 4195474 (1980-04-01), Bintz et al.
patent: 4338780 (1982-07-01), Sakamoto et al.

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