Method and apparatus for intercooling gas turbines

Power plants – Combustion products used as motive fluid

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60 3953, 60728, F02C 330, F02C 7143

Patent

active

056692170

ABSTRACT:
The invention relates to an intercooled gas turbine having at least two air compression stages, and at least one nozzle for supplying a liquid coolant to air travelling between the at least two air compression stages. The invention also relates to a method for intercooling a gas turbine having at least two compression stages in which a liquid coolant is supplied to air travelling between the at least two compression stages, whereby the liquid coolant cools the air.

REFERENCES:
patent: 2407165 (1946-09-01), Kreitner et al.
patent: 2432359 (1947-12-01), Streid
patent: 2549819 (1951-04-01), Kane
patent: 2678531 (1954-05-01), Miller
patent: 3877218 (1975-04-01), Nebgen
patent: 5353585 (1994-10-01), Munk

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