System and method for improved engine cooling in conjunction wit

Power plants – Combustion products used as motive fluid

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Details

60 3975, 4151737, F02C 718, F02C 728

Patent

active

053117344

ABSTRACT:
A method and system for cooling a gas turbine engine in conjunction with an improved gas bearing face seal assembly. The gas turbine engine has a multi-stage compressor which discharges compressor discharge air for expansion by a combustor. A cavity which is aerodynamically linked to a turbine stage on its downstream end is formed by a metal structure the upstream end of which is connected to a seal which substantially inhibits the flow of compressor discharge air into the cavity. A conduit links an intermediate stage of the multi-stage compressor to the cavity for purposes of cooling the cavity and the turbine stage components located downstream of the cavity.

REFERENCES:
patent: 3383033 (1968-05-01), Moore
patent: 3989410 (1976-11-01), Ferrari
patent: 4265590 (1981-05-01), Davies
patent: 4318668 (1982-03-01), Chaplin et al.
patent: 4332133 (1982-06-01), Schwarz et al.
patent: 4351532 (1982-09-01), Laverty
patent: 4375891 (1983-03-01), Pask
patent: 4466239 (1984-08-01), Napoli et al.
patent: 4561246 (1985-12-01), Hovan
patent: 4653267 (1987-03-01), Brodell et al.
patent: 4815272 (1989-03-01), Laurello
patent: 4901520 (1990-02-01), Kozak

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