Cooling arrangement for a gas turbine driven power system

Details Cooling arrangement for a gas turbine driven power system Cooling arrangement for a gas turbine driven power system

1998-09-22

2000-10-24

Freay, Charles G.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3983, F02G 100

Patent

active

061348783

ABSTRACT:
A gas turbine driven power system includes a shell having an air inlet and an exhaust outlet. Mufflers are provided at the air inlet and the exhaust outlet, respectively. A gas turbine as a power source is provided in the shell and includes an inlet port and an outlet port. A heat exchanger is further provided in the shell in an air-passing space free of barrier formed between the muffler at the air inlet and the inlet port of the gas turbine. It is so arranged that all the air introduced into the shell through the air inlet passes through the heat exchanger for heat exchange with heat generated inside the shell.

REFERENCES:
patent: 3791682 (1974-02-01), Mitchell
patent: 4002023 (1977-01-01), Hartmann
patent: 4382359 (1983-05-01), Sampayo
patent: 4864812 (1989-09-01), Rodgers et al.
patent: 5649418 (1997-07-01), Ludwig

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