Balanced dual flow regenerator heat exchanger system and core dr

Details Balanced dual flow regenerator heat exchanger system and core dr Balanced dual flow regenerator heat exchanger system and core dr

1995-05-15

1996-12-24

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

With exhaust treatment

165 8, F02C 7105

Patent

active

055864309

ABSTRACT:
A gas turbine engine includes a gas generator having a compressor, a first turbine member, and a combustor member between the compressor and the first turbine member for increasing the temperature of the fluid medium to be worked upon by the engine. A second turbine is located adjacent to the gas generator and it extracts energy from the fluid medium to produce rotary power. A heat scavenging member is located adjacent to the gas generator for extracting heat from the fluid medium after flowing from said second turbine and for transferring the heat into the fluid medium exiting the compressor by passing the fluid medium at least two times through the scavenging member to heat the fluid medium before flowing into the combustor member.

REFERENCES:
patent: 2865611 (1958-12-01), Bentele
patent: 4121417 (1978-10-01), Koppenhofer et al.
patent: 4300349 (1981-11-01), Heckel
patent: 4491171 (1985-01-01), Zenkner

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