Gas turbine

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 7/10 (2006.01) F01K 21/04 (2006.01) F02C 3/34 (2006.01) F02C 7/08 (2006.01) F02C 7/143 (2006.01)

Patent

CA 2037205

ABSTRACT A gas turbine operating on a regenerative gas turbine cycle includes a compressor having liquid feed means for feeding water into air compressed during compression and intercooling means for cooling compressed air between compression stages. A heat exchanger provides for heating of compressed air by hot exhaust gases from the power generating turbine of the gas turbine, before the compressed air is fed into a combustion chamber where it is mixed with fuel and the fuel is combusted for generating pressure/heat energy for driving the power generating turbine. The intercooling of air compressed in the compressor together with air cooling as a result of water vaporization and simultaneous vapour loading of the air, and the employment of hot exhaust gases for heating compressed air, result in a gas turbine cycle that can provide a gas turbine having a high thermal efficiency. .

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