Multi-shaft reheat turbine mechanism for generating power
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United States of America Patent
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Nov 7, 2000
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N/A
app pub date -
Mar 4, 1998
filing date -
Mar 4, 1998
priority date (Note) -
Expired
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Abstract
A multi-shaft reheat turbine mechanism includes multiple turbines mounted on respective compressor shafts, and catalytic reactors feeding respective ones of the turbines. Fuel is introduced into a low pressure compressor, whereby there is no need to pressurize the fuel. The compressor side of the mechanism emits a compressed air/fuel flow, portions of which are combusted in respective ones of the catalytic reactors. The air/fuel flow traveling from the compressor side to the turbine side passes through a regenerator in heat exchanging relationship with exhaust gas from a low pressure turbine.
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