Multi-shaft reheat turbine mechanism for generating power

Power plants – Combustion products used as motive fluid

Patent

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Details

60 3917, 60 39512, F02C 106, F02G 1055

Patent

active

061419532

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.

REFERENCES:
patent: 2621475 (1952-12-01), Loy
patent: 2624172 (1953-01-01), Houdry
patent: 3747944 (1973-07-01), Roy et al.
patent: 3975900 (1976-08-01), Pfefferle
patent: 5347806 (1994-09-01), Nakhamkin
patent: 5386688 (1995-02-01), Nakhamkin

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