Method for operating a gas turbine group with catalytic gas gene

Details Method for operating a gas turbine group with catalytic gas gene Method for operating a gas turbine group with catalytic gas gene

1997-12-03

1999-08-17

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

60 3912, 60723, F02C 320

Patent

active

059376325

ABSTRACT:
In the case of a method for operating a gas turbine group, the gas turbine group essentially consists of a compressor (1), a combustion chamber (5), a turbine (2) and a generator (3). Fuel is mixed in a premixer (18) of the combustion chamber (5), prior to the combustion, with air compressed in the compressor (1), and subsequently burned in a combustion space (19).
Compressed air, fed via an air line element (15) , is mixed with fuel fed via a fuel line element (16) and delivered to a reactor (10) having a catalytic coating. The air/fuel mixture is converted in the reactor (10) into a synthesis gas comprising hydrogen, carbon monoxide, residual air and residual fuel and this synthesis gas is injected into the zones of the combustion chamber (5) where the flame is stabilized.

REFERENCES:
patent: 2655786 (1953-10-01), Carr
patent: 3167913 (1965-02-01), Muhlberg et al.
patent: 5048284 (1991-09-01), Lywood et al.
patent: 5729967 (1998-03-01), Joos et al.

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