Synthesis gas expander located immediately upstream of combustio

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39 12, F02C 1310

Patent

active

060619368

ABSTRACT:
The invention improves the reliability and efficiency of the burning of a synthesis gas as a fuel for a combustion turbine to produce power by incorporating a synthesis gas expander immediately upstream of the combustion turbine. Increased efficiency occurs from the additional power output from the expander and by a reduction or elimination of nitrogen compression from an air separation unit for the control of oxides of nitrogen.

REFERENCES:
patent: 2592749 (1952-04-01), Sedille et al.
patent: 4028883 (1977-06-01), Meyer-Kahrweg
patent: 4199933 (1980-04-01), Pfenninger
patent: 4733528 (1988-03-01), Pinto
patent: 5220781 (1993-06-01), Keller
patent: 5289676 (1994-03-01), Brown et al.
patent: 5715671 (1998-02-01), Griffiths

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