Low NOX combustor for a gas turbine
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United States of America Patent
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-
Aug 31, 2004
Grant Date -
Nov 20, 2003
app pub date -
May 2, 2003
filing date -
May 20, 2002
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A combustion system for a gas turbine includes a steam reformer and a combustor connected in series. A portion of the incoming fuel is diverted to the steam reformer, the balance passing directly to the combustor. The effluent from the steam reformer, which effluent includes a significant amount of hydrogen, is combined with the unreformed fuel entering the combustor. The result is a hot combustion gas which contains very little NOx.
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