| 摘要 |
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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