Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method

A method for the combustion of hydrogen-rich, gaseous fuels in combustion air in a burner of a gas turbine includes injecting the hydrogen-rich, gaseous fuel at least partially isokinetically with respect to the combustion air such that the partially hydrogen-rich, gaseous fuel is injected at least...

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Bibliographische Detailangaben
Hauptverfasser: CARRONI RICHARD, BERNERO STEFANO, LACHAUX THIERRY, BIAGIOLI FERNANDO
Format: Patent
Sprache:eng
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Zusammenfassung:A method for the combustion of hydrogen-rich, gaseous fuels in combustion air in a burner of a gas turbine includes injecting the hydrogen-rich, gaseous fuel at least partially isokinetically with respect to the combustion air such that the partially hydrogen-rich, gaseous fuel is injected at least partially in the same direction and at least partially at the same velocity as the combustion air.