FIELD: gas turbines.
SUBSTANCE: according to the invention, the hydrogen-containing fuel can be stably ignited using a gaseous fuel that does not contain hydrogen, and the dispersion of the hydrogen-containing fuel can be increased. The combustion device of the gas turbine plant includes a burner including: a starting fuel pipeline in which the starting fuel circulates; a first main fuel pipeline in which the main fuel circulates; a second main fuel pipe in which the main fuel circulates; a fuel mixer to which a starting fuel line and a first main fuel line are connected; an internal fuel injector to which the fuel mixer is connected; a plurality of external fuel injectors to which the second main fuel line is connected; a starting fuel control valve provided in the starting fuel line; a first fuel control valve provided in the first main fuel line; and a second fuel control valve provided in the second main fuel line.
EFFECT: fuel dispersion increased.
14 cl, 14 dwg
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Authors
Dates
2021-04-12—Published
2020-09-28—Filed