FIELD: engines and pumps.
SUBSTANCE: ammonia and fuel with ignitability higher than that of ammonia can be supplied as fuel to gas turbine engine. In working zone of worse ignitability, in which ammonia ignitability deteriorates in comparison to the time of normal operation of gas turbine engine, fuel fraction with ignitability higher than that of ammonia in fuel that is supplied to gas turbine engine is increased in comparison to the time of normal operation.
EFFECT: even at use of poor inflammable ammonia as main fuel there can be provided stable start up, operation and shutdown of gas turbine at reduced carbon dioxide emissions.
16 cl, 6 dwg
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