| CPC F02C 9/40 (2013.01) [F02C 3/22 (2013.01); F02C 3/24 (2013.01); F23K 5/18 (2013.01); F23R 3/36 (2013.01); F02C 7/222 (2013.01); F02C 7/232 (2013.01); F05D 2260/602 (2013.01); F23D 2209/30 (2013.01)] | 9 Claims |

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1. A method of operating a dual-fuel aircraft engine, the method comprising:
feeding a liquid fuel to a combustor of the aircraft engine via a liquid fuel circuit including a dual-fuel nozzle;
feeding a gaseous fuel to the combustor of the aircraft engine via a gaseous fuel circuit including the dual-fuel nozzle;
purging the gaseous fuel circuit of the dual-fuel aircraft engine with an inert gas during shutdown of the aircraft engine to prevent flashback; and
purging the gaseous fuel circuit and the liquid fuel circuit simultaneously with the inert gas.
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