Fuel systems and methods for purging
A fuel system can include a first fuel circuit, a second fuel circuit, and an inert gas purge system operatively connected to both the first fuel circuit and the second fuel circuit to purge at least a portion of either or both of the first and/or second fuel circuit. The first fuel can be a liquid fuel and the second fuel can be a gaseous fuel. The first fuel circuit can include a first fuel manifold configured to fluidly communicate a first fuel supply with at least one dual fuel nozzles downstream of the first fuel manifold.
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.
2. The method of claim 1 , further comprising reducing a gaseous fuel pressure to a predetermined threshold pressure at or greater than a combustor pressure, before purging.
3. The method of claim 2 , further comprising shutting off a flow of the gaseous fuel before purging.
4. The method of claim 1 , wherein purging includes issuing the inert gas while issuing the gaseous fuel to the dual-fuel nozzle.
5. The method of claim 4 , wherein issuing the inert gas includes mixing the inert gas with the gaseous fuel within a manifold.
6. The method of claim 1 , comprising purging the liquid fuel circuit of the dual-fuel aircraft engine with the inert gas.
7. The method of claim 1 , comprising:
purging the gaseous fuel circuit of the dual-fuel aircraft engine with the inert gas during shutdown of the aircraft engine; and
once a flameout in the combustor has been detected, ceasing to purge the gaseous fuel circuit.
8. The method of claim 1 , comprising purging the gaseous fuel circuit of the dual-fuel aircraft engine with the inert gas during shutdown of the aircraft engine by maintaining a higher pressure in the gaseous fuel circuit than in the combustor.
9. The method of claim 1 , comprising purging the gaseous fuel circuit of the dual-fuel aircraft engine with the inert gas during shutdown of the aircraft engine by progressively increasing an amount of the inert gas with the gaseous fuel until a flameout, and then ceasing to purge the gaseous fuel circuit after the flameout.