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 fuel system of an aircraft engine, comprising:
a combustor;
a liquid fuel circuit selectively fluidly connected to the combustor via a liquid fuel manifold;
a gaseous fuel circuit selectively fluidly connected to the combustor via a gaseous fuel manifold;
an inert gas source selectively fluidly connected to the gaseous fuel manifold; and
a controller configured to, during a shutdown of the aircraft engine, cause inert gas from the inert gas source to be issued to the gaseous fuel manifold while gaseous fuel is issued to the gaseous fuel manifold to cause mixing of the inert gas with the gaseous fuel;
wherein:
the gaseous fuel manifold fluidly communicates a gaseous fuel supply with at least one dual fuel nozzle downstream of the gaseous fuel manifold;
the fuel system further comprises a purge gas circuit in fluid communication with the inert gas source and the gaseous fuel manifold such that the gaseous fuel circuit and the purge gas circuit share a common outlet of the gaseous fuel manifold;
the liquid fuel circuit fluidly communicates a liquid fuel supply with the at least one dual fuel nozzle downstream of the liquid fuel supply;
the purge gas circuit is in fluid communication with the liquid fuel manifold such that the liquid fuel circuit and the purge gas circuit share a common outlet of the liquid fuel manifold; and
the purge gas circuit includes at least one three-way valve configured to issue the inert gas to the gaseous fuel manifold and the liquid fuel manifold simultaneously.
2. The system of claim 1 , wherein the at least one three-way valve is configured to issue the inert gas to either the gaseous fuel manifold or the liquid fuel manifold.
3. The system of claim 1 , wherein the controller is operatively connected to the purge gas circuit and configured to control a flow of the inert gas through the purge gas circuit.
4. The system of claim 3 , wherein the controller is configured to issue the flow of the inert gas through the purge gas circuit to at least one of the gaseous fuel manifold or the liquid fuel manifold.
5. The fuel system of claim 1 , wherein the controller configured to, during a startup of the aircraft engine:
cause the inert gas to be issued to the gaseous fuel manifold before the gaseous fuel is issued to the gaseous fuel manifold; and
once a pressure of the inert gas inside of the gaseous fuel manifold has reached a predetermined pressure, cause the inert gas to cease being issued to the gaseous fuel manifold and cause the gaseous fuel to be issued to the gaseous fuel manifold.
6. A fuel system, comprising:
a combustor;
a liquid fuel circuit selectively fluidly connected to the combustor via a liquid fuel manifold;
a gaseous fuel circuit selectively fluidly connected to the combustor via a gaseous fuel manifold, the gaseous fuel manifold fluidly communicating a gaseous fuel supply with at least one dual fuel nozzle downstream of the gaseous fuel manifold;
a gas source selectively fluidly connected to the gaseous fuel manifold; and
a purge gas circuit in fluid communication with the gas source and the gaseous fuel manifold such that the gaseous fuel circuit and the purge gas circuit share a common outlet of the gaseous fuel manifold, wherein:
the liquid fuel circuit fluidly communicates a liquid fuel supply with the at least one dual fuel nozzle downstream of the liquid fuel supply;
the purge gas circuit is in fluid communication with the liquid fuel manifold such that the liquid fuel circuit and the purge gas circuit share a common outlet of the liquid fuel manifold; and
the purge gas circuit includes at least one three way valve configured to issue a purge gas to the gaseous fuel manifold and the liquid fuel manifold simultaneously.