Multi-fuel engine for an aircraft
A method is provided for operating an aircraft system. During this method, an engine is operated using first fuel provided by a first fuel source. A fuel supply for the engine is switched between the first fuel source and a second fuel source, where the switching of the fuel supply includes shutting down the engine during aircraft flight. The engine is operated using second fuel provided by the second fuel source.
1. A method for operating an aircraft system, comprising:
operating an engine using first fuel provided by a first fuel source;
switching a fuel supply for the engine between the first fuel source and a second fuel source, the switching of the fuel supply comprising shutting down the engine during aircraft flight such that a flame in an annular combustion chamber of the engine is extinguished, and the switching of the fuel supply further comprising
operating a first flow regulator to stop flow of the first fuel from the first fuel source prior to the flame being extinguished; and
operating a second flow regulator to start flow of the second fuel from the second fuel source after the flame being extinguished; and
operating the engine using second fuel provided by the second fuel source.
2. The method of claim 1 , wherein the engine is part of an aircraft propulsion system.
3. The method of claim 1 , further comprising operating a second engine, the switching of the fuel supply for the engine performed while the second engine is operating.
4. The method of claim 1 , wherein the switching of the fuel supply further comprises igniting the second fuel within a combustor of the engine.
5. The method of claim 1 , wherein the switching of the fuel supply further comprises purging the first fuel from one or more components of the engine using a purge fluid that is different than the second fuel.
6. The method of claim 5 , wherein the purge fluid comprises inert gas.
7. The method of claim 1 , wherein
one of the first fuel or the second fuel comprises gaseous fuel; and
the other of the first fuel or the second fuel comprises liquid fuel.
8. The method of claim 1 , wherein
one of the first fuel or the second fuel comprises non-hydrocarbon fuel; and
the other of the first fuel or the second fuel comprises hydrocarbon fuel.
9. The method of claim 1 , wherein the first fuel or the second fuel comprises hydrogen fuel.
10. The method of claim 1 , wherein the switching of the fuel supply is initiated by an operator.
11. The method of claim 1 , wherein the switching of the fuel supply is initiated by a controller.
12. The method of claim 1 , wherein the switching of the fuel supply comprises
restarting the engine concurrently using the first fuel and the second fuel; and
stopping flow of the first fuel following the restarting of the engine.
13. The method of claim 1 , wherein
a first fuel injector receives the first fuel from the first fuel source, and the first fuel injector directs the first fuel into the annular combustion chamber for combustion during the operating of the engine using the first fuel;
a second fuel injector receives the second fuel from the second fuel source, and the second fuel injector directs the second fuel into the annular combustion chamber for combustion during the operating of the engine using the second fuel; and
the first fuel injector is dedicated to the first fuel source, and the second fuel injector is dedicated to the second fuel source.
14. The method of claim 3 , further comprising:
operating the second engine using the first fuel while the fuel supply for the engine is switched between the first fuel source and the second fuel source; and
switching the second engine from the first fuel to the second fuel, wherein the engine is operated using the second fuel during the switching of the second engine from the first fuel to the second fuel.
15. A method for operating an aircraft system, comprising:
operating a first engine;
operating a second engine using first fuel provided by a first fuel source;
switching a fuel supply for the second engine between the first fuel source and a second fuel source while the first engine is operating, wherein a flame within an annular combustion chamber of the second engine is extinguished during the switching of the fuel supply,
during the switching of the fuel supply, controlling a flow of the first fuel from the first fuel source such that the first fuel is stopped prior to the flame being extinguished, and controlling a flow of the second fuel from the second fuel source such that the second fuel is started after the flame being extinguished; and
operating the second engine using second fuel provided by the second fuel source.
16. The method of claim 15 , wherein the switching of the fuel supply for the second engine is performed while the first engine is operating using the first fuel.
17. The method of claim 15 , wherein the switching of the fuel supply for the second engine comprises shutting down the second engine during aircraft flight.
18. A method for operating an aircraft system, comprising:
operating a first engine using first fuel;
operating a second engine using the first fuel;
switching operation of the first engine from using the first fuel to second fuel, wherein a flame within a combustion chamber of the first engine is extinguished during the switching of the operation of the first engine, and wherein the second engine continues to operate using the first fuel during the switching of the operation of the first engine; and
switching operation of the second engine from using the first fuel to the second fuel following the switching of the operation of the first engine, wherein a flame within a combustion chamber of the second engine is extinguished during the switching of the operation of the second engine, and wherein the first engine continues to operate using the second fuel during the switching of the operation of the second engine
wherein during the switching of the fuel supply of the first engine or the second engine, controlling a flow of the first fuel from a first fuel source such that the first fuel is stopped prior to the flame being extinguished, and controlling a flow of the second fuel from a second fuel source such that the second fuel is started after the flame being extinguished.
19. The method of claim 18 , wherein
the combustion chamber of the first engine is an annular combustion chamber; and
the combustion chamber of the second engine is an annular combustion chamber.
20. The method of claim 18 , wherein at least one of during the switching of the operation of the first engine from using the first fuel to the second fuel, the flow of the second fuel to the first engine is started after the flow of the first fuel to the first engine is terminated; or during the switching of the operation of the second engine from using the first fuel to the second fuel, the flow of the second fuel to the second engine is started after the flow of the first fuel to the second engine is terminated.