초록 ▼

An internal combustion engine including a pilot subchamber, a pilot fuel injector having a tip in communication with the pilot subchamber, an ignition element positioned to ignite fuel within the pilot subchamber, and a main fuel injector spaced apart from the pilot fuel injector. The engine include

An internal combustion engine including a pilot subchamber, a pilot fuel injector having a tip in communication with the pilot subchamber, an ignition element positioned to ignite fuel within the pilot subchamber, and a main fuel injector spaced apart from the pilot fuel injector. The engine includes a common rail in fluid communication with the main fuel injector and with the pilot fuel injector and a pressure regulating mechanism in fluid communication with the common rail for regulating a fuel pressure therein. A method of combusting fuel in an internal combustion engine is also provided.

대표청구항 ▼

1. A method of combusting fuel in an internal combustion engine having a rotatable body defining at least one combustion chamber, the method comprising: pressurizing the fuel in a common rail;feeding a pilot injector with the common rail to inject fuel in a pilot subchamber;igniting the fuel within

1. A method of combusting fuel in an internal combustion engine having a rotatable body defining at least one combustion chamber, the method comprising: pressurizing the fuel in a common rail;feeding a pilot injector with the common rail to inject fuel in a pilot subchamber;igniting the fuel within the pilot subchamber;circulating the ignited fuel out of the pilot subchamber and into one of the at least one combustion chamber; andfeeding a main injector separate from the pilot injector with the common rail to inject fuel into the one of at least one combustion chamber spaced apart from the pilot subchamber and the pilot injector. 2. The method as defined in claim 1, wherein the internal combustion engine further comprises at least one additional rotatable body each defining at least one combustion chamber, the method further comprising, for each additional rotatable body: feeding a respective additional pilot injector with the common rail to inject fuel in a respective additional pilot subchamber;igniting the fuel within the respective additional pilot subchamber;circulating the ignited fuel out of the respective additional pilot subchamber and into one of the at least one combustion chamber defined by the additional rotatable body; andfeeding a respective additional main injector separate from the respective additional pilot injector with the common rail to inject fuel into the one of at least one combustion chamber defined by the additional rotatable body spaced apart from the respective additional pilot subchamber and the respective additional pilot injector. 3. The method as defined in claim 1, wherein the fuel is heavy fuel. 4. The method as defined in claim 1, wherein pressurizing the fuel in the common rail includes regulating a fuel pressure in the common rail with an engine control unit. 5. The method as defined in claim 1, wherein injecting the fuel in the pilot subchamber and injecting the fuel into the one of at least one combustion chamber are performed at a same fuel pressure. 6. An internal combustion engine comprising: an outer body defining an internal cavity;a rotatable body sealingly and rotationally received within the internal cavity to define at least one combustion chamber of variable volume;a pilot subchamber defined in the outer body in communication with the internal cavity;a pilot fuel injector having a tip in communication with the pilot subchamber;an igniter positioned to ignite fuel within the pilot subchamber;a main fuel injector spaced apart from the pilot fuel injector and having a tip in communication with the internal cavity at a location spaced apart from the pilot subchamber;a common rail in fluid communication with the main fuel injector and with the pilot fuel injector; anda metering or pressure regulating valve in fluid communication with the common rail for regulating a fuel pressure therein. 7. The engine as defined in claim 6, wherein the metering or pressure regulating valve is provided at least in part in a pump in fluid communication with a fuel source and with an inlet of the common rail. 8. The engine as defined in claim 7, wherein a fuel outlet of the common rail is in selective fluid communication with the fuel source through the metering or pressure regulating valve. 9. The engine as defined in claim 8, wherein the valve is actuable by an engine control unit. 10. The engine as defined in claim 6, wherein the internal cavity is defined by two axially spaced apart end walls and a peripheral wall extending between the end walls, and the rotatable body is a rotor body rotatable within the internal cavity in sealing engagement with the peripheral and end walls. 11. The engine as defined in claim 10, wherein the internal cavity defines an epitrochoid shape with two lobes, the rotor body has three circumferentially spaced apex portions, and the at least one combustion chamber include three rotating chambers of variable volume, the rotor body being engaged to an eccentric portion of a shaft to rotate and perform orbital revolutions within the cavity with each of the apex portions remaining in sealing engagement with the peripheral wall and separating the chambers. 12. The engine as defined in claim 6, wherein the pilot injector and the main injector have tip openings through which the fuel is injected, and an open area defined by the tip openings of the pilot injector is smaller than that defined by the tip openings of the main injector. 13. The engine as defined in claim 6, wherein the engine includes at least one additional rotatable body sealingly and rotationally received within a respective additional internal cavity of the outer body to define at least one combustion chamber of variable volume, and further including, for each additional rotatable body, a respective additional pilot subchamber defined in the outer body in communication with the respective additional internal cavity, an additional pilot fuel injector having a tip in communication with the respective additional pilot subchamber, an additional igniter positioned to ignite fuel within the respective additional pilot subchamber, and an additional main fuel injector having a tip in communication with the respective additional internal cavity at a location spaced apart from the respective additional pilot subchamber, the common rail also being in fluid communication with the additional main fuel injector and with the additional pilot fuel injector of each additional rotatable body. 14. A rotary internal combustion engine comprising: an outer body having an internal cavity defined by two axially spaced apart end walls and a peripheral wall extending between the end walls;a rotor body rotatable within the internal cavity in sealing engagement with the peripheral and end walls and defining at least one chamber of variable volume in the internal cavity around the rotor body;a pilot subchamber defined in the outer body in fluid communication with the internal cavity;a pilot fuel injector having a tip in communication with the pilot subchamber;an igniter positioned to ignite fuel within the pilot subchamber;a main fuel injector spaced apart from the pilot fuel injector, the main fuel injector having a tip in communication with the internal cavity at a location spaced apart from the pilot subchamber;a common rail in fluid communication with the main fuel injector and with the pilot fuel injector; anda metering or pressure regulating valve in fluid communication with the common rail for regulating a fuel pressure therein. 15. The engine as defined in claim 14, wherein the internal cavity defines an epitrochoid shape with two lobes, the rotor body has three circumferentially spaced apex portions, and the at least one combustion chamber include three rotating chambers of variable volume, the rotor body being engaged to an eccentric portion of a shaft to rotate and perform orbital revolutions within the cavity with each of the apex portions remaining in sealing engagement with the peripheral wall and separating the chambers. 16. The engine as defined in claim 14, wherein the metering or pressure regulating valve is provided at least in part in a pump in fluid communication with a fuel source and with an inlet of the common rail. 17. The engine as defined in claim 16, wherein a fuel outlet of the common rail is in selective fluid communication with the fuel source through the metering or pressure regulating valve. 18. The engine as defined in claim 17, wherein the valve is actuable by an engine control unit. 19. The engine as defined in claim 14, wherein the pilot injector and the main injector have tip openings through which the fuel is injected, and an open area defined by the tip openings of the pilot injector is smaller than that defined by the tip openings of the main injector. 20. The engine as defined in claim 14, wherein the engine includes at least one additional rotor body engaged to a same shaft as the rotor body, the additional rotor body being in sealing engagement with peripheral and end walls of a respective additional internal cavity of the outer body to define at least one combustion chamber of variable volume, and further including, for each additional rotor body, a respective additional pilot subchamber defined in the outer body in communication with the respective additional internal cavity, an additional pilot fuel injector having a tip in communication with the respective additional pilot subchamber, an additional igniter positioned to ignite the fuel within the respective additional pilot subchamber, and an additional main fuel injector spaced apart from the additional pilot fuel injector and having a tip in communication with the respective additional cavity at a location spaced apart from the respective pilot subchamber, the common rail also being in fluid communication with the additional main fuel injector and with the additional pilot fuel injector of each additional rotor body.