Optimized fuel management system for direct injection ethanol enhancement of gasoline engines
US-2015369117-A1 · Dec 24, 2015 · US
US10077750B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10077750-B2 |
| Application number | US-201715411256-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 20, 2017 |
| Priority date | Jan 20, 2016 |
| Publication date | Sep 18, 2018 |
| Grant date | Sep 18, 2018 |
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Systems and methods are provided for operation of fuel injectors within an applied-ignition, direct-injection internal combustion engine. In one example, a needle of a fuel injector is moved from a retracted position to an extended position relative to a plurality of injection holes of a nozzle of the fuel injector, with at least one injection hole being separated from a fuel supply system earlier than each other injection hole. In a partially retracted position, fuel flow along a first side of the needle is decreased relative to fuel flow along a second side of the needle.
Opening claim text (preview).
The invention claimed is: 1. A method for operating an applied-ignition, direct-injection internal combustion engine having at least one cylinder, in which each cylinder is, for the direct introduction of fuel into the cylinder, equipped with an injection device which has a moveable closure body, the method comprising: connecting at least two openings provided in a housing of the injection device to a fuel supply system by moving the moveable closure body from a rest position in which the at least two openings are separated from the fuel supply system to a working position connecting the at least two openings to the fuel supply system; and proceeding from the working position in which the at least two openings are connected to the fuel supply system, moving the closure body from the working position into the rest position, with the at least two openings of the injection device being separated from the fuel supply system in succession with a time offset in such a way that at least one opening of the at least two openings is already fully separated from the fuel supply system while at least one other opening of the at least two openings is still connected to the fuel supply system, the opening fully separated from the fuel supply system later in time having a greater angle relative to a direction of gravity than another opening. 2. A fuel injector comprising: a housing including a nozzle tip and a seating surface formed within the nozzle tip; a plurality of injection holes formed by the nozzle tip; and a needle housed within the housing, the needle moveable to a first extended position and a first retracted position, the first extended position in which the needle directly contacts the seating surface at a first side of the housing and does not directly contact the seating surface at a second side of the housing and the first retracted position in which the needle does not contact the seating surface. 3. The fuel injector of claim 2 , wherein the needle is moveable to a second extended position in which the needle directly contacts the seating surface at both the first side and the second side of the housing, and wherein the first extended position is between the second extended position and the first retracted position. 4. The fuel injector of claim 3 , wherein the needle is moveable in a direction of a central axis of the fuel injector between each of the first retracted position, the first extended position, and the second extended position. 5. The fuel injector of claim 3 , wherein the needle is moveable in an arcing direction relative to a central axis of the fuel injector between the first extended position and the second extended position. 6. The fuel injector of claim 5 , wherein the needle is moveable in a direction of the central axis between the first extended position and the first retracted position. 7. The fuel injector of claim 2 , wherein the plurality of injection holes includes a first injection hole positioned toward the first side and a second injection hole positioned toward the second side, and wherein a fuel flow from the first injection hole is less than a fuel flow from the second injection hole with the needle in the first extended position. 8. The fuel injector of claim 2 , wherein the plurality of holes is positioned at a distal end of the nozzle tip downstream of the seating surface, and wherein the seating surface at the first side of the housing extends further away from the plurality of holes than the seating surface at the second side of the housing. 9. A fuel injector comprising: a body forming a nozzle tip; a fuel passage positioned within the body, the fuel passage fluidly coupled to a plurality of injection holes formed at the nozzle tip; and a needle moveable within an interior of the body and upstream of the plurality of injection holes, a first position of the needle including an end shaped to press against an inner surface of the body to allow fuel to flow along the inner surface at a first side of the needle and to not allow fuel to flow along the inner surface at a second side of the needle, a second position of the needle allowing fuel to flow along the inner surface of the first and second sides, the fuel flow in the first position being greater in a first injection hole than a second injection hole. 10. The fuel injector of claim 9 , wherein the end of the needle has an approximately spherical shape. 11. The fuel injector of claim 9 , wherein the inner surface of the body includes a first protrusion shaped to directly contact the end of the needle at the second side. 12. The fuel injector of claim 11 , wherein the first protrusion extends away from the nozzle tip in a direction of a central axis of the fuel injector. 13. The fuel injector of claim 11 , wherein the first protrusion does not directly contact the end of the needle at the first side. 14. The fuel injector of claim 11 , wherein the first protrusion is one of a plurality of protrusions, and wherein each protrusion of the plurality of protrusions extends away from the nozzle tip in a direction of a central axis of the fuel injector. 15. The fuel injector of claim 14 , wherein each protrusion of the plurality of protrusions extends inward toward the central axis by a same amount. 16. The fuel injector of claim 14 , wherein the first protrusion extends away from the nozzle tip by a greater amount than each other protrusion of the plurality of protrusions. 17. The fuel injector of claim 16 , wherein the plurality of protrusions is positioned upstream of the plurality of injection holes, and wherein the end of the needle presses against a sealing line positioned upstream of the plurality of injection holes and downstream of the plurality of protrusions. 18. The fuel injector of claim 17 , wherein the sealing line is formed by the inner surface, and wherein a midpoint of the sealing line is offset a distance from a central axis of the needle.
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