Method for controlling an injection process of a magnetic injector
US-2015377173-A1 · Dec 31, 2015 · US
US9404456B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9404456-B2 |
| Application number | US-201313737645-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 9, 2013 |
| Priority date | Jan 11, 2012 |
| Publication date | Aug 2, 2016 |
| Grant date | Aug 2, 2016 |
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One passage for swirling is formed in an orifice plate fixed on a nozzle body. Two swirl chambers in which fuel is caused to swirl so that the fuel has swirling force are provided at an end of the one passage for swirling on the downstream side of the flow direction of fuel. Therefore, the collision between the swirling flow in the swirl chamber and the fuel flowing in the passage for swirling is mitigated, and the swirling flow can be smoothly produced to promote pulverization of sprays injected from fuel injection ports.
Opening claim text (preview).
The invention claimed is: 1. A fuel injection valve comprising: a slidable valve element; a valve seat member having a valve seat formed thereon and an opening at a downstream side, the slidable valve element being seated on the valve seat at a time of valve closing; a passage for swirling provided at each of two opposite downstream sides of a central hole, the passage for swirling communicating with the opening of the valve seat member; at least one swirl chamber formed on a downstream side of the passage for swirling, an entirety of the at least one swirl chamber having a curved inner surface and causing fuel to swirl in an interior of the at least one swirl chamber so as to give swirling force to the fuel; and at least one fuel injection port having a cylindrical shape and being formed in a bottom portion of the at least one swirl chamber, the fuel being injected outside through the at least one fuel injection port, wherein the passage for swirling has two swirl chambers at a downstream end thereof, the two swirl chambers defining individual chambers, at least two immediately adjacent swirl chambers share a common starting end, the common starting end dividing one stream of fuel flowing from the passage for swirling into two separate streams of fuel such that only one of the two separate streams of fuel flows into each of the at least two immediately adjacent swirl chambers, and fuel in one of the at least two immediately adjacent swirl chambers flows in a clockwise direction, and fuel in another of the at least two immediately adjacent swirl chambers flows in a counter clockwise direction. 2. The fuel injection valve according to claim 1 , wherein the two swirl chambers have wall surfaces, the wall surfaces having first ends that are connected to the downstream end of the passage for swirling and that are positioned at a center in a width direction of the passage for swirling and that form a partition wall having a predetermined thickness. 3. The fuel injection valve according to claim 2 , wherein the first ends of the wall surfaces are positioned between outer wall surfaces of the at least one swirl chamber (a segment Y 1 ) on a side of the passage for swirling and centers of the at least one fuel injection port (a segment Y). 4. The fuel injection valve according to claim 2 , wherein the partition wall has a partially circular section. 5. The fuel injection valve according to claim 4 , wherein the two swirl chambers and the passage for swirling are formed in a configuration in which a relationship between Dw and Sw is represented by the formula: Sw>Dw wherein Dw is a distance from a first segment Y connecting centers of the swirl chambers to a fourth segment Y 1 connecting the wall surfaces of the two swirl chambers on the side of the passage for swirling, and Sw is a width of the passage for swirling. 6. The fuel injection valve according to claim 1 , wherein the at least one swirl chamber has a section of an involute curve or a spiral curve. 7. The fuel injection valve according to claim 1 , wherein each of the two swirl chambers has a respective fuel injection port. 8. The fuel injection valve according to claim 1 , wherein the divider portion is edge-shaped. 9. The fuel injection valve according to claim 1 , wherein the divider portion is a thickness forming portion. 10. The fuel injection valve according to claim 1 , wherein the starting end of each swirl chamber is joined together by a region having a convex shape. 11. A fuel injection valve comprising: a slidable valve element; a nozzle body having a valve seat formed at a first end thereof, the slidable valve element being seated on the valve seat at a time of valve closing; and an orifice plate fixed to a second end of the nozzle body, the orifice plate including at least one swirl chamber an entirety of which having a curved inner surface that gives swirling force and a passage for swirling, provided at each of two opposite downstream sides of a central hole, through which fuel is supplied to the at least one swirl chamber, wherein the passage for swirling has two swirl chambers at a downstream end thereof, the two swirl chambers defining individual chambers, at least two immediately adjacent swirl chambers share a common starting end, the common starting end dividing one stream of fuel flowing from the passage for swirling into two separate streams of fuel such that only one of the two separate streams of fuel flows into each of the at least two immediately adjacent swirl chambers, and fuel in one of the at least two immediately adjacent swirl chambers flows in a clockwise direction, and fuel in another of the at least two immediately adjacent swirl chambers flows in a counter clockwise direction. 12. The fuel injection valve according to claim 11 , wherein each of the two swirl chambers has a respective fuel injection port. 13. The fuel injection valve according to claim 11 , wherein the divider portion is edge-shaped. 14. The fuel injection valve according to claim 11 , wherein the divider portion is a thickness forming portion. 15. The fuel injection valve according to claim 11 , wherein the starting end of each swirl chamber is joined together by a region having a convex shape.
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Means to impart a whirling motion to fuel upstream or near discharging orifices · CPC title
using electromagnetic operating means · CPC title
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