Internal combustion engine with shrouded injection valve and pre-combustion chamber system
View Patent ↗An engine is provided. In one embodiment, the engine includes a precombustion chamber having a body, a secondary combustion chamber disposed at least partially in the body, and a plurality of passages configured to place the precombustion chamber in fluid communication with a main combustion chamber.
1. A device, comprising:
a precombustion chamber, comprising:
a body having a central axis;
a secondary combustion chamber having an internal surface disposed at least partially in the body;
a first passage extending through the body into the secondary combustion chamber in a first inwardly angled direction offset from a center of the secondary combustion chamber to intake all of a first fluid only in one rotational direction about the center of the secondary combustion chamber to flow the first fluid along the internal surface in the one rotational direction; and
a second passage extending through the body into the secondary combustion chamber in a second inwardly angled direction offset from the center of the secondary combustion chamber to intake all of a second fluid only in the one rotational direction about the center of the secondary combustion chamber to flow the second fluid along the internal surface in the one rotational direction, wherein the one rotational direction of all of the first and second fluids is configured to induce a swirling flow only in the one rotational direction about the center of the secondary combustion chamber.
2. The device of claim 1 , wherein the second passage comprises:
a primary passage coupled to the secondary combustion chamber; and
a plurality of passages coupled to the primary passage, wherein the plurality of passages extend from the primary passage toward an external surface.
3. The device of claim 2 , wherein the primary passage is tangential to a curved internal surface of the internal surface of the secondary combustion chamber.
4. The device of claim 2 , wherein the plurality of passages comprises more than four passages.
5. The device of claim 2 , wherein the plurality of passages are angled away from one another.
6. The device of claim 1 , wherein the secondary combustion chamber generally defines a sphere.
7. The device of claim 1 , wherein the precombustion chamber comprises a spark plug centered along the central axis, and a tip of the spark plug is recessed from the internal surface of the secondary combustion chamber.
8. The device of claim 1 , comprising an engine having a main combustion chamber and the precombustion chamber.
9. The device of claim 8 , wherein the engine comprises a two-stroke engine.
10. The device of claim 8 , wherein the engine comprises:
a cylinder that is generally concentric about the central axis, wherein an interior of the cylinder generally defines the main combustion chamber;
a gas injection valve coupled to the cylinder, wherein the gas injection valve comprises a nozzle configured to project a jet of fuel most of the way across the main combustion chamber.
11. The device of claim 10 , wherein the gas injection valve is oriented at an angle between approximately 5 and 85 degrees relative to the central axis.
12. The device of claim 10 , wherein the precombustion chamber comprises a dome facing into the main combustion chamber, the second passage comprises a plurality of passages extending through the dome to the main combustion chamber, and the plurality of passages diverge from one another.
13. The device of claim 10 , wherein the precombustion chamber comprises a spark plug centered along the central axis, and the first and second inwardly angled directions of the respective first and second passages are tangential to at least one curved inner surface of the internal surface of the secondary combustion chamber.
14. The device of claim 1 , wherein the first and second inwardly angled directions of the respective first and second passages are oriented to induce the swirling flow only in the one rotational direction along at least one curved inner surface of the internal surface of the secondary combustion chamber.
15. The device of claim 14 , wherein the first and second inwardly angled directions of the respective first and second passages are tangential to the at least one curved inner surface of the internal surface of the secondary combustion chamber.
16. The device of claim 1 , wherein the first passage comprises a fuel passage, and the second passage comprises at least one outlet passage.
17. A device, comprising:
a precombustion chamber, comprising:
a body having a central axis; and
a secondary combustion chamber having an internal surface disposed at least partially in the body;
wherein the precombustion chamber is configured to receive all of a fuel flow inwardly into the secondary combustion chamber only in one rotational direction about a center of the secondary combustion chamber to flow the fuel flow along the internal surface in the one rotational direction, the precombustion chamber is configured to receive all of a fluid flow inwardly into the secondary combustion chamber only in the one rotational direction about the center of the secondary combustion chamber to flow the fluid flow along the internal surface in the one rotational direction, the one rotational direction of all of the fuel flow and all of the fluid flow is configured to induce a swirling flow only in the one rotational direction about the center of the secondary combustion chamber, and the precombustion chamber is configured to output a mixture of the fuel flow and the fluid flow.
18. The device of claim 17 , wherein the precombustion chamber comprises a fuel passage that is flush and tangential to at least one curved inner surface of the internal surface of the secondary combustion chamber, and the precombustion chamber comprises a fluid passage that is flush and tangential to the at least one curved inner surface of the internal surface of the secondary combustion chamber.
19. A device, comprising:
a precombustion chamber, comprising:
a body;
a secondary combustion chamber disposed at least partially in the body, wherein the secondary combustion chamber comprises an internal surface having at least one curved surface extending about a center of the secondary combustion chamber;
a fuel passage oriented tangential to the at least one curved surface, wherein the fuel passage is configured to inject all of a fuel flow only in one rotational direction about a center of the secondary combustion chamber to flow the fuel flow along the internal surface in the one rotational direction, and the one rotational direction of all of the fuel flow is configured to induce a swirling flow only in the one rotational direction about the center of the secondary combustion chamber; and
an outlet passage.
20. The device of claim 19 , wherein the outlet passage is oriented tangential to the at least one curved surface, the outlet passage is configured to receive all of a fluid flow into the secondary combustion chamber only in the one rotational direction about the center of the combustion chamber to flow the fluid flow along the internal surface in the one rotational direction, the one rotational direction of all of the fluid flow is configured to help induce the swirling flow only in the one rotational direction about the center of the secondary combustion chamber, the swirling flow is configured mix the fuel flow and the fluid flow to create a mixture, and the outlet passage is configured to output the mixture from the secondary combustion chamber to a main combustion chamber of an engine.
21. The device of claim 20 , wherein the fuel passage and the outlet passage are flush with the at least one curved surface.