PRE-CHAMBER FOR AN INTERNAL COMBUSTION ENGINE AND COMBUSTION ENGINE

Abstract

A pre-chamber component for an internal combustion engine includes a chamber for accommodating an air-fuel-mixture to be ignited, wherein the pre-chamber component includes a first opening into the chamber for arranging an ignition device, in particular a spark plug, and a second opening for introducing the air-fuel-mixture in the form of a mixture flow into the chamber. The pre-chamber component includes a mixture flow guiding device, which is shaped such that the mixture flow of the air-fuel-mixture in the chamber is oriented substantially transversely with respect to a longitudinal axis from the second opening of the chamber to at least a part of the chamber adjacent to the first opening and/or in the form of a turbulent flow.

Claims

1. A system, comprising: a pre-chamber component configured to couple to an internal combustion engine, comprising: a chamber configured to receive an air-fuel-mixture; a first opening into the chamber, wherein the first opening is configured to receive an ignition device to ignite the air-fuel mixture; a second opening into the chamber, wherein the second opening is configured to introduce the air-fuel-mixture as a mixture flow into the chamber; a mixture flow guiding device shaped such that the mixture flow of the air-fuel-mixture in the chamber is: oriented substantially transversely with respect to a longitudinal axis from the second opening of the chamber to at least a part of the chamber adjacent to the first opening; and/or in the form of a turbulent flow.

2. The system of claim 1, wherein the mixture flow guiding device comprises a first guiding wall substantially parallel to a surface of the chamber having the first opening.

3. The system of claim 2, wherein the mixture flow guiding device comprises a second guiding wall substantially aligned in parallel with the longitudinal axis.

4. The system of claim 3, wherein the mixture flow guiding device comprises a flow break-away edge configured to create the turbulent mixture flow.

5. The system of claim 4, wherein the first guiding wall and/or the flow break-away edge is disposed on a peripheral wall of the chamber or at a greater distance from the first opening than an adjacent section of the peripheral wall.

6. The system of claim 1, wherein the mixture flow guiding device is shaped such that the transverse mixture flow impinges onto the ignition device when the ignition device is arranged in the first opening.

7. The system of claim 1, wherein the mixture flow guiding device comprises the second opening facing transversely with respect to the longitudinal axis.

8. The system of claim 1, wherein viewed in a section along the longitudinal axis, the chamber has a first wider part and a second narrower part, wherein the first opening and the second opening are arranged in the first wider part.

9. The system of claim 1, comprising the internal combustion engine having the pre-chamber component.

10. The system of claim 9, wherein the ignition device is arranged in the first opening and a device axis of the ignition device is parallel to the longitudinal axis of the chamber.

11. The system of claim 10, wherein the internal combustion engine comprises a reciprocating piston and the longitudinal axis of the chamber is parallel to a moving axis of the piston.

12. The system of claim 11, wherein a supply conduct configured to deliver the air-fuel-mixture to the chamber through the second opening is substantially aligned in parallel to the longitudinal axis of the chamber.

13. The system of claim 12, wherein the chamber and a main combustion chamber are in fluid communication via a plurality of transfer passages extending through the pre-chamber component.

14. A system, comprising: a mixture flow guide configured to couple to a pre-chamber component of an internal combustion engine, wherein the pre-chamber component comprises a chamber, a first opening configured to receive an igniter, and a second opening configured to introduce an air-fuel mixture into the chamber, wherein the mixture flow guide is configured to guide the air-fuel mixture into the chamber as a mixture flow: oriented substantially transversely with respect to a longitudinal axis from the second opening of the chamber to at least a part of the chamber adjacent to the first opening; and/or in the form of a turbulent flow.

15. The system of claim 14, comprising the pre-chamber component, the internal combustion engine, or a combination thereof, having the mixture flow guide.

16. The system of claim 14, wherein the mixture flow guide comprises a first guiding wall substantially parallel to a surface of the chamber having the first opening, and a second guiding wall substantially aligned in parallel with the longitudinal axis.

17. The system of claim 16, wherein the mixture flow guide comprises a flow break-away edge configured to create the turbulent mixture flow.

18. The system of claim 17, wherein the first guiding wall and/or the flow break-away edge is disposed on a peripheral wall of the chamber or at a greater distance from the first opening than an adjacent section of the peripheral wall.

19. The system of claim 14, wherein the mixture flow guide is shaped such that the transverse mixture flow impinges onto the igniter when the igniter is arranged in the first opening.

20. A method, comprising: guiding an air-fuel mixture as a mixture flow into a chamber of a pre-chamber component of an internal combustion engine via a mixture flow guide, wherein the pre-chamber component comprises a first opening configured to receive an igniter and a second opening configured to introduce the air-fuel mixture into the chamber, wherein the mixture flow is: oriented substantially transversely with respect to a longitudinal axis from the second opening of the chamber to at least a part of the chamber adjacent to the first opening; and/or in the form of a turbulent flow.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0073] Further details and advantages are apparent from the figures and the accompanying description of the figures, which show:

[0074] FIG. 1 is a cross-sectional view of an embodiment of a pre-chamber component according to certain embodiments of the invention,

[0075] FIG. 2 is the embodiment of FIG. 1 in a broader view mounted inside the cylinder head, and

[0076] FIGS. 3a-3d illustrate the pre-chamber component and a spark plug sleeve according to certain embodiments of the invention.

DETAILED DESCRIPTION

[0077] FIG. 1 and FIG. 2 depict a cross-sectional view of the pre-chamber component 1, according to certain embodiments of the invention, as part of an internal combustion engine Surrounding components, like the cylinder head 2 and the piston 16, are partly shown as well.

[0078] The pre-chamber component 1 is part of an ignition assembly shown in FIG. 2 also comprising the ignition device 5 (in this case a spark plug) and the supply conduit 17 for delivering the air-fuel-mixture to the pre-chamber component 1.

[0079] Only schematically indicated are a supply A for air and a reservoir F for fuel as well as a mixture device 22 for providing the air-fuel mixture. The mixture device 22 can for example be realized as a conduit for air and a fuel injector for injecting fuel, or a mixing device for mixing the fuel with the air.

[0080] The basic functionality of a mixture scavenged pre-chamber is that: [0081] the air-fuel-mixture is supplied (via the supply conduit 17 and the valve 21) to the chamber 3 of the pre-chamber component 1, [0082] the air-fuel-mixture in the chamber 3 is ignited by the ignition device 5 (arranged in the first opening 4), [0083] the combusting air-fuel-mixture expands through the chamber 3 (in the depiction of FIG. 1 downwards) through the transfer passages 19, and [0084] because of the shape of the transfer passages 19, the combusting air-fuel-mixture forms flame jets (as indicated in FIG. 2) expanding into the main combustion chamber 18 effectively igniting the mixture of air and fuel in the main combustion chamber 18.

[0085] It should be mentioned that the transfer passages 19 do not show up in full length in the sectional view of FIG. 1, as they are oriented in various directions and as such only partly intersect the view of FIG. 1.

[0086] In this embodiment, the internal combustion engine 10 shown in FIG. 1 is of a reciprocating piston configuration, such that the main combustion chamber 18 is formed by a crank case (or a cylinder liner), a reciprocating piston 16, and a cylinder head 2, which together form the cylinder.

[0087] Of course, other components like the pre-chamber component 1 according to certain embodiments of the invention, valves and the like can also be arranged in the cylinder.

[0088] The mixture flow reaches the chamber 3 through the second opening 6, where also the mixture flow guiding device 7 is arranged.

[0089] The mixture flow guiding device 7 comprises a first guiding wall 8 and a second guiding wall 9. The first guiding wall 8 faces the surface of the chamber 3 in which the first opening 4 and the ignition device 5 are arranged. The second guiding wall 9 is parallel to the portion of the peripheral wall 20 of the chamber 3, but at a greater distance from the longitudinal axis X (or the first opening 4).

[0090] The first guiding wall 8 and the second guiding wall 9 together turn the mixture flow entering through the second opening 6 as a flow parallel to the longitudinal axis X of the chamber 3 by about 90, so that the mixture flow transversely crosses the chamber 3 to reach the ignition device 5 in an essentially laminar manner.

[0091] The peripheral wall 20 and the first guiding wall 8 form a flow break-away edge 12 for creating the turbulent mixture flow. As indicated by the area of the chamber with reference T, the portion of the chamber 3 in which a (macroscopic) turbulent flow will be prevalent is quite well definedat least before ignition takes place.

[0092] Therefore, according to certain embodiments of the invention, the pre-chamber component 1 comprises the mixture flow guiding device 7 for creating both a transverse and turbulent mixture flow, where the transverse mixture flow reaches the (vicinity of the) first opening 4/the ignition device 5 in a substantially laminar way and in a separate portion T of the chamber is turbulent in nature. Therefore, on the one hand, the air-fuel-mixture reaches the ignition device 5 quickly resulting in a fast ignition of the air-fuel-mixture, and, on the other hand, the turbulence present in the chamber 3 will support a fast and thorough burning of the air-fuel-mixture once ignited.

[0093] It should be mentioned that the visualization of the portion T, where turbulent flow is prevalent, is only to be understood as a very specific example at a very specific time during the combustion cycle. Especially after ignition, the flow inside most of the chamber 3 will be turbulent on microscopic and macroscopic levels, and the ignited air-fuel-mixture will expand rapidly towards the main combustion chamber 18.

[0094] The basic idea of certain embodiments of the invention of creating a transversally and turbulently scavenged pre-chamber, therefore, not only improves the ignition performance of a mixture scavenged pre-chamber, but can also be economically implemented in, e.g., a serialized gas engine.

[0095] In the cross-sectional view of FIG. 1, along the longitudinal axis X, the chamber 3 has a first wider part 14 and a second narrower part 15, wherein the first opening 4 and the second opening 6 are arranged in the first wider part 14.

[0096] The second narrower part 15 realizes a channel for the ignited and expanding air-fuel-mixture from the first wider part 15 of the chamber towards the main combustion chamber 18 on the one hand, and for gases being transferred from the main combustion chamber 18 into the pre-chamber component 1 during a compression stroke. In the latter case, the second narrower part 15 of the chamber 3 has the effect of a buffer volume, such that the gases from the main combustion chamber 18 do not immediately reach the wider first part 14 of the chamber 3, where the ignition of the air-fuel-mixture takes place. Potentially detrimental effects of the gases from the main combustion chamber 18 on the ignition can be reduced or avoided in this way.

[0097] The chamber 3, in particular the second narrower part 15 of the chamber 3, and a main combustion chamber 18 are in fluid communication via the plurality of transfer passages 19 extending through the pre-chamber component 1.

[0098] The transfer passages 19 have a smaller cross-section compared to the second narrower part 15 of the chamber 3. Accordingly, the air-fuel-mixture ignited in the first wider part 14 of the chamber 3 is guided by successively narrower channels (first wider part 14, second narrower part 15, transfer passages 19 with smaller cross-section compared to the second narrower part 15) into the main combustion chamber 18. This results in fast directed flame jets extending from the transfer passages 19 deep into the main combustion chamber 18, which results in a thorough ignition of the mixture of fuel and air present in the main combustion chamber 18. Even cylinders of a very large capacity filled with a lean mixture of air and fuel can in such a way be fired effectively.

[0099] It should be mentioned that the longitudinal axis X of the chamber 3, a device axis of the ignition device 5, and the orientation of the supply conduit 17 are all parallel to each other. A moving axis of the reciprocating piston 16 is also parallel to the longitudinal axis X and, in the particular embodiment of FIG. 1, even coincides with the longitudinal axis X of the chamber 3. The ignition assembly comprising the pre-chamber component 1, the ignition device 5, as well as the supply conduit 17 is therefore very compact above the cylinder, so that other features like inlet valves, exhaust valves and cooling cavities can easily be accommodated in the cylinder head 2.

[0100] FIG. 2 shows the embodiment of FIG. 1 in a broader situation within the internal combustion engine 10 and makes clear the geometrically optimized way of integrating the pre-chamber component 1 according to certain embodiments of the invention into an internal combustion engine 10.

[0101] FIGS. 3a and 3b show the pre-chamber component part 1 in a perspective view and a top view, respectively. As can be seen, there is a recess 22 in which the spark plug can arranged (i.e., the recess 22 transitions into the first opening 4).

[0102] Additionally, the pre-chamber component part 1 includes an alignment 23 bore for an alignment dowel.

[0103] Furthermore, the outlets of the transfer passages 19 are visible in FIG. 3a.

[0104] FIGS. 3c and 3d depict an embodiment of a spark plug sleeve 24, which can be used together with a pre-chamber component part 1, according to certain embodiments of the invention. The spark plug sleeve 24 includes an inner surface 26, which can accommodate a thread so that the spark plug can be threaded into the spark plug sleeve 24.

[0105] Also, the spark plug sleeve 24 comprises an alignment bore 23, so that the spark plug sleeve 24 can be easily and accurately aligned relative to the pre-chamber component part 1 using an alignment dowel (not depicted).

[0106] Lastly, the spark plug sleeve 24 comprises the supply conduit 17. As shown in the embodiment according to FIGS. 3c and 3d, the supply conduit 17 can have a slightly inclined arrangement, so as to introduce the air-fuel-mixture into the chamber 3 closer to the ignition device 5 (compared to embodiments where the supply conduit 17 is not inclined).