GAS INJECTOR INCLUDING AN OUTWARDLY OPENING VALVE CLOSURE ELEMENT

Abstract

A gas injector for directly injecting a gaseous fuel into a combustion chamber of an internal combustion engine, including a valve closure element for releasing and closing a passage opening, the valve closure element opening in the direction of a flow direction of the gas injector, a sealing seat between the valve closure element and a valve body, a flow-guiding element being situated downstream of the sealing seat in the flow direction of the gas injector and configured to form a gas jet to be injected into the combustion chamber.

Claims

1-18. (canceled)

19. A gas injector for directly injecting a gaseous fuel into a combustion chamber of an internal combustion engine, comprising: a valve closure element for releasing and closing a passage opening, the valve closure element opening in a direction of a flow direction of the gas injector; a sealing seat between the valve closure element and a valve body; and a flow-guiding element situated downstream of the sealing seat in the flow direction of the gas injector, and is configured to form a gas jet to be injected into the combustion chamber.

20. The gas injector as recited in claim 19, wherein the flow-guiding element is situated on the valve body.

21. The gas injector as recited in claim 20, wherein the flow-guiding element is integrally formed with the valve body.

22. The gas injector as recited in claim 19, wherein the flow-guiding element is situated on the valve closure element.

23. The gas injector as recited in claim 22, wherein the flow-guiding element is integrally formed with the valve closure element.

24. The gas injector as recited in claim 19, wherein the flow-guiding element includes a partial sphere surface.

25. The gas injector as recited in claim 19, wherein the flow-guiding element includes a conical surface.

26. The gas injector as recited in claim 19, wherein the flow-guiding element includes a cylindrical surface.

27. The gas injector as recited in claim 19, wherein a center axis of the gas jet intersects an axial axis of the gas injector at an angle.

28. The gas injector as recited in claim 27, wherein the angle lies in a range from 0° through 60°.

29. The gas injector as recited in claim 28, wherein the angle is in a range from 10° through 60°.

30. The gas injector as recited in claim 19, wherein the sealing seat is a flat seat.

31. The gas injector as recited in claim 19, wherein the flow-guiding element is of symmetrical design.

32. The gas injector as recited in claim 19, wherein the flow-guiding element is configured to generate one of a cylindrical or conical or annular gas jet.

33. The gas injector as recited in claim 19, wherein the valve closure element has a conical sealing surface on the sealing seat.

34. The gas injector as recited in claim 19, wherein the flow-guiding element includes a first and a second arcuate guide surface, which are connected to one another by an inflection point apparent in a cross-sectional plane.

35. An internal combustion engine, comprising: a cylinder head; a gas injector situated directly on a combustion chamber and in the cylinder head, the gas injector for directly injecting a gaseous fuel into the combustion chamber, the gas injector including a valve closure element for releasing and closing a passage opening, the valve closure element opening in a direction of a flow direction of the gas injector, a sealing seat between the valve closure element and a valve body, and a flow-guiding element situated downstream of the sealing seat in the flow direction of the gas injector, and is configured to form a gas jet to be injected into the combustion chamber.

36. The internal combustion engine as recited in claim 35, wherein the gas injector is situated in the cylinder head in such a way that a combustion chamber-side end of the flow-guiding element is spaced at a distance from a combustion chamber-side end of the cylinder head.

37. The internal combustion engine as recited in claim 36, wherein the combustion chamber-side end of the flow-guiding element protrudes into the combustion chamber.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Preferred exemplary embodiments of the present invention are explained in greater detail below with reference to the figures. Identical or functionally identical parts are denoted using the same reference symbols.

[0020] FIG. 1 shows a schematic sectional view of a gas injector according to a first exemplary embodiment of the present invention.

[0021] FIGS. 2 to 15 show various further exemplary embodiments of the gas injector according to the present invention.

DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS

[0022] A gas injector 1 according to a first preferred exemplary embodiment of the present invention is described in detail below with reference to FIG. 1.

[0023] As shown in FIG. 1, gas injector 1 includes a valve closure element 2, which in this exemplary embodiment is a valve needle. Gas injector 1 is an outwardly opening gas injector, since valve closure element 2 opens in the direction of flow (arrow B). This means that valve closure element 2 lifts off from a valve seat 4 in the direction of a combustion chamber 10. In FIG. 1, the direction of movement for opening valve closure element 2 is indicated by arrow A.

[0024] Valve closure element 2 opens and closes a passage opening 8, which is formed in a valve body 3. Valve body 3 also forms the housing of gas injector 1.

[0025] Valve closure element 2 is opened with the aid of a solenoid actuator 7. Solenoid actuator 7 includes an armature 70, which is directly connected to the valve closure element 2. Furthermore, a coil 71 and an internal pole 72 are provided. When coil 71 is energized, the armature is moved in the direction of combustion chamber 10 against a spring force of a restoring element 9, as a result of which valve closure element 2 lifts off from sealing seat 4. As a result, passage opening 8 is released, so that gaseous fuel is injected into combustion chamber 10.

[0026] FIG. 1 schematically shows a gas jet 6 in dashed lines, which indicates the gaseous spray into combustion chamber 10 in the opened state of gas injector 1. Gas jet 6 has a conical outer surface. In order to achieve this, a flow-guiding element 5 is provided according to the present invention. Flow-guiding element 5 is integrally formed with valve body 3 and includes a first guide surface 51 and a second guide surface 52. First guide surface 51 is perpendicular to an axial axis X-X of gas injector 1. Immediately adjoining this is second guide surface 52, which is conical in design. As a result, gas jet 6 acquires the conical outer surface area.

[0027] An angle between axial axis X-X and flow-guiding element 5 is denoted by α/2 and is approximately 250. This angle α may be arbitrarily set between 0° and 180° according to the requirements of the combustion method.

[0028] According to the present invention, flow-guiding element 5 is thus situated downstream of sealing seat 4 in flow direction B of gas injector 1. Consequently, according to the present invention, a shaping of gas jet 6 is carried out separately from sealing seat 4 or from an annular gap between valve closure element 2 and valve body 3 in the completely open state of the gas injector, which defines the maximum volume flow. As a result, a customer-specific design of flow-guiding element 5 may be made possible. According to the present invention, sealing seat 4 may also be optimized independently of additional, in particular, shaping influences for gas jet 6 in order to optimally absorb occurring flow forces and closing forces. This is achieved according to the present invention in combination with an outwardly opening gas injector 1. Consequently, a very variable design of gas injector 1 is obtained, which is possible both for a central installation as shown in FIG. 1, and a lateral installation in a cylinder head. Consequently, an independent design of sealing seat 4 and the fuel flow, i.e., generated gas jet 6, may be obtained in combustion chamber 10 for an outwardly opening gas injector 1 by the positioning of flow-guiding element 5 downstream of sealing seat 4. Since, according to the present invention a gaseous fuel is provided, the problem in the case of liquid fuels, namely that droplets form on flow-guiding element 5 resulting in a detrimental effect on the formation of exhaust gas, does not arise either.

[0029] FIG. 2 shows a gas injector 1 according to a second exemplary embodiment of the present invention. As is apparent from FIG. 1, flow-guiding element 5 includes, as in the first exemplary embodiment, a second conical guide surface 52. However, the guide surface provided between second guide surface 52 and sealing seat 4 in the second exemplary embodiment is designed as an arcuate guide surface 53. As a result, a continuous transition from arcuate guide surface 53 into second conical guide surface 52 may be made possible.

[0030] FIG. 3 shows a gas injector 1 according to a third exemplary embodiment of the present invention. In this third exemplary embodiment, flow-guiding element 5 includes, as shown in FIG. 2, first arcuate guide surface 53 and a second arcuate guide surface 54. Between the two arcuate guide surfaces 53, 54, an inflection point W, which may be seen in a cross-sectional plane, is provided in the geometric profile of flow-guiding element 5. In particular, this results in a so-called central jet as gas jet 6, which is essentially annular-cylindrical and consequently parallel to axial axis X-X of gas injector 1. Instead of being cylindrical, the surface of gas jet 6 may also be slightly conical.

[0031] FIG. 4 shows a gas injector according to a fourth exemplary embodiment of the present invention, whereby an installation position in a cylinder head 11 is shown in particular. As is apparent from FIG. 4, gas injector 1 is set back somewhat from combustion chamber 10. More precisely, a distance 12 is provided between a combustion chamber-side end of cylinder head 11 and a combustion chamber-side end 50 of flow-guiding element 5. Sealing seat 4 may be positioned somewhat farther away from hot combustion chamber 10, so that an elastomeric sealing element may also be considered as a sealing element.

[0032] FIG. 5 shows a fifth exemplary embodiment of gas injector 1, which represents a different installation position from that shown in FIG. 4. In the fifth exemplary embodiment, gas injector 1 is situated protruding into the combustion chamber, a combustion-side end of flow-guiding element 5 protruding into combustion chamber 10 from the combustion-side end of cylinder 11 by a distance 13.

[0033] In the fifth exemplary embodiment, a conical gas jet 6 results, since combustion chamber-side end 50 of flow-guiding element 5 is shortened compared to FIG. 4.

[0034] FIG. 6 shows a gas injector 1 according to a sixth exemplary embodiment of the present invention. The shaping of flow-guiding element 5 of the sixth exemplary embodiment corresponds to that of the third exemplary embodiment, so that flow-guiding element 5 of the sixth exemplary embodiment includes a first arcuate guide surface 53 and a second arcuate guide surface 54, which are connected to one another via an inflection point W. In contrast to the third exemplary embodiment, however, valve closing element 2 is also designed to have a flow-guiding area 20. Flow-guiding element 5 on valve body 3 is responsible for the shaping of gas jet 6 on the outer surface of the gas jet, and flow-guiding area 20, which is formed downstream of sealing seat 4 on valve closing element 2, is responsible for the shaping of an inner surface area 60 of gas jet 6. Consequently, in addition to flow-guiding element 5 on valve body 3, a flow-guiding area 20 is also provided on valve closure element 2. As a result, a very exact shaping of gas jet 6 may be obtained both on its outer circumference and also on its inner circumference. In this exemplary embodiment, flow-guiding area 20 is formed in such a way that a tapering inner surface area is obtained on inner circumference 60.

[0035] FIG. 7 shows a gas injector 1 according to a seventh exemplary embodiment of the present invention. The seventh exemplary embodiment essentially corresponds to the sixth exemplary embodiment, whereby a recess 61 is provided for reducing the weight on valve closure element 2 in the area downstream of sealing seat 4. As a result, a faster movement of valve closure element 2 for opening and closing may be ensured.

[0036] FIG. 8 shows a gas injector 1 according to an eighth exemplary embodiment of the present invention. In contrast to the preceding exemplary embodiment, in the eighth exemplary embodiment, flow guiding element 5 is formed in such a way that a radial outflow of gas jet 6 from valve body 3 is possible. On valve closure element 2, flow guiding element is formed in such a way that the radial outflow is assisted. Flow-guiding element 5 includes an arcuate guide surface 53, so that radial outflow is achieved.

[0037] FIGS. 9 through 12 show a gas injector 1, which in each case has a flat sealing seat 4. In this case, a sealing partner 30 on valve body 3 has a surface which is perpendicular to axial axis X-X.

[0038] In the ninth exemplary embodiment of gas injector 1 shown in FIG. 9, a radial outflow of gas jet 6 is implemented as in FIG. 8. In this case, flow-guiding element 5 is provided with a surface 55, which is perpendicular to axial axis X-X.

[0039] In the tenth exemplary embodiment of gas injector 1 shown in FIG. 10, flow-guiding element 5 includes a guide area on surface 55, which is perpendicular to axial axis X-X, and a guide surface 51, which is conical. This results in a gas jet 6, similar to the first exemplary embodiment in FIG. 1, but with the difference that, in the case of an outwardly opening gas injector 1, a flat sealing seat 4 is now implemented.

[0040] The eleventh exemplary embodiment of gas injector 1 shown in FIG. 11 includes a flow-guiding element 5 including an arcuate guide surface 53 in combination with a flat sealing seat 4. As a result of this, it is essentially possible to achieve a conically expanding gas jet 6, a flat seat being provided as a sealing seat.

[0041] FIG. 12 shows a gas injector 1 according to a twelfth exemplary embodiment of the present invention, whereby, in addition to flow-guiding element 5 on valve body 3, a flow-guiding area 20 is also provided on valve closure element 2. This results in an annular gas jet 6, which expands in the combustion chamber. An inner circumference 60 of gas jet 6 is defined here by the shaping of flow-guiding area 10 on valve closure element 2.

[0042] FIG. 13 shows a gas injector 1 according to a thirteenth exemplary embodiment of the present invention. A shaping of gas jet 6 corresponds to the exemplary embodiment shown in FIG. 10 having a rectilinear surface 55 which is perpendicular to axial axis X-X and a conical guide surface 51. However, flow-guiding element 5 is provided as a separate component on valve body 3 in the thirteenth exemplary embodiment. Flow-guiding element 5 is, for example, connected to valve body 3 with the aid of a weld 31. Consequently, valve body 3 and flow-guiding element 2 are provided as a two-part component; however, providing flow-guiding element 5 separately makes it possible to respond in a simple manner to different requirements of internal combustion engine manufacturers by simply exchanging flow-guiding element 5.

[0043] Gas injectors 1 described in the preceding exemplary embodiments in FIGS. 1 through 13 each have a symmetrical design of flow-guiding element 5 as well as of valve closure element 2 with respect to axial axis X-X.

[0044] The fourteenth exemplary embodiment of gas injector 1 shown in FIG. 14, on the other hand, shows a design of flow-guiding element 5 in asymmetrical form. In other words, flow-guiding element 5 is asymmetrical in relation to axial axis X-X. As is apparent from FIG. 14, a first area 56 formed by a plurality of arcuate surfaces and a second area 57 having a recess, result. As a result, a gas jet 6 is achieved, center axis Y-Y of which is at an angle γ in relation to axial axis X-X. Consequently, the present invention makes it possible to define a jet angle γ in relation to axial axis X-X and adapt it to particular customer requirements. In the exemplary embodiment, gas jet 6 is provided in cylindrical form.

[0045] FIG. 15 shows a fifteenth exemplary embodiment of the present invention in which flow-guiding element 5 of gas injector 1 is likewise designed asymmetrically. A conical gas jet 6 is achieved by the shaping of flow-guiding element 5 in this exemplary embodiment.

[0046] According to the present invention, in the case of an outwardly opening gas injector, a separation of the geometry of the sealing seat from the geometry of the jet formation, which is predefined with the aid of flow-guiding element 5 on valve body 3 and/or flow-guiding area 20 on valve closure element 2, is achieved for the first time. As a result, individual approaches for gas jets 6, which are injected directly into a combustion chamber 10, are possible. Therefore, the fact is particularly utilized that due to the gaseous fuel there is no wall wetting and droplet formation of the fuel during the injection process. Consequently, sealing seat 4 may also be designed independently of the jet application process of gas jet 6.