Valve device for a turbine of an exhaust gas turbocharger, and turbine for an exhaust gas turbocharger

Abstract

A valve device for a turbine of an exhaust gas turbocharger includes a valve element for at least partial fluidic shutting of a bypass line via which a turbine wheel of the turbine can be bypassed by exhaust gas. The valve device also has an actuating arm which is coupled in an articulated manner to the valve element and via which the valve element can be pivoted and has at least one spring element via which the valve element is supported on the actuating arm. The valve element has at least one uneven supporting surface via which the spring element is supported on the valve element.

Claims

1. A valve device for a turbine of an exhaust gas turbocharger, comprising: a valve element for at least partially fluidically blocking a bypass line via which a turbine wheel of the turbine is bypassable by exhaust gas; an actuating arm which is coupled in an articulated manner to the valve element and via which the valve element is pivotable; and a spring element via which the valve element is supported on the actuating arm; wherein the valve element has a first uneven supporting surface via which the spring element is supported on the valve element; and wherein the first uneven supporting surface includes a rounded corner.

2. The valve device according to claim 1, wherein the first uneven supporting surface is disposed on a side of the valve element that faces a partial region of the spring element.

3. The valve device according to claim 1, wherein the spring element directly touches the first uneven supporting surface.

4. The valve device according to claim 1, wherein the first uneven supporting surface is convex.

5. The valve device according to claim 1, wherein the spring element has a second uneven supporting surface via which the spring element is supported on the first uneven supporting surface and wherein the second uneven supporting surface and the first uneven supporting surface are adapted to each other with respect to their respective shapes.

6. The valve device according to claim 1, wherein the spring element has a second uneven supporting surface or an even supporting surface via which the spring element is supported on the first uneven supporting surface.

7. The valve device according to claim 6, wherein the second uneven supporting surface or the even supporting surface directly touches the first uneven supporting surface.

8. The valve device according to claim 1, wherein the spring element has a second uneven supporting surface via which the spring element is supported on the first uneven supporting surface and wherein the second uneven supporting surface is curved.

9. The valve device according to claim 8, wherein the second uneven supporting surface is curved concavely or convexly.

10. A turbine for an exhaust gas turbocharger, comprising: a valve device, wherein the valve device includes: a valve element for at least partially fluidically blocking a bypass line via which a turbine wheel of the turbine is bypassable by exhaust gas; an actuating arm which is coupled in an articulated manner to the valve element and via which the valve element is pivotable; and a spring element via which the valve element is supported on the actuating arm; wherein the valve element has an uneven supporting surface via which the spring element is supported on the valve element; and wherein the uneven supporting surface includes a rounded corner.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 shows a schematic and sectioned top view of part of a valve device according to the invention, with a valve element, with an actuating arm coupled in an articulated manner to the valve element and with a spring element via which the valve element is supported on the actuating arm, wherein the valve element has an uneven supporting surface via which the spring element is supported on the valve element, and wherein a starting position of the valve element is shown in FIG. 1; and

(2) FIG. 2 shows a further schematic and sectioned top view of part of the valve device, wherein FIG. 2 shows a movement position of the valve element different from the starting position.

DETAILED DESCRIPTION OF THE DRAWINGS

(3) In the Figures, identical or functionally identical elements are provided with the same reference signs.

(4) FIG. 1 shows, in a schematic and sectioned top view, part of a valve device 1 for a turbine of an exhaust gas turbocharger, in particular for an internal combustion engine. The internal combustion engine is, for example, part of a drive train of a motor vehicle which is designed in particular as an automobile and as a passenger vehicle and is drivable by means of the drive train, in particular by means of the internal combustion engine. The internal combustion engine here has, for example, at least one combustion chamber which is designed in particular as a cylinder and in which combustion operations proceed during a fired operation of the internal combustion engine. The combustion operations result in exhaust gas of the internal combustion engine, the exhaust gas being removed from the combustion chamber by means of an exhaust train of the internal combustion engine. The turbine is arranged in the exhaust tract and, accordingly, the exhaust gas can flow through the turbine and can drive same. For this purpose, the turbine comprises a turbine housing (not shown in the Figures) with a receiving space in which a turbine wheel (not shown in the Figures) of the turbine is at least partially, in particular at least predominantly or completely, rotatably accommodated. The turbine wheel can therefore rotate relative to the turbine housing. The exhaust gas can flow through the turbine housing, wherein the exhaust gas flowing through the turbine housing can flow by means of the turbine housing to the receiving space and therefore to the turbine wheel. The turbine wheel is thereby driven by the exhaust gas.

(5) The turbine or the exhaust gas turbocharger has at least one bypass channel through which at least some of the exhaust gas can flow. At least some of the exhaust gas can bypass the turbine wheel via the bypass channel. This means that the exhaust gas flowing through the bypass channel does not flow through the turbine wheel and accordingly does not drive the latter.

(6) The valve device 1 has a valve element 2 which, for example, is designed at least substantially in a disk-like or disk-shaped manner and therefore, for example, as a disk valve. For this purpose, the valve element 2 comprises, for example, a valve disk 3 and a shaft 4 which is connected to the valve disk 3 and is formed, for example, integrally with the valve disk 3. The valve element 2 is movable, in particular pivotable, between a closed position and at least one open position relative to the turbine housing. In the closed position, at least a part of the bypass channel is fluidically blocked by the valve element 2, in particular by the valve disk 3, in particular the bypass channel is at least predominantly, in particular completely, fluidically blocked by means of the valve element 2, in particular by means of the valve disk 3, in the closed position. In the open position, the valve element 2 opens up at least a part of the bypass channel, and therefore exhaust gas can flow through the part. By pivoting of the valve element 2 between the open position and the closed position, for example, a quantity of the exhaust gas flowing through the bypass channel can be set, as a result of which, for example, a charging pressure of the exhaust gas turbocharger can be set, in particular adjusted. In the closed position, the valve element 2, in particular the valve disk 3, sits, for example, on a corresponding valve seat, as a result of which at least the part of the bypass channel is fluidically blocked. For example, an in particular at least substantially annular sealing surface 5 of the valve element 2, in particular of the valve disk 3, touches the corresponding valve seat.

(7) The valve device 1 furthermore comprises an actuating arm 6 which is pivotable about a pivot axis relative to the turbine housing. The valve element 2 is coupled here in an articulated manner to the actuating arm 6, and therefore the valve element 2 is pivotable between the open position and the closed position via the actuating arm 6, that is to say by pivoting of the actuating arm 6. In other words, in order to pivot the valve element 2 between the open position and the closed position, the actuating arm 6 is pivoted here. For this purpose, for example, an actuator, not illustrated in the Figures, such as, for example, an electric linear actuator or rotary actuator or a pressure capsule, in particular a negative pressure capsule, is provided, by means of which the actuating arm 6 and, via the latter, the valve element 2 can be pivoted.

(8) The articulated coupling of the valve element 2 to the actuating arm 6 should be understood as meaning in particular that the valve element 2—while it is connected to the actuating arm 6, can be moved, in particular pivoted, relative to the actuating arm 6. In order to couple the valve element 2 to the actuating arm 6, the actuating arm 6, for example, has a passage opening 7 which is penetrated by the shaft 4. A connecting element 9 designed, for example, as a ring is arranged on a side 8 of the actuating arm 6 that faces away from the valve disk 3, the connecting element being used to hold the valve element 2 on the actuating arm 6.

(9) The valve device 1 furthermore comprises a spring element 10 which is also simply referred to as spring. The spring element 10 is arranged on a side 11 of the actuating arm 6 that faces away from the side 8 and therefore faces the valve disk 3, wherein the spring element 10 is arranged between the actuating arm 6 and the valve disk 3. In particular, the spring element 10 is arranged between the actuating arm 6, in particular the side 11, and a side 12 of the valve disk 3 that faces the actuating arm 6 and is also referred to as the rear side.

(10) It can be particularly readily seen from FIGS. 1 and 2 that the valve element 2 is supported, in particular supported in a sprung manner, on the actuating arm 6 via the spring element 10. FIG. 1 shows a starting position of the valve element 2, wherein FIG. 2 shows a movement position of the valve element 2 different from the starting position. In the starting position shown in FIG. 1, the valve element 2 and the spring element 10 take up a respective installation position. In the starting position or in the installation position, for example, the spring element 10 is elastically deformed and thereby pretensioned such that the spring element 10 has a pretension in the starting position or in the installation position and, accordingly, provides, for example, a spring force which acts on the valve element 2 and by means of which the valve element is held in the starting position relative to the actuating arm 6. In particular, it is provided, for example, that the spring element 10 directly touches or contacts the actuating arm 6 and/or the valve element 2.

(11) As will also be explained in more detail below, the valve device 1 is now configured in such a manner that, when, for example, the valve element 2 moves relative to the actuating arm 6 and is thereby moved from the starting position into the movement position shown in FIG. 2, the spring element 10 is not elastically deformed to a greater extent than in the starting position and therefore is not tensioned beyond the pretension. As a result, the spring element 10, for example in the starting position and in the movement position, provides at least substantially the same spring force which acts on the valve element 2 and the actuating arm 6.

(12) In order to be able to realize this and, as a result, particularly high robustness of the valve device 1 and thereof the turbine as a whole, the valve element 2 has at least one supporting surface 16 via which the spring element 10 is supported on the valve element 2, wherein the supporting surface 16 is uneven. In the exemplary embodiment illustrated in FIGS. 1 and 2, the supporting surface 16 is uneven and has a shape different from a conical shape. In particular, the supporting surface 16 is designed, for example, to be at least substantially spherical or globular or parabolic or ball-shaped. The supporting surface 16 is arranged here on a side 14 of the valve element 2 that faces at least a partial region 13 of the spring element 10, wherein, in the exemplary embodiment illustrated in FIGS. 1 and 2, the supporting surface 16 is arranged on the rear side (side 12) of the valve disk 3.

(13) In addition, it is provided in the exemplary embodiment that the spring element 10 directly touches or contacts the supporting surface 16. In addition, the supporting surface 16 is designed to be curved and convex, and therefore the supporting surface 16 is curved toward the spring element 10.

(14) By means of this configuration of the supporting surface 16, a geometry of the valve element 2, in particular of the supporting surface 16, is provided in such a manner that the spring element 10 via its pretension provided in the installation position and via a gas-dynamic and thermal loading acting on the spring element 10 during operation of the turbine and brought about, for example, by the exhaust gas, does not experience any further loading-relevant, in particular plasticizing deformation if, for example because of the operation, a relative movement occurs between the valve element 2 and the actuating arm 6. In other words, the spring beyond its pretension in the installation position and the thermal loading during the operation is not additionally loaded and damaged by deformation and plasticization if the valve element 2 is moved relative to the actuating arm 6.

(15) By means of this design of the valve element 2, in particular of the supporting surface 16, the spring element 10 both in the starting position and in the movement position and also in all other movement positions into which the valve element 2 can be moved relative to the actuating arm 6, is at least substantially identically elastically deformed and therefore provides the at least substantially identical spring force, and therefore movement of the valve element 2 out of the starting position does not cause a further elastic deformation and also does not cause a plastic deformation of the spring element 10, but rather the spring element 10 has its pretension, for example, both in the starting position and in the movement positions and provides the spring force.

(16) In particular, it can be provided that the spring element 10 has a second supporting surface 15 via which the spring element 10 is supported on the first supporting surface 16 and therefore on the valve element 2. The second supporting surface 15 is preferably of uneven design here, wherein preferably the second supporting surface 15 directly touches or contacts the first supporting surface 16. In particular, it is conceivable for the second supporting surface 15 to be curved, in particular concavely or convexly. Furthermore, it is possible for the second supporting surface 15 to be formed of even design. It is preferably provided that the supporting surfaces 16 and 15 are adapted to each other in respect of their respective shapes, and therefore, for example, the supporting surface 15 is adapted in respect of its curvature to the curvature of the supporting surface 16, or vice versa. By this means, particularly high robustness can be provided. In addition, it is possible for the second supporting surface 15 to be designed as a convex bead which is then opposed to the first supporting surface 16 and, instead of surface contact, has only linear contact with the first supporting surface 16.

(17) The supporting surfaces 15 and 16 preferably contact or touch each other directly. Furthermore, it is provided that the supporting surface 15 is at least partially, in particular at least predominantly or completely, arranged in the partial region 13 or is formed by the latter, and therefore the supporting surfaces 15 and 16 face each other and can therefore directly touch each other.

(18) It is preferably provided that the supporting surfaces 15 and 16 are completely closed or encircle in a completely closed manner, for example in the circumferential direction of the spring element 10 or of the valve element 2, and are therefore, for example, of annular design. For example, the supporting surface 15 forms a receiving region or receiving space in which the supporting surface 16 is accommodated, and therefore, for example, the supporting surface 15 is arranged on opposite sides, in the direction of which the valve element 2 is supported on the spring element 10 via the supporting surface 16 or on the supporting surface 16.

LIST OF REFERENCE CHARACTERS

(19) 1 Valve device 2 Valve element 3 Valve disk 4 Shaft 5 Sealing surface 6 Actuating arm 7 Through opening 8 Side 9 Connecting element 10 Spring element 11 Side 12 Side 13 Partial region 14 Side 15 Second supporting surface 16 First supporting surface

(20) The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.