Exhaust-gas turbocharger with acoustically active imperfections

Abstract

An exhaust-gas turbocharger (1) having a turbine housing (2), which has a bypass duct (10) with a bypass opening (9); and having a control flap (3), which is mounted pivotably between a closed position and an open position in the turbine housing (2), the control flap (3), when in its closed position, resting on a bearing region (8) of a housing wall (11) which conducts exhaust gas and contains the bypass opening (9), wherein at least one flow imperfection (12A, 12B; 23A, 23B) is arranged in the turbine housing wall (11) in the bearing region (8) of the control flap (3) and/or in the control flap (3).

Claims

1. An insert ring (13) adapted to be seated in a bypass opening (9) of an exhaust-gas turbocharger (1), the insert ring (13) having at least one flow imperfection (12; 12A, 12B; 23A, 23B) in a form of a bevel, a notch, a protrusion, or a flow guiding profile, being arranged completely around or partially around a circumference of the bypass opening (9) to reduce vibration excitation of flow.

2. The insert ring according to claim 1, wherein the at least one flow imperfection is a plurality of flow imperfections (12; 12A, 12B; 23A, 23B).

3. The insert ring according to claim 2, wherein the plurality of the flow imperfections (12; 12A, 12B; 23A, 23B) is arranged around the circumference of the bypass opening (9) at varying intervals (A1, A2) apart.

4. The insert ring according to claim 2, wherein the plurality of the flow imperfections (12; 12A, 12B; 23A, 23B) is arranged completely around the bypass opening (9).

5. The insert ring according to claim 2, wherein the plurality of the flow imperfections (12; 12A, 12B; 23A, 23B) is arranged partially around the bypass opening (9).

6. The insert ring according to claim 2, wherein the plurality of the flow imperfections (12; 12A, 12B; 23A, 23B) in a bearing region (8) is provided with different separations from each other.

7. The insert ring according to claim 1, wherein the at least one flow imperfection (12; 12A, 12B; 23A, 23B) has a width (B) or a depth (T) which varies.

8. An exhaust-gas turbocharger (1) having a turbine housing (2), which has a bypass duct (10) with a bypass opening (9); and a control flap (3), which is mounted pivotably between a closed position and an open position in the turbine housing (2), the control flap (3), when in its closed position, resting on a bearing region (8) of a housing wall (11) which conducts exhaust gas and contains the bypass opening (9), and when in the open position is pivoted away from the bypass opening (9), wherein at least one flow imperfection (12; 12A, 12B; 23A, 23B) in a form of a bevel, a notch, a protrusion, or a flow guiding profile is arranged in at least one of the housing wall (11) in the bearing region (8) of the control flap (3), and the control flap (3).

9. The exhaust-gas turbocharger according to claim 8, wherein the at least one flow imperfection is a plurality of flow imperfections (12; 12A, 12B, 23A, 23B).

10. The exhaust-gas turbocharger according to claim 9, wherein the plurality of flow imperfections (12; 12A, 12B; 23A, 23B), these are arranged distributed around the circumference of the bypass opening (9) at varying intervals (A1, A2) apart.

11. The exhaust-gas turbocharger according to claim 9, wherein the plurality of the flow imperfections (12; 12A, 12B, 23A, 23B) is in the form of a bevel or a notch and is completely arranged around the bypass opening (9).

12. The exhaust-gas turbocharger according to claim 9, wherein the plurality of the flow imperfections (12; 12A, 12B, 23A, 23B) is in the form of a bevel or a notch having a width (B) and a depth (T) and wherein the plurality of the flow imperfections (12, 12A, 12B; 23A, 23B) is arranged partially around the bypass opening (9).

13. The exhaust-gas turbocharger according to claim 9, wherein the plurality of the flow imperfections (12; 12A, 12B; 23A, 23B) in the bearing region (8) is provided with different separations from each other.

14. The exhaust-gas turbocharger according to claim 8, wherein the at least one flow imperfection (12; 12A, 12B; 23A, 23B) has a width (B) or a depth (T) which varies.

15. The exhaust-gas turbocharger according to claim 8, wherein the at least one flow imperfection (12; 12A, 12B; 23A, 23B) is formed in an insert ring (13) inserted in the bypass opening (9).

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

(1) Further details, features and advantages of the invention will become apparent from the following description of exemplary embodiments on the basis of the drawing, in which:

(2) FIG. 1 shows a schematic sectional illustration of a first embodiment of an exhaust-gas turbocharger according to the invention,

(3) FIG. 2 shows a schematically simplified enlarged sectional illustration of part of the turbine housing of the exhaust-gas turbocharger with a control flap and a bypass opening,

(4) FIG. 3 shows a perspective illustration of an insert ring, and

(5) FIG. 4 shows an illustration, corresponding to FIG. 2, of an enlarged sectional illustration of a further embodiment of the exhaust-gas turbocharger according to the invention, and

(6) FIGS. 5 and 6 show schematically simplified illustrations of the amplitudes of the flow, plotted against the flow frequency in the case of a turbocharger according to the prior art and, respectively, a turbocharger according to the principles of the present invention.

DETAILED DESCRIPTION OF THE INVENTION

(7) FIG. 1 shows an exhaust-gas turbocharger 1 according to the invention, which comprises a turbine housing 2 provided with a wastegate arrangement. This wastegate arrangement has a bypass duct 10, which connects the turbine inlet and the turbine outlet and for this purpose is provided with a bypass opening 9. Furthermore, the wastegate arrangement has a control flap 3, which is mounted pivotably between a closed position, which is shown in FIG. 1, and an open position in the turbine housing. To actuate the control flap (wastegate flap) 3, provision is made of an actuating device 4, in this example a control capsule, which is connected to the control flap 3 via a control rod 5, a connecting piece 6 and an outer lever 7, such that this actuating apparatus 4 can be used to pivot the control flap 3 into the aforementioned closed position and the open position, in which the control flap 3 releases the bypass opening 9 of the bypass duct 10, such that exhaust gas fed in can be guided past the turbine wheel 19 to the turbine housing outlet 20.

(8) The exhaust-gas turbocharger 1 according to the invention of course also has all of the other components of such turbochargers, such as in particular the compressor with a compressor wheel and a compressor housing, but these do not have to be described in detail for explaining the principles of the present invention.

(9) FIG. 2 shows a partial section through the turbine housing 2, in which the bypass duct 10 with the bypass opening 9 thereof is visible. The control flap 3, which is connected via an inner lever 22 to the control shaft 18 connected to the outer lever 7, is in the closed position, in which the bypass duct 10 or the bypass opening 9 is closed.

(10) In this closed position, a bearing region 8 of a turbine wall 11 of the turbine housing 2 is formed, the control flap 3 resting on said bearing region with its outer circumferential rim on the end face 21 of said turbine wall 11, as can be seen in detail in FIG. 2.

(11) At least one flow imperfection 12A, 12B, which can have a width B and a depth T which in principle are freely selectable, is arranged in said bearing region 8.

(12) Although, in FIG. 2, this flow imperfection 12A, 12B is arranged only in the bearing region 8, it is likewise possible according to the invention to provide such a flow imperfection or a plurality of such flow imperfections in the control flap 3, these then being arranged in the region of the control flap which rests on the bearing region 8.

(13) According to the invention, it is possible that the flow imperfection runs partially around the bypass opening 9 or is formed so as to run completely around this opening 9.

(14) Furthermore, it is possible, as already stated above, to provide a plurality of such flow imperfections 12A, 12B.

(15) The width B and the depth T in the case of a plurality of flow imperfections 12A, 12B can be adapted or chosen depending on the application and it is possible that the individual flow imperfections each have different widths and depths, but it is likewise possible in principle that all of the flow imperfections have an identical form both in respect of their geometrical configuration and their dimensioning.

(16) Furthermore, it is possible according to the invention to vary the positions of the flow imperfections from application to application, in order to be able to achieve noise reduction.

(17) This also applies to the choice of the number of flow imperfections, which can likewise vary from case to case.

(18) In a particularly preferred embodiment, the bypass opening 9 is provided with an insert ring 13, which is shown in FIG. 3. When inserted in the bypass opening 9, this insert ring 13 forms the wall region which corresponds to the turbine housing wall 11 of the embodiment as shown in FIG. 2, which comprises the bearing region 8. Accordingly, this region of the insert ring which corresponds to the bearing region 8 is provided with at least one flow imperfection 12A, 12B. When an insert ring 13 is provided, it is also possible, however, to provide a plurality of flow imperfections 12A, 12B in different widths and depths and positions, as can be seen from FIG. 3.

(19) FIG. 4 shows an illustration, corresponding to FIG. 2, of a further embodiment of the exhaust-gas turbocharger according to the invention. In contrast to the embodiment shown in FIG. 2, in this embodiment two protrusions or flow-guiding profiles 23A and 23B are provided as flow imperfections. It is possible in this embodiment, too, as described above on the basis of the bevels or notches, to vary the number, position and dimensioning of these flow-guiding profiles and the interval therebetween. Accordingly, the two flow-guiding profiles 23A and 23B visible in FIG. 4 are only representatives of either one or a plurality of such flow imperfections in the form of protrusions.

(20) Otherwise, reference can be made to the description of FIG. 2 in respect of the further components visible in FIG. 4.

(21) FIGS. 5 and 6 schematically show slightly simplified illustrations of amplitudes of the flow through the bypass opening. FIG. 5 in this respect shows the peaks P1 to P4 of a known arrangement, which, as a comparison with FIG. 6 shows, are considerably higher than the peaks P1 to P4 of the arrangement according to the invention, which are assigned by way of example to flow imperfections 12 of the bypass opening 9.

(22) Since at least one flow imperfection is provided in the control flap itself and/or in a bearing region of the control flap around the bypass opening, the body-borne noise in the 8.7 kHz range can be reduced to a measure which was no longer measurable; this was shown by further tests carried out within the context of the invention. In the 0.57 kHz range, these tests furthermore showed that it was possible to reduce the body-borne noise considerably.

(23) In summary, it can therefore be established that the introduction of flow imperfections of an indeterminate width, depth, number and position over the ring circumference (bearing region of the control flap) makes it possible to considerably improve the production/excitation of the flow noise and thereby the acoustic characteristics of the exhaust-gas turbocharger according to the invention.

(24) In addition to the above written disclosure of the invention, reference is hereby explicitly made to the diagrammatic illustration thereof in FIGS. 1 to 6.

LIST OF REFERENCE SIGNS

(25) 1 Exhaust-gas turbocharger 2 Turbine housing 3 Control flap 4 Actuating device 5 Control rod 6 Connecting piece 7 Outer lever 8 Bearing region 9 Bypass opening 10 Bypass duct 11 Turbine housing wall 12, 12A, 12B Flow imperfection (bevels, notches) 13 Insert ring 14, 15 Outlet regions 16, 17 Base corners 18 Control shaft 19 Turbine wheel 20 Turbine outlet 21 End face 22 Inner lever A1, A2 Varying intervals 23A, 23B Flow imperfections in the form of protrusions B Width T Depth P1-P4 Peaks of the prior art P1-P4 Peaks according to the principles of the present invention