COMPRESSOR WHEEL

Abstract

A compressor wheel for a compressor of a turbocharger has a hub (16) and a multiplicity of blades (12) on the hub (16). In intermediate spaces of the multiplicity of blades (12), a channel is in each case formed between a suction side (24) and a pressure side (26). The channel guides fluid that flows in axially in relation to a rotation axis (22) radially or radially-axially outward. The hub (16) in relation to the rotation axis (22) in at least one channel is contoured with a rotationally symmetrical portion (18′) and a non-rotationally symmetrical portion (18). The non-rotationally symmetrical portion (18) is formed by radii that are variable in the flow direction, and a transition region (28) between the hub (16) and the blade (12) adjoins the non-rotationally symmetrical portion (18).

Claims

1. A compressor wheel for a compressor of a turbocharger, the compressor wheel comprising a hub and a multiplicity of blades on the hub, wherein in intermediate spaces of the multiplicity of blades a channel is in each case formed between a suction side and a pressure side, the channel guiding fluid that flows in axially in relation to a rotation axis radially or radially-axially outward, wherein the hub in relation to the rotation axis in at least one channel is contoured with a rotationally symmetrical portion and a non-rotationally symmetrical portion, wherein the non-rotationally symmetrical portion is formed by radii that are variable in the flow direction, and a transition region between the hub and the blade adjoins the non-rotationally symmetrical portion.

2. The compressor wheel as claimed in claim 1, wherein the transition region is embodied as a constant-radius connection or as variable radiusing.

3. The compressor wheel as claimed in claim 2, wherein the transition region is embodied as a constant-radius connection, and wherein the radius of the constant-radius connection corresponds to that of a ball cutter.

4. The compressor wheel as claimed in claim 1, wherein the non-rotationally symmetrical portion of the hub has a region of modified thickness.

5. The compressor wheel as claimed in claim 4, wherein the region of modified thickness is embodied in that a surface of the hub is raised or lowered in comparison to a rotationally symmetrical hub.

6. The compressor wheel as claimed in claim 4, wherein the region of modified thickness is embodied such that internal stress in the compressor wheel is reduced.

7. The compressor wheel as claimed in claim 1, wherein the rotationally symmetrical portion and the non-rotationally symmetrical portion of the hub are produced in a milling process.

8. The compressor wheel as claimed in claim 1, wherein the non-rotationally symmetrical portion of the hub begins at the external periphery of the hub and extends radially inward.

9. The compressor wheel as claimed in claim 1, wherein the non-rotationally symmetrical portion of the hub partially spans the region between the blades.

10. The compressor wheel as claimed in claim 1, wherein the non-rotationally symmetrical portion of the hub is configured on all channels of the compressor wheel.

11. A charging device in a vehicle, wherein the charging device has a compressor having a compressor wheel as claimed in claim 1.

12. The compressor wheel as claimed in claim 2, wherein the non-rotationally symmetrical portion of the hub has a region of modified thickness.

13. The compressor wheel as claimed in claim 3, wherein the non-rotationally symmetrical portion of the hub has a region of modified thickness.

14. The compressor wheel as claimed in claim 12, wherein the region of modified thickness is embodied in that a surface of the hub is raised or lowered in comparison to a rotationally symmetrical hub.

15. The compressor wheel as claimed in claim 13, wherein the region of modified thickness is embodied in that a surface of the hub is raised or lowered in comparison to a rotationally symmetrical hub.

16. The compressor wheel as claimed in claim 3, wherein the non-rotationally symmetrical portion of the hub begins at the external periphery of the hub and extends radially inward.

17. The compressor wheel as claimed in claim 4, wherein the non-rotationally symmetrical portion of the hub begins at the external periphery of the hub and extends radially inward.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] A number of exemplary embodiments will be discussed in more detail below on the basis of the drawing, in which:

[0026] FIG. 1 shows a charging device for an internal combustion engine in a sectional illustration;

[0027] FIG. 2 shows an embodiment of a compressor wheel according to the invention in a perspective lateral view;

[0028] FIG. 3A shows a further compressor wheel according to the invention in a partially cut-away, perspective lateral view;

[0029] FIG. 3B shows a detail of the compressor wheel from FIG. 3A in a partially cut-away, perspective lateral view;

[0030] FIG. 3C shows a further detail of the compressor wheel from FIG. 3A in a partially cut-away, perspective lateral view;

[0031] FIG. 4A in a comparative example shows a known compressor wheel in a perspective lateral view;

[0032] FIG. 4B shows a detail of the compressor wheel from FIG. 4A in a perspective lateral view;

[0033] FIG. 5A shows a further compressor wheel according to the invention in a partially cut-away, perspective lateral view; and

[0034] FIG. 5B shows a detail of the compressor wheel from FIG. 5A in a partially cut-away, perspective lateral view.

DETAILED DESCRIPTION

[0035] In the figures, identical or functionally equivalent components are provided with the same reference signs.

[0036] Firstly, a charging device 1 in which a design embodiment of a compressor wheel according to the invention can preferably be used will be schematically described hereunder by means of FIG. 1. FIG. 1 in a sectional view here shows the charging device 1 only in a highly schematic manner in order to be able to illustrate the position of the individual components. Charging devices 1 of this type are known per se from the prior art.

[0037] FIG. 1 shows a perspective, partially sectional view of a charging device 1 according to the invention. The charging device 1 has a turbine housing 2 and a compressor housing 3 connected to the turbine housing 2 via a bearing housing 4. The turbine housing 2, the compressor housing 3 and the bearing housing 4 are disposed along an axis Z. The turbine housing 2 is shown in a partially sectional view. The shaft 5 here connects a turbine wheel 10 to a compressor wheel 6. A variable turbine geometry, which has a plurality of adjustable blades 8 that are distributed across the circumference and have corresponding rotation axes, is disposed on the turbine side by means of a blade bearing ring 7. As a result, nozzle cross sections are formed which are larger or smaller depending on the position of the adjustable blades 8 and via which the exhaust gas of an engine supplied via a supply duct 11 and discharged via a central port impinges to a greater or lesser extent the turbine rotor 10 situated in the center on the axis Z, in order, via the turbine rotor 10, to drive the compressor wheel 6. To control the movement or the position of the adjustable blades 8, an activation installation or an actuator is provided, which may be designed for example as an electric actuator or as a pneumatic actuator. The activation installation can set in a slight rotating movement an adjustment ring 9 which lies behind the blade bearing ring 7.

[0038] It goes without saying that charging devices 1, as are schematically illustrated in FIG. 1 for the purpose of explanation, generally comprise even further components in order to be able to be used in an internal combustion engine. A charging device 1 of this type is also referred to as a VTG charger.

[0039] The design embodiment of the compressor wheel 6 according to the invention, which can be used in the charging device 1, will now be described below in more detail. However, a compressor wheel 6 according to the invention can also be used in an electrically assisted turbocharger (also referred to as an E-Turbo) or an electrically driven compressor. Besides the use in a charging device, the compressor wheel 6 according to the invention can also be used in an air supply to a fuel cell or else in a recuperation fan of a fuel cell.

[0040] The compressor wheel 6 is illustrated in a perspective lateral view in FIG. 2. It can be seen that the compressor wheel 6 has rotor blades or blades 12 which are preferably equidistantly spaced apart and disposed on a hub 16 provided with a bore 14.

[0041] The hub 16 has a rotationally symmetrical portion and a non-rotationally symmetrical portion. The non-rotationally symmetrical portion in FIG. 2 is identified by means of the reference sign 18. This here is thus a region of a greater thickness such that the hub is thickened or raised in comparison to the planar rear side 20. The term rotationally symmetrical here refers to the rotation axis 22 which is established in the center of the bore 14 through the shaft. The rotationally symmetrical portion 18′ and the non-rotationally symmetrical portion 18 of the hub 16 are conjointly formed in a milling process. The thickening about the non-rotationally symmetrical portion 18 in the compressor wheel 6 according to the invention is configured on the suction side of the blade 12.

[0042] The suction side here is understood to be the side of the blade 12 that is visible from the inflow direction of the compressor wheel 6. The opposite side in this instance is correspondingly the pressure side. The suction side is provided with the reference sign 24 in FIG. 2, while the pressure side is provided with the reference sign 26.

[0043] The transition between the blade 12 on the suction side 24 and the non-rotationally symmetrical portion 18 of the hub 16 in the case of the compressor wheel 6 according to FIG. 2 is embodied with a constant-radius connection 28. This also applies to the transition of the blade 12 on the pressure side 26. The transition between the blade 12 and the hub 16 is thus embodied by way of constant radiusing. The previously required variable radiusing on the blade is replaced by a non-rotationally symmetrical portion of the hub. However, it is also possible for variable radiusing to be provided here instead of the constant-radius connection.

[0044] This is shown once again in a different illustration in FIG. 3. A further embodiment of a compressor wheel 6 according to the invention is shown with reference to FIG. 3A, FIG. 3B and FIG. 3C. A partially cut-away, perspective lateral view of the compressor wheel 6 is illustrated in FIG. 3A. A detail in the region of the non-rotationally symmetrical portion 18 is illustrated once again in an enlarged manner in FIG. 3B. The detail from FIG. 3B is shown in a non-cut-away illustration in FIG. 3C. It can be seen from FIGS. 3A to 3C that the radius 30, or else the width, of the non-rotationally symmetrical portion 18 varies across the length of the hub 16.

[0045] In comparison thereto, a compressor wheel 32 of identical construction, with variable radiusing 34 is shown in a partially cut-away perspective lateral view in FIG. 4A and in a detail from the latter in FIG. 4B.

[0046] A yet again further embodiment of a compressor wheel 6 according to the invention is shown with reference to FIG. 5A and FIG. 5B. FIG. 5A here again corresponds to a partially cut-away, perspective lateral view, and FIG. 5B corresponds to a detail of the latter. In this example, the radii 30 along the hub 16 are configured with less dissimilarity than in comparison to the embodiment according to FIGS. 4A, 4B and 4C. By virtue of the compressor wheel 6 being produced by means of a milling process, the surface contours of the different compressor wheels 6 shown are moreover also superimposed by milling grooves which for the sake of simplicity have been omitted in the idealized illustrations of the embodiments discussed.

[0047] Rotationally symmetrical hubs which have been embodied with a variable connection to the blade have been used in compressor wheels known in the prior art to date. The variable connection can take place by way of a radius which is configured so as to be variable over the flow direction. According to the invention, the rotationally symmetrical portion 18′ of the hub is followed by a non-rotationally symmetrical portion 18 that is formed by a radius 30 which is variable in the flow direction. The radiused connection 28, which is likewise formed by a radius that is constant over the flow direction, adjoins the non-rotationally symmetrical portion 18.

[0048] The features specified above and in the claims and shown in the figures can be advantageously implemented both individually and in various combinations. The invention is not restricted to the exemplary embodiments described, but may be modified in various ways within the scope of the abilities of a person skilled in the art.

LIST OF REFERENCE SIGNS

[0049] 1 Charging device

[0050] 2 Turbine housing

[0051] 3 Compressor housing

[0052] 4 Bearing housing

[0053] 5 Shaft

[0054] 6 Compressor wheel

[0055] 7 Vane bearing ring

[0056] 8 Adjustable blades

[0057] 9 Adjusting ring

[0058] 10 Turbine wheel

[0059] 11 Supply duct

[0060] 12 Vane

[0061] 14 Bore

[0062] 16 Hub

[0063] 18 Non-rotationally symmetrical portion

[0064] 18′ Rotationally symmetrical portion

[0065] 20 Rear side

[0066] 22 Rotation axis

[0067] 24 Suction side

[0068] 26 Pressure side

[0069] 28 Radiused connection

[0070] 30 Radius

[0071] 32 Compressor wheel

[0072] 34 Radiusing