SUPERCHARGING DEVICE

Abstract

A supercharging device, for example an exhaust gas turbocharger, may include a rotor mounted in a housing via an axial bearing. The axial bearing may include an axial bearing disc, a membrane, and a screw connection that secures the axial bearing disc to the membrane through an opening in the membrane. The axial bearing may further include a bush connected to the housing. The membrane may be clamped in between the bush and the housing. An adjusting screw may be inserted into an opening of the bush. The adjusting screw may delimit and/or facilitate an axial movement of the screw connection and the axial bearing disc.

Claims

1. A supercharging device comprising: a rotor mounted in a housing; the rotor mounted in the housing via an axial bearing disposed on an end side of the rotor; the axial bearing including: an axial bearing disc with a first bearing surface; a membrane with a central first opening; a screw connection that secures the axial bearing disc to the membrane through the central first opening; a bush with a central second opening, wherein the bush is connected to the housing and the membrane is clamped in between the bush and the housing; and an adjusting screw screwed into the central second opening of the bush, wherein the adjusting screw delimits and facilitates an axial movement of the screw connection and the axial bearing disc.

2. The supercharging device according to claim 1, wherein the axial bearing disc has a truncated cone-like shape and the first bearing surface is arranged spaced via a gap from a second bearing surface of the rotor disposed opposite the first bearing surface.

3. The supercharging device according to claim 1, wherein the screw connection includes a washer.

4. The supercharging device according to claim 3, wherein the washer is arranged on a side of the membrane facing away from the rotor.

5. The supercharging device according to claim 1, wherein the membrane is clamped in entirely over a circumference directly or indirectly between the bush and the housing.

6. The supercharging device according to claim 1, wherein the supercharging device is an exhaust gas turbocharger.

7. The supercharging device according to claim 1, further comprising a cover disc arranged between the bush and the membrane.

8. The supercharging device according to claim 1, wherein the bush is a threaded bush including an external thread and the housing includes an associated internal thread.

9. The supercharging device according to claim 1, further comprising an adjusting device for turning the adjusting screw.

10. The supercharging device according to claim 1, wherein the axial bearing disc includes a graphite material, the graphite material including one or more fillings.

11. The supercharging device according to claim 10, wherein the one or more fillings of the graphite material include at least one of antimony, copper and silver.

12. The supercharging device according to claim 1, wherein the axial bearing disc includes a copper material and a graphite coating disposed on the copper material.

13. The supercharging device according to claim 12, wherein the copper material is a copper alloy.

14. The supercharging device according to claim 1, wherein the bush is screwed to the housing.

15. The supercharging device according to claim 1, wherein the axial bearing disc has a truncated cone shape and the first bearing surface is arranged spaced via a gap from a second bearing surface of the rotor disposed contacting the first bearing surface.

16. The supercharging device according to claim 1, wherein the rotor defines a rotation axis and the axial bearing is disposed on an axial end side of the rotor.

17. The supercharging device according to claim 1, wherein the membrane is clamped only in at least three locations between the bush and the housing.

18. The supercharging device according to claim 1, wherein the axial bearing disc is screwed via the screw connection to the membrane through the central first opening.

19. The supercharging device according to claim 1, further comprising a radial bearing element mounting the rotor in the housing in a radial direction of the rotor.

20. An exhaust gas turbocharger, comprising: a rotor defining a rotation axis; a housing; an axial bearing disposed on an axial end side of the rotor with respect to the rotation axis, the rotor mounted in the housing via the axial bearing, the axial bearing including: an axial bearing disc having a first bearing surface; a membrane having a central first opening; a screw connection that secures the axial bearing disc to the membrane through the central first opening; a bush having a central second opening, wherein the bush is connected to the housing and the membrane is clamped in between the bush and the housing; and an adjusting screw disposed in the central second opening of the bush, wherein the adjusting screw delimits and facilitates an axial movement of the screw connection and the axial bearing disc.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0018] There it shows, in each case schematically,

[0019] FIG. 1A illustrates a sectional representation through a supercharging device according to the invention in the region of an axial bearing,

[0020] FIG. 1B illustrates an exploded representation of FIG. 1A,

[0021] FIG. 2A illustrates a representation as in FIG. 1A, however with an alternative embodiment of the axial bearing,

[0022] FIG. 2B illustrates an oblique view of the sectional representation according to FIG. 2A,

[0023] FIG. 3A illustrates a representation as in FIG. 2A, however with an alternative embodiment of the screw connection,

[0024] FIG. 3B illustrates an oblique view of the sectional representation according to FIG. 3A,

[0025] FIG. 4A illustrates a representation as in FIG. 3A according to an example,

[0026] FIG. 4B illustrates a detail A of the representation of FIG. 4A,

[0027] FIG. 5A illustrates a further embodiment with a cup for the aerodynamically favourable covering of the axial bearing,

[0028] FIG. 5B illustrates an oblique view of the sectional representation according to FIG. 5A,

[0029] FIG. 6 illustrates an exploded representation of FIG. 5B,

[0030] FIG. 7 illustrates a sectional representation through a supercharging device with an axial bearing according to the invention on only one side,

[0031] FIG. 8 illustrates a sectional representation through a supercharging device with axial bearings according to the invention arranged on both sides,

[0032] FIG. 9 illustrates a sectional representation through a supercharging device with an axial bearing according to the invention on the compressor side.

DETAILED DESCRIPTION

[0033] According to FIGS. 1 to 9, a supercharging device 1 according to the invention, for example an exhaust gas turbocharger 2, comprises a rotor 4 mounted in a housing 3. Here, the rotor 4 is mounted on the longitudinal end side in an axial bearing 6 on the end side in the housing 3 via suitable bearing sections 5. The axial bearing 6 according to the invention comprises the following components: an axial bearing disc 7 with a first bearing surface 8, a membrane 9 with a central first opening 10, a screw connection 11, via which the axial bearing disc 7 is screwed to the membrane 9 through the central first opening 10, a bush 12 with a central second opening 13, wherein the bush 12 is connected, in particular screwed to the housing 3 and the membrane 9 is either directly clamped in between the bush 12 and the housing 3 (see FIG. 1) or indirectly via a cover disc 14 (see FIGS. 2 and 3) arranged between the bush 12 and the membrane 9. Here, the bush 12 can be designed as a threaded bush with an external thread while the housing 3 has an associated internal thread (see FIGS. 2 to 8) or is screwed to the housing 3 via screws 25 or connected to the same in another way (see FIGS. 1 and 9). In addition, the axial bearing 6 according to the invention comprises an adjusting screw 21, which is screwed into the central second opening 13 of the bush 12 and depending on position, delimits or makes possible an axial movement of the screw connection 11 in axial direction, i.e. along an axis of rotation 17. By way of the adjusting screw 21 it is also possible to tension the membrane 9 and/or adjust a rotor position and an axial gap between a compressor wheel 31 and a compressor housing 32 and/or an axial gap between a turbine wheel 33 and a turbine housing 34. The axial bearing disc 7 can for example comprise graphite or be formed thereof. The graphite in turn can have various fillings or cores, for example of antimony, copper or silver. The axial bearing disc 7 can also be produced from copper or a copper alloy and have a graphite coating.

[0034] Looking at FIGS. 1 to 9 further, it is evident that the axial bearing disc 7 has a truncated cone-like shape and with its first bearing surface 8 is arranged spaced via a gap 15 from a second bearing surface 16 (see in particular FIG. 3) of the rotor located opposite. With the moveably mounted axial bearing disc 7 according to the invention, i.e. in the stator of the axial bearing 6, it is possible to easily offset deviations with respect to an axis of rotation 17 between the rotor 4 and the axial bearing disc 7 and thereby comparatively easily compensate in particular production inaccuracies. With the at least slightly tiltable axial bearing disc 7, uneven temperature strain of the housing 3 can additionally be offset since the axial bearing disc 7 is no longer rigidly connected to the housing. In order to be able to further increase the flexibility of the adjusting possibility of the axial bearing disc 7, the membrane 9 can comprise at least one through-opening 18, which as cross-sectional weakening, reduces the stiffness of the membrane 9.

[0035] Looking at the supercharging device 1 according to FIGS. 1 to 9 further, it is evident that in the housing 3 a radial bearing element 19 is arranged, which brings about a radial mounting of a bearing section 5 and additionally of the rotor 4 and which is fixed on the housing via a radial screw 20 (see FIG. 1) that is accessible from the outside.

[0036] Here, the membrane 9 can be clamped in either over its entire circumference between the housing 3 and the bush 12 (see FIG. 1) or the cover disc 14 (see FIGS. 2 and 3) or only in suitable sections. Because of this, the stiffness of the membrane 9 can also be influenced in a comparatively easy manner. It is conceivable for example that the membrane 9 is clamped in between the bush and the housing 3 or between the cover disc 14 and the housing 3 only in at least three locations.

[0037] In the case of air mounting of rotors 4 it is generally important that both parts of the bearing device, here of the axial bearing 6, i.e. both rotor 4 and also the fixed axial bearing disc 7 (stator) are aligned parallel to one another to the maximum possible. Even a relatively minor tilting of both of these planes in this case results in a deterioration or even a complete loss of the load carrying capacity of the bearing or of the axial bearing 6. Through the axial bearing 6 according to the invention, which comprises a tiltable axial bearing 7 which is thus not arranged fixed on the housing 3, a resilient design can be achieved with which it is possible, in particular, to compensate form instabilities for example because of different heat strain. In order to fix the rotor 4 in axial direction, i.e. in the direction of the axis of rotation 17, the adjusting screw is provided.

[0038] The air cushion between the two bearing surfaces 8, 16 required for the air mounting of the rotor 4 in axial direction in this case can be favoured via suitable grooves 22 (see FIG. 3) or other flow guiding elements. Here, the grooves 22 can be arranged either on the first bearing surface 8 of the axial bearing disc 7 and/or on the second bearing surface 16 of the rotor 4.

[0039] For locking the adjusting screw 21 in axial direction, lock nuts 23 can obviously be additionally provided. In addition, the screw connection 11 can comprise a washer 24 which on the one hand is able to resiliently preload the axial bearing 7 against the membrane 9 by means of the screw connection 11. Here, the washer 24 is arranged on the side of the membrane 9 facing away from the rotor 4.

[0040] Preferentially, an adjusting device 28 for turning the adjusting screw 21 and thus for adjusting the axial bearing 6 is additionally provided. The adjusting device 28 can for example be an electric motor or an electric control which opens up the possibility of changing or regulating an axial gap between the compressor wheel and the compressor housing during operation. This would have a very good thermodynamic influence. Such an adjusting device 28 is shown only highly schematically in FIG. 1, wherein in this case obviously the lock nuts 23 would not be present.

[0041] Looking at the FIGS. 2 and 3 in comparison it is evident that according to FIG. 2 a ball segment-like extension 26 is provided on the adjusting screw 21, while this ball segment-like extension 26 according to the embodiment of FIG. 3 is arranged on the screw of the screw connection 11. The last mentioned version is likely to be preferred, both alternative embodiments having in common that only a very small and low-friction contact surface to the screw of the screw connection 11 (see FIG. 2) or to the adjusting screw 21 (see FIG. 3) is created via the ball segment-like extension 26.

[0042] In FIG. 4, a detail A on an outer edge of the membrane 9 is shown, wherein it is evident that here the housing 3 has an annular recess 27, as a result of which the membrane 9 can make better contact.

[0043] In the FIGS. 5 and 6 an embodiment is shown, in which a cup 29 for the aerodynamically favourable covering of the axial bearing 6 is provided. This cup 29 is simply pressed into an associated opening 30 of the housing 3. The cup 29 can for example be formed as a cost-effective plastic injection moulding, provided it is arranged on the compressor side.

[0044] FIG. 7 shows a sectional representation through a supercharging device 1 with an axial bearing 6 according to the invention arranged on the turbine side. On the compressor side (left) by contrast an axial bearing which is fixed in axial direction is provided. Compared with this, FIG. 9 shows a sectional representation through a supercharging device 1 with an axial bearing 6 according to the invention arranged on the compressor side. On the turbine side (left) by contrast an axial bearing that is fixed in axial direction is provided. Alternatively it is obviously also conceivable that an axial bearing 6 according to the invention is arranged on both the compressor side and also on the turbine side, as is shown in FIG. 8.

[0045] Generally it is possible to connect the bush 12 on the housing 3 via separate fastening screws 25 (see FIG. 1), wherein in this case the fastening screws 25 penetrate the bush 12. Alternatively it is also conceivable that the bush 12 has an external thread via which it can be screwed into a corresponding internal thread on the housing 3, as is shown according to FIGS. 2 to 8.

[0046] With the axial bearing 6 according to the invention it is possible for the first time to simply offset temperature or production-related axial deviations between the rotor 4 and the axial bearing disc 7 since the latter is not arranged in a fixed manner on the housing 3 as in the past, but at least slightly moveably on the membrane 9.