Exhaust-gas turbocharger

Abstract

An exhaust-gas turbocharger (1) having a compressor housing (2); a turbine housing (3); and a bearing housing (4) which has a compressor-side flange (5) and which has a turbine-housing-side flange (6). The turbine-housing-side flange (6) is produced from a material which corresponds in terms of its mechanical and thermal properties to the material of the turbine housing (2).

Claims

1. An exhaust-gas turbocharger (1) having a compressor housing (2); a turbine housing (3) having a bearing-housing-side flange having a planar contact surface; and a bearing housing (4) which has a compressor-side flange (5) and which has a turbine-housing-side flange (6) as a separately produced component which is connected to the bearing housing (4) and has a planar contact surface adapted to mating to the planar contact surface of the turbine housing (3) bearing-housing-side flange, wherein the turbine housing is formed of a material adapted to withstand exhaust-gas temperatures and thermal variations, the turbine-housing-side flange (6) of the bearing housing (4) is produced from steel and the remainder of the bearing housing (4) is produced from iron.

2. The exhaust-gas turbocharger as claimed in claim 1, wherein the turbine-housing-side flange (6) is connected to the bearing housing (4) by means of a screw connection, a shrink fit, welding, adhesive bonding, soldering or composite casting or combinations of these connection types.

3. The exhaust-gas turbocharger as claimed in claim 1, wherein the material of the bearing housing (4) turbine-housing-side flange (6) is a ferritic steel.

4. The exhaust-gas turbocharger as claimed in claim 1, wherein the material of the bearing housing (4) turbine-housing-side flange (6) is an austenitic steel.

5. The exhaust-gas turbocharger as claimed in claim 1, wherein the bearing housing other than the turbine-housing-side flange (6) is a cast part composed of a pearlitic microstructure.

6. A bearing housing (4) for an exhaust-gas turbocharger (1), having a compressor-housing-side flange (5) and a turbine-housing-side flange (6), wherein the bearing housing other than the turbine-housing-side flange (6) is a cast part composed of a pearlitic microstructure, and wherein the turbine-housing-side flange (6) is a separately produced component which is connected to the bearing housing (4) and is produced from a high-temperature-resistant ferritic or from an austenitic cast steel.

7. The bearing housing as claimed in claim 6, wherein the turbine-housing-side flange (6) is connected to the bearing housing (4) by means of a screw connection, a shrink fit, welding, adhesive bonding, soldering or composite casting or combinations of these connection types.

Description

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

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

(3) FIG. 2 shows a plan view of the bearing housing of the exhaust-gas turbocharger as viewed from the turbine,

(4) FIG. 3 shows a section through the bearing housing along the line A-A in FIG. 2,

(5) FIG. 4 shows a perspective illustration of a further embodiment of the bearing housing according to the invention,

(6) FIG. 5 shows a sectional illustration, corresponding to FIG. 3, of the bearing housing as per FIG. 4,

(7) FIG. 6 shows a partial view of the bearing housing as per FIG. 4,

(8) FIG. 7 shows an illustration, corresponding to FIG. 4, of a further embodiment of the bearing housing according to the invention,

(9) FIG. 8 shows an illustration, corresponding to FIG. 5, of the bearing housing as per FIG. 7,

(10) FIG. 9 shows an illustration, corresponding to FIG. 6, of the bearing housing as per FIG. 7,

(11) FIG. 10 shows an illustration, corresponding to FIG. 7, of a further embodiment of the bearing housing according to the invention, and

(12) FIG. 11 shows an illustration, corresponding to FIG. 8, of the bearing housing as per FIG. 10.

(13) FIG. 1 illustrates an exhaust-gas turbocharger 1 according to the invention which has a compressor 7 and a compressor housing 2.

(14) The exhaust-gas turbocharger 1 also has a turbine 8 with a turbine housing 3 and has a bearing housing 4 which is connected via a compressor-side flange 5 to the compressor 7 and via a turbine-housing-side flange 6 to the turbine 8 or the turbine housing 3.

(15) The design of the turbine-housing-side flange 6 will be explained in detail below on the basis of FIGS. 2 to 11. The exhaust-gas turbocharger illustrated in FIG. 1 self-evidently also has all the other components of such turbochargers, said components however not being described in detail because they are not required for explaining the principles of the present invention.

(16) FIGS. 2 and 3 illustrate a first embodiment of the bearing housing 6 according to the invention of the exhaust-gas turbocharger 1.

(17) The view in FIG. 2 is a view from the direction of the turbine 8, and shows the bearing housing 4 with its turbine-housing-side flange 6, wherein, owing to the selected illustration, it is possible to see an arrangement 9 composed of a bush, a lever and a pin, and also two dowel pins 10 and 11.

(18) FIG. 3 shows that the turbine-housing-side flange 6, which is formed as a separate component, is formed as a steel flange which can be either screwed or welded to the bearing housing 4. The reference numeral 14 symbolically indicates one of the possible weld points of a multiplicity of weld points.

(19) FIGS. 4 to 6 illustrate a further embodiment of the bearing housing 4 according to the invention, wherein all of the features which correspond to FIGS. 2 and 3 are denoted by the same reference numerals.

(20) In said design variant, the flange 6 is cast integrally with the bearing housing 4, wherein FIG. 5 shows that the connection is realized by means of a suitable shaping 17.

(21) FIGS. 4 and 6 furthermore show two recesses 15 and 16 which, in said embodiment, are situated entirely within the surface of the flange 6.

(22) FIGS. 7 to 9 illustrate a further design variant of an integrally cast flange 6, wherein FIG. 8 again shows the form fit 17. Said embodiment otherwise corresponds to the embodiment as per FIGS. 4 to 6, aside from the fact that FIG. 9 shows that the recesses 15 and 16 are situated partially in the material of the flange 6 and partially in the material of the bearing housing 4.

(23) FIGS. 10 and 11 show a variant which substantially corresponds to the embodiment as per FIGS. 2 and 3 and in which the flange 6 is screwed to the bearing housing 4 by means of an internal/external thread 13. The recesses 15 and 16 as per FIG. 9 serve, together with the pressed-in bush 9 or the pressed-in pin 11 (shown in FIG. 2), as a rotation prevention means.

(24) All of the above-explained design variants of the bearing housing 4 according to the invention have in common the fact that the flange 6 is matched in terms of its material properties to the material of the turbine housing 3, such that the problems explained in the introduction, in particular with regard to undesired crack formation in the region of the contact point between the bearing housing 4 and the turbine housing 3, can be eliminated.

(25) In addition to the above written disclosure of the invention, reference is hereby made explicitly to the diagrammatic illustration thereof in FIGS. 1 to 11.

LIST OF REFERENCE NUMERALS

(26) 1 Exhaust-gas turbocharger 2 Compressor housing 3 Turbine housing 4 Bearing housing 5 Compressor-side flange 6 Turbine-housing-side flange 7 Compressor 8 Turbine 9 Arrangement composed of bush, lever and pin 10, 11 Dowel pins 12 Circumferential collar 14 Weld point 13 Internal thread/external thread 15, 16 Recesses 17 Connecting device with suitable shaping (form fit) which engages into the bearing housing 4