Exhaust-gas turbocharger

Abstract

An exhaust-gas turbocharger (1) having a compressor housing (2) in which a compressor wheel (2) is arranged; a bearing housing (3); and a turbine housing (4) in which a turbine wheel (4) is arranged. The axial abutment surfaces (5, 6) are provided between the bearing housing (3) and the turbine housing (4). The axial abutment surfaces (5, 6) have at least one notch (9).

Claims

1. An exhaust-gas turbocharger (1) having: a compressor housing (2) in which a compressor wheel (2) is arranged; a bearing housing (3), the bearing housing including a turbine housing facing axial abutment surface (6); a turbine housing (4) in which a turbine wheel (4) is arranged, the turbine housing (4) including a bearing housing facing axial abutment surface (5); and means for mounting the turbine housing (4) axially tightly to the bearing housing (3), wherein at least one of the turbine housing facing axial abutment surface (6) of the bearing housing (3) and the bearing housing facing axial abutment surface (5) turbine housing of the (4) is provided with a notch, wherein the turbine housing facing axial abutment surface (6) of the bearing housing (3) is spaced apart from bearing housing facing axial abutment surface (5) of the turbine housing (4) by at least one thermal insulator (10) which is arranged in the notch such that the thermal insulator (10) prevents direct contact between the axial abutment surfaces (5, 6) and such that any transmission of axial force between the bearing housing (3) and the turbine housing (4) takes place via the thermal insulator (10).

2. The exhaust-gas turbocharger as claimed in claim 1, wherein the thermal insulator (10) is ceramic.

3. The exhaust-gas turbocharger as claimed in claim 1, wherein the thermal insulator (10) is constructed from a multiplicity of separate segments.

4. The exhaust-gas turbocharger as claimed in claim 1, wherein the thermal insulator (10) extends radially inward behind the turbine wheel (4).

5. The exhaust-gas turbocharger as claimed in claim 1, wherein a further thermal insulator is provided which is arranged behind the turbine wheel (4).

6. The exhaust-gas turbocharger as claimed in claim 1, having a radial centering surface pairing (7, 8) formed by a multiplicity of centering lobes (11-15).

7. The exhaust-gas turbocharger as claimed in claim 6, wherein a clearance (17) is arranged between the centering lobes (11-15).

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

(1) FIG. 1 shows a schematically slightly simplified sectional illustration through an exhaust-gas turbocharger according to the invention,

(2) FIG. 2 shows an illustration, corresponding to FIG. 1, of a sub-region of the bearing housing and of the turbine housing according to a second embodiment of the exhaust-gas turbocharger according to the invention, and

(3) FIG. 3 shows a slightly simplified perspective detail illustration of a centering lobe arrangement.

DETAILED DESCRIPTION OF THE INVENTION

(4) The exhaust-gas turbocharger 1 illustrated in FIG. 1 has a compressor housing 2 with a compressor wheel 2 arranged therein, a bearing housing 3, and a turbine housing 4, said housings being mounted on one another. The bearing housing 3 serves for mounting a shaft 12 which, on one end, bears the compressor wheel 2 and, on its other end, bears a turbine wheel 4 which is arranged in the turbine housing 4.

(5) The turbine housing 4 has a turbine-housing-side axial abutment surface 5. The bearing housing 3 has a bearing-housing-side axial abutment surface 6.

(6) Furthermore, there is a centering surface pairing formed by a turbine-housing-side centering surface 7 and a bearing-housing-side centering surface 8.

(7) It can be seen from FIG. 1 that the axial abutment surfaces 5, 6 have a notch 9 in which, in the particularly preferred embodiment illustrated in FIG. 1, there is arranged a thermal insulator 10 which may be constructed for example from ceramic material. As explained in the introduction, it would basically also be conceivable to provide only the notch 9 without the thermal insulator 10, which in itself would result in a reduction of the introduction of heat into the bearing housing 3 because a heat-transmitting contact surface between the axial abutment surfaces 5, 6 can be reduced in size simply by means of a notch 9 of said type.

(8) The embodiment illustrated in FIG. 1 is however preferable owing to the provision of a thermal insulator 10, because, by means of said thermal insulator 10, contact between the abutment surfaces 5 and 6 can be prevented, as emerges from the illustration of FIG. 1. In this case, the transmission of force between the bearing housing 3 and the turbine housing 4 takes place via the thermal insulator 10, as illustrated in FIG. 2.

(9) Here, FIG. 2 shows that it is possible for the thermal insulator 10 to be of such a size that, as viewed in the radial direction R of the exhaust-gas turbocharger 1, it extends behind the turbine wheel 4, which permits a further reduction of the transfer of heat into the bearing housing 3.

(10) The radial centering surface pairing 7, 8 may be in the form of a centering lobe arrangement, wherein in FIG. 1, owing to the selected illustration, one centering lobe 11 is visible.

(11) It would however be preferable, as shown in FIG. 3, for four such centering lobes 12, 13, 14 and 15, for example, to be provided, which centering lobes may be arranged in each case separately from one another on the turbine housing 4 or on the bearing housing 3. The clearance generated by said arrangement is denoted in FIG. 1 by the reference sign 17.

(12) In addition to the above written disclosure of the invention, reference is hereby explicitly made to the illustrative representation in FIGS. 1 to 3 to supplement the disclosure.

LIST OF REFERENCE SIGNS

(13) 1 Exhaust-gas turbocharger 2 Compressor 2 Compressor wheel 3 Bearing housing 4 Turbine housing 4 Turbine wheel 5 Turbine-housing-side abutment surface 6 Bearing-housing-side abutment surface 7 Turbine-housing-side radial centering surface 8 Bearing-housing-side centering surface 9 Notch (groove) 10 Thermal insulator 11-15 Centering lobes 16 Shaft 17 Clearance R Radial direction