The invention relates to an exhaust-gas turbocharger according to the preamble of claim 1.
In the case of such an exhaust-gas turbocharger, provision is made of a variable turbine geometry (VTG), in which guide vanes are adjusted by means of a unison ring, which can be rotated by means of an adjusting shaft.
It is an object of the present invention to provide an exhaust-gas turbocharger of the type described in the preamble of claim 1, in which the bearing forces in the system of the VTG and in particular of the adjusting shaft can be reduced.
This object is achieved by the features of claim 1.
The dependent claims contain advantageous developments of the invention.
Claims 7 and 8 define a VTG cartridge according to the invention as an object which can be marketed independently.
Further details, features and advantages of the invention become apparent from the following description of exemplary embodiments with reference to the drawing, in which:
The exhaust-gas turbocharger 1 also has a turbine 2, which comprises a turbine wheel 3 surrounded by an intake duct 4, which is provided with a so-called VTG cartridge 5. This VTG cartridge 5 will be described in detail hereinbelow with reference to
The exhaust-gas turbocharger 1 also of course has all the other common parts of an exhaust-gas turbocharger, such as a rotor 20, which is mounted rotatably in a bearing housing 21 and which bears the turbine wheel 3 at one end and a compressor wheel 19 of a compressor 18 at the other end. These parts are likewise shown only in schematically greatly simplified form in
The VTG cartridge, which, as mentioned, will be explained in detail hereinbelow with reference to
A VTG cartridge is understood to mean a structural unit which, between a vane bearing ring 7 and a disk 6, delimits an intake duct 4 for the passage of exhaust gases to the turbine wheel 3. Furthermore, a VTG cartridge 5 of this type has a plurality of vanes, which are arranged in the intake duct 4 and of which
Each vane lever 10 has a lever head 11, which engages into an associated groove 12 in a unison ring 13.
For radially mounting the unison ring 13, provision is made of a radial bearing, which according to the invention is formed by the vane levers 10. For this purpose, the vane levers 10 are formed as rolling levers, the lever heads 11 of which are supported in the grooves 12 in the unison ring 13.
As can be seen when
However,
As can also be seen from
The adjusting lever 14 also has a second end region 14B, which is arranged adjacent to the vane bearing ring 7, in particular above the vane bearing ring 7, and is provided with a recess 17 in which the adjusting shaft 15 is fixed. In
In addition to the above written disclosure, reference is hereby explicitly made to the illustrative representation of the invention in
1 Exhaust-gas turbocharger
2 Turbine
3 Turbine wheel
4 Intake duct
5 VTG cartridge
6 Disk
7 Vane bearing ring
8 Vanes
9 Vane shafts
10 Vane levers
11 Lever heads
12 Grooves
13 Unison ring
14 Adjusting lever
14A, 14B End regions of the unison ring
15 Adjusting shaft
16 Groove
17 Positioning pin
L Charger longitudinal axis
Number | Date | Country | Kind |
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10 2012 008 588 | Apr 2012 | DE | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2013/037328 | 4/19/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2013/163024 | 10/31/2013 | WO | A |
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2008075635 | Apr 2008 | JP |
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Entry |
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International Search Report in International Application No. PCT/US2013/037328 dated Jul. 29, 2013. |
Number | Date | Country | |
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20150086340 A1 | Mar 2015 | US |