The invention relates to an exhaust-gas turbocharger as per the preamble of claim 1.
An exhaust-gas turbocharger of said type is known from DE 10 2008 053 079 A1. In said known design, a coupling rod connects the actuator (for example an electric actuator or a pneumatic control capsule) to the assembly of an adjusting shaft of a variable turbine geometry (VTG), also referred to as a guide grate. Here, the coupling rod transmits the movement generated by the actuator to the VTG. Instead of a VTG or in addition to the VTG, the use of a coupling rod is also possible in the case of an exhaust-gas turbocharger with a wastegate, which constitutes a turbine bypass. Here, the coupling rod is mounted on a pin assigned to the actuator and on a pin assigned to the adjusting shaft and is secured by means of a lock washer. The known lock washers have the disadvantage, however, that as a result of the difficult mounting process, the clipping thereof to the pin diameter cannot be ensured in a reliable manner in terms of a process.
It is therefore an object of the present invention to provide an exhaust-gas turbocharger of the type specified in the preamble of claim 1 which permits simpler mounting of its coupling rod between the actuator and variable turbine geometry (VTG) and/or wastegate.
Said object is achieved by means of the features of claim 1.
By virtue of the fact that the lock washers at the two ends of the coupling rod are components which are integrated in the coupling rod, the invention makes it possible during assembly for the coupling rod together with the integrated lock washers to be mounted in one working step.
The subclaims relate to advantageous refinements of the invention.
Claims 11 and 12 define a coupling rod as an object that can be marketed independently.
Further details, features and advantages of the invention will emerge from the following description of an exemplary embodiment on the basis of the drawing, in which:
To control the movement or the position of the adjustable blades 7, an actuating device or an actuator 11 is provided which may for example be in the form of an electric actuator or pneumatic control capsule. In the embodiment illustrated, the actuating device 11 has a control housing 12 and a coupling rod 14 in order to transmit the movement thereof to an adjusting ring 5 situated behind the blade bearing ring 6, said movement being converted into a slight rotational movement of said adjusting ring. Between the blade bearing ring 6 and an annular part 15 of the turbine housing 2 there is formed a free space 13 for the adjustable blades 7. To be able to safeguard said free space 13, the blade bearing ring 6 has spacers 16. The free space for the adjustable blades 7 is delimited in the upward direction above the spacers 16 by a receiving disk 19.
The coupling rod 14 which is only partially visible in
The end regions 21 and 22 are each provided with passage recesses 23 and 24 respectively.
As shown in particular in
If the coupling rod 14 is a metal rod, the integration of the lock washers 25 and 26 may be realized by calking or welding of the edge regions.
As can also be seen from
Furthermore, the particularly preferred embodiments of the lock washers 25 and 26 as per
In the mounted state illustrated in
In addition to the above written disclosure of the invention, reference is hereby explicitly made to the diagrammatic disclosure thereof in
1 Exhaust-gas turbocharger
2 Turbine housing
3 Compressor housing
4 Turbine wheel
5 Adjusting ring
6 Blade bearing ring
7 Adjustable blades
8 Rotary shafts
9 Supply duct
10 Axial connecting piece
11 Actuating device/Actuator
12 Control housing
13 Free space for guide blades 7
14 Coupling rod
15 Annular part of the turbine housing 2
16 Spacer/Spacer cam
17 Compressor wheel
18 Variable turbine geometry VTG/Guide grate
19 Depression
20 Bearing housing
21, 22 End regions
23, 24 Passage recesses
23′ Connecting region
25, 26 Lock washers
27 Through opening
28, 29, 30, 31 Slots
32 Edge region/Outer edge
33 Pin
R Axis of rotation
Number | Date | Country | Kind |
---|---|---|---|
10 2011 109 742.6 | Aug 2011 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US2012/047952 | 7/24/2012 | WO | 00 | 1/28/2014 |