The invention relates to a turbocharger as per the preamble of claim 1.
A turbocharger of said type is known from DE 10 2006 038 830 A1. Said turbocharger has a silencer in order to be able to at least lessen the occurrence of acoustic disturbances which can occur as a result of high-frequency flow noises, which may be caused for example by geometric irregularities. In unfavorable inflow situations, however, very noticeable tones can be generated by the silencer itself. A conventional silencer is composed of an air-guiding duct which is traversed by flow and to which hydraulic buffer chambers or ducts for producing buffer volumes can be coupled. The connecting points between the air-guiding duct and the buffer chambers or the ducts have a considerable thickness and sharp edges, in particular in the case of injection-molded parts. Said noticeable tones can therefore be generated by the silencer itself at the sharp edges.
It is therefore an object of the present invention to provide a turbocharger of the type specified in the preamble of claim 1, by means of which it is possible to reduce or completely eliminate tones generated by the silencer.
Said object is achieved by means of the features of claim 1.
By eliminating a sharp-edged radially inner corner, it is possible for the generation of noticeable tones by the silencer itself to be prevented without impairing the actual function of the silencer.
Subclaims 2 to 8 relate to advantageous refinements of the invention.
Claims 9 and 10 define a silencer as an object which can be marketed separately.
The radially inner corner of the edge of the opening from the air-guiding duct to the buffer chamber may be formed for example as a rounding, as a bevel or as an inwardly directed bulge.
Here, tests carried out within the context of the invention have yielded that, surprisingly, simply machining said radially inner edge makes it possible to effectively suppress the tone generation by the silencer itself.
Further details, advantages and features of the present invention will emerge from the following description of exemplary embodiments on the basis of the drawing, in which:
All the other components of the turbocharger 1 illustrated by way of example will not be described in detail below because they are not required for explaining the principles of the present invention. For the explanation of the reference symbols used in
Arranged in the silencer housing 23 is an insert part 25 which has a tubular base part 37 which is provided with a spacer 38, which in the example is in the shape of a disk, for forming a buffer chamber 24. The insert part 25 may be fixed in the silencer housing 23 by means of a suitable retaining device 39 with the interposition of a sealing ring 40. The base part 37 is provided at least with one opening, but generally with two or three openings 26, which connect an air-guiding duct 27 arranged in the base part 37 to the buffer chamber 24.
The opening 26 has an edge 28 which is provided with a radially inner corner 29. The edge 28 also has a radially outer corner 29′, wherein
As is also shown in
Furthermore, the silencer housing 23 is provided, on its other end region 34, with a connecting piece 33 in which, in the example, a further insert part 35 with slots is arranged, one of which slots is denoted, representatively for all of the slots, by the reference numeral 36. Said insert part 35 likewise serves as a silencer. A line to the charge-air cooler, if one is provided, or to the engine may be connected to the connecting piece 33.
To be able to prevent the generation of disturbance noises by the silencer 21 itself, the radially inner corner 29 thereof is machined in order to eliminate a sharp-edged design.
All of said designs can prevent the occurrence of disturbance noises, since the sharp edge of the radially inner corner 29 of the edge 28 is eliminated.
In addition to the above written disclosure of the invention, reference is hereby made explicitly to the diagrammatic illustration thereof in
1 Turbocharger/exhaust-gas turbocharger
2 Turbine housing/turbine
3 Compressor housing/compressor
4 Turbine wheel
5 Adjusting ring
6 Blade bearing ring
7 Guide blades
8 Blade shaft
9 Supply duct
10 Axial connecting piece
11 Actuating device
12 Control capsule
13 Free space for guide blades 7
14 Plunger element
15 Annular part of the turbine housing 2
16 Spacer/spacer cam
17 Compressor wheel
18 Guide grate/guide apparatus
19 Bearing housing
20 Compressor outlet
21 Silencer
22 First end region
23 Silencer housing
24 Buffer chamber/buffer volume
25 Insert part
26 Opening
27 Air-guiding duct
28 Edge
29 Radially inner corner
29′ Radially outer corner
30 Rounding
31 Bevel
32 Bulge
33 Connecting piece
34 Second end region
35 Insert part
36 Slot
37 Base part
38 Spacer
39 Retaining device
40 Sealing ring
41 Pipe piece
42 Buffer chamber
43 Outer wall
L Longitudinal central line of the silencer housing 23
R Radius
Number | Date | Country | Kind |
---|---|---|---|
102010033966.0 | Aug 2010 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US2011/046528 | 8/4/2011 | WO | 00 | 1/30/2013 |