INTAKE DEVICE FOR A COMPRESSOR
20230213009 · 2023-07-06
Inventors
Cpc classification
F02M35/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1288
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/96
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1277
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1283
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/4213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02M35/1211
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1272
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The invention relates to an intake device for a compressor. The intake device comprises a support structure having a plurality of struts which are arranged in the circumferential direction about an axis of the support structure and extend in the radial direction. Furthermore, the intake device comprises a plurality of first sound-damping elements which are arranged in the radial continuation of the plurality of struts. In addition, the intake device comprises a plurality of second sound-damping elements, each of which is arranged between adjacent first sound-damping elements. The invention furthermore relates to an exhaust-gas turbocharger having the intake device according to the invention, and an internal combustion engine having an exhaust-gas turbocharger of this kind.
Claims
1. An intake device for a compressor, comprising: a support structure having a multiplicity of struts, which are arranged around an axis of the support structure in the circumferential direction and extend in the radial direction, a multiplicity of first muffler elements, which are arranged in the radial continuation of the multiplicity of struts, and a multiplicity of second muffler elements, each of which is arranged between adjacent first muffler elements, wherein radially inwardly directed ends of the multiplicity of first muffler elements are each in contact with radially outwardly directed ends of the multiplicity of struts in such a way that a continuous flow area is formed by the side faces of the first muffler elements and the side faces of the struts, and wherein the multiplicity of second muffler elements each have a radially inner end with a taper.
2. The intake device as claimed in claim 1, wherein the radially inwardly directed ends of the multiplicity of first muffler elements are each in positive-locking contact with the radially outwardly directed ends of the multiplicity of struts.
3. The intake device as claimed in claim 1, further comprising a multiplicity of third muffler elements, which are each arranged between a first muffler element and a second muffler element, wherein the third muffler elements have a smaller radial extent than the second muffler elements.
4. The intake device as claimed in claim 1, wherein the support structure comprises a central conical element, and wherein the multiplicity of struts are connected to an outer circumferential surface of the central conical element.
5. The intake device as claimed in claim 4, wherein the central conical element is a hollow conical element, and wherein the outer circumferential surface is concave.
6. The intake device as claimed in claim 1, wherein the multiplicity of struts comprises a first group of first struts and a second group of second struts, wherein the first struts have a longer axial extent than the second struts.
7. The intake device as claimed in claim 1, wherein the multiplicity of struts each have a radially inner end with a taper.
8. The intake device as claimed in claim 3, wherein the third muffler elements taper radially inwards.
9. The intake device as claimed in claim 1, wherein the second muffler elements are each arranged at least partially between adjacent struts.
10. The intake device as claimed in claim 1, further comprising a front element and a rear element, wherein at least one of the first muffler elements , the second muffler elements, and the third muffler elements can be mounted in such a way that they can be inserted radially between the front element and the rear element.
11. The intake device as claimed in claim 10, wherein the front element has a first positioning device for at least one of the first muffler elements, the second muffler elements, and the third muffler elements, and wherein the rear element has a second positioning device for at least one of the first muffler elements, the second muffler elements, and the third muffler elements, and wherein the first positioning device is located opposite the second.
12. The intake device as claimed inclaim wherein radially outer ends of the first muffler elements, radially outer ends of the second muffler elements and radially outer ends of the third muffler elements lie on a common circumferential surface.
13. The intake device as claimed claim 1, wherein the first muffler elements have a first length L1, the second muffler elements have a second length L2, and the third muffler elements have a third length L3, wherein the third length L3 is less than the first length L1, and wherein the first length L1 is less than the second length (L3<L1<L2) .
14. An exhaust turbocharger having an intake device for a compressor, the intake device comprising: a support structure having a multiplicity of struts, which are arranged around an axis of the support structure in the circumferential direction and extend in the radial direction, a multiplicity of first muffler elements, which are arranged in the radial continuation of the multiplicity of struts, and a multiplicity of second muffler elements, each of which is arranged between adjacent first muffler elements, wherein radially inwardly directed ends of the multiplicity of first muffler elements are each in contact with radially outwardly directed ends of the multiplicity of struts in such a way that a continuous flow area is formed by the side faces of the first muffler elements and the side faces of the struts, and wherein the multiplicity of second muffler elements each have a radially inner end with a taper, wherein the support structure of the intake device is connected to a compressor housing of the exhaust turbocharger.
15. An internal combustion engine having an exhaust turbocharger as claimed in claim 14.
16. The intake device as claimed in claim 1, wherein the support structure comprises a central conical element, and wherein the multiplicity of struts are integrally connected to an outer circumferential surface of the central conical element.
17. The intake device as claimed in claim 4, wherein the multiplicity of struts comprises a first group of first struts and a second group of second struts, wherein the first struts have a longer axial extent than the second struts.
18. The intake device as claimed in claim 4, wherein the multiplicity of struts each have a radially inner end with a taper.
19. The intake device as claimed in claim 4, wherein the second muffler elements are each arranged at least partially between adjacent struts.
20. The intake device as claimed in claim 1, wherein the first muffler elements have a first length L1, the second muffler elements have a second length L2, and the third muffler elements have a third length L3, wherein the third length L3 is less than the first length L1, and wherein the second length L2 is less than the first length L1 (L3<L2<L1).
Description
BRIEF DESCRIPTION OF THE FIGURES
[0013] The invention will be explained below with reference to exemplary embodiments, which are illustrated in the figures and from which further advantages and modifications can be derived. Here:
[0014]
[0015]
DETAILED DESCRIPTION OF THE FIGURES
[0016] The various embodiments will now be discussed in detail below, one or more examples thereof being illustrated in each figure. Each example serves for explanation and should not be interpreted as restrictive. For example, features illustrated or described as part of one embodiment may be used on or in conjunction with any other embodiment to obtain a further embodiment. It is intended that the present disclosure should include such modifications and variations.
[0017] In the following description of the drawings, the same reference numbers refer to the same or similar components. In general, only the differences with respect to the individual embodiments are described. Unless stated otherwise, the description of a part or aspect in one embodiment may also relate to a corresponding part or corresponding aspect in another embodiment.
[0018]
[0019] According to one embodiment, which can be combined with other embodiments described herein, the intake device 1 comprises a support structure 2 having a multiplicity of struts 3. The multiplicity of struts 3 is arranged around an axis 4 of the support structure 2 in the circumferential direction. The axis 4 of the support structure 2 extends in the axial direction x. The multiplicity of struts 3 extends in the radial direction r. Typically, the axis 4 of the support structure 2 is a central axis of the support structure 2. As illustrated by way of example in
[0020] It should be noted that the muffler elements described herein can also be referred to as guide ribs. As can be seen from
[0021] Thus, an intake device is advantageously provided which is improved over the intake devices known from the prior art. In particular, the intake device is advantageously designed in such a way that the flow through the intake device can have a largely constant speed of flow. Furthermore, the intake device makes it possible to minimize outflow vortices and sudden changes in cross section, thereby advantageously making it possible to reduce pressure losses. In this context, it should be noted that, in principle, each element which is installed in the flow leads to pressure losses. These arise on account of various mechanisms, such as surface friction and outflow vortices. The pressure losses rise sharply with increasing speed of flow. From this point of view, the embodiments of the intake device which are described herein are improved in terms of fluid mechanics.
[0022] Moreover, an intake device is provided which enables a compact installation space and low-cost production and meets the acoustic requirements with regard to the lowest possible noise generation.
[0023] According to one embodiment, which can be combined with other embodiments described herein, radially inwardly directed ends 51 of the multiplicity of first muffler elements 5 are each in contact with radially outwardly directed ends 33 of the multiplicity of struts 3 in such a way that a continuous flow area is formed by the side faces 53 of the first muffler elements and the side faces 35 of the struts 3, as shown by way of example in
[0024] According to one embodiment, which can be combined with other embodiments described herein, the radially inwardly directed ends 51 of the multiplicity of first muffler elements 5 can each be in positive-locking contact with the radially outwardly directed ends 33 of the multiplicity of struts 3.
[0025] According to one embodiment, which can be combined with other embodiments described herein, the intake device 1 further comprises a multiplicity of third muffler elements 7, as illustrated by way of example in
[0026] According to one embodiment, which can be combined with other embodiments described herein, the support structure 2 comprises a central conical element 21, as illustrated by way of example in
[0027] According to one embodiment, which can be combined with other embodiments described herein, the central conical element 21 is a hollow conical element. Typically, the outer circumferential surface 211 of the conical element 21 is of concave design, as illustrated by way of example in
[0028] According to one embodiment, which can be combined with other embodiments described herein, the multiplicity of struts 3 comprises a first group of first struts 31 and a second group of second struts 32, as shown by way of example in
[0029] According to one embodiment, which can be combined with other embodiments described herein, the multiplicity of struts 3 each have a radially inner end 34 with a taper, as shown by way of example in
[0030] As an alternative or in addition, the multiplicity of second muffler elements 6 can each have a radially inner end 61 with a taper, as is likewise shown in
[0031] According to one embodiment, which can be combined with other embodiments described herein, the third muffler elements 7 taper radially inward, as shown by way of example in
[0032] According to one embodiment, which can be combined with other embodiments described herein, the second muffler elements 6 are each arranged at least partially between adjacent struts 3, as illustrated by way of example in
[0033] According to one embodiment, which can be combined with other embodiments described herein, the intake device 1 further comprises a front element 8 and a rear element 9, as shown by way of example in
[0034] According to one embodiment, which can be combined with other embodiments described herein, the front element 8 has a first positioning device 81 for the first muffler elements 5 and/or the second muffler elements (6) and/or the third muffler elements 7. Furthermore, the rear element 9 can have a second positioning device 82 for the first muffler elements 5 and/or the third muffler elements 7. The first positioning device 81 is typically located opposite the second positioning device 82.
[0035] According to one embodiment, which can be combined with other embodiments described herein, radially outer ends 52 of the first muffler elements 5, radially outer ends 62 of the second muffler elements 6 and radially outer ends 72 of the third muffler elements 7 lie on a common circumferential surface 63, as illustrated by way of example in
[0036] According to one embodiment, which can be combined with other embodiments described herein, the first muffler elements 5 have a first length L1, the second muffler elements 6 have a second length L2, and the third muffler elements 7 have a third length L3. The third length L3 is typically less than the first length L1. The first length L1 can be less than the second length. Alternatively, the second length L2 can be less than the first length L1. Mathematically speaking, one of the following inequalities can be satisfied: (1) L3<L1<L2 or (2) L3<L2<L1.
[0037] According to one embodiment, which can be combined with other embodiments described herein, the first muffler elements 5 described herein and/or the second muffler elements 6 described herein and/or the third muffler elements 7 described herein each comprise an absorption element, which typically consists of a damping material. For example, the damping material can be a foam material, a felt or a nonwoven, in particular a polyester nonwoven. The absorption element is typically at least partially surrounded by a damping and absorbing protector. In particular, the damping and absorbing protector can be a damping plate, which is designed, for example, in such a way that an interspace is formed between the side walls of a damping element. The absorption element can be introduced into this interspace.
[0038] As can be seen from the embodiments described herein, an intake device, an exhaust turbocharger and an internal combustion engine are advantageously provided which are improved over the prior art. In particular, a compact intake device for a compressor is provided with which, in comparison with the prior art, a lower pressure loss can be achieved, while the acoustic requirements with regard to the lowest possible noise generation can be met. According to the embodiments described herein, the speed of flow is advantageously kept virtually constant in each cross section in the muffling region of the intake device, leading to minimization of the flow losses. The available installation space can be optimally equipped with muffler elements, thus enabling optimum acoustic damping to be achieved. It should be mentioned at this point that the intake device described herein can also be used without muffler elements, comprising only the support structure 2 with the struts 3. This can be taken into consideration, for example, when noise generation does not play a role and no sound damping is therefore necessary.
[0039] Thus, by means of the embodiments described herein, it is possible to provide an intake device for a turbocharger which meets the requirements of low-cost production, a small overall volume, low pressure loss and optimum sound damping.
[0040] By using the intake device according to the embodiments described herein for a turbocharger of an internal combustion engine, it is thus possible to provide an improved turbocharger and hence an improved internal combustion engine.
TABLE-US-00001 LIST OF REFERENCE SIGNS 1 intake device 11 flow direction of the flow between the muffler elements 2 support structure 21 central conical element of the support structure 211 outer circumferential surface of the central conical element 3 multiplicity of struts 31 first struts 32 second struts 33 radially outwardly directed ends of the multiplicity of struts 34 radially inner end of the second struts 35 side face of the multiplicity of struts 4 axis of the support structure 5 first muffler elements 51 radially inwardly directed ends of the first muffler elements 52 radially outer ends of the first muffler elements 53 side face of the first muffler elements 6 second muffler elements 61 radially inner end of the second muffler elements 62 radially outer ends of the second muffler elements 63 circumferential surface 7 third muffler elements 71 radially inner end of the third muffler elements 72 radially outer ends of the third muffler elements 8 front element 81 first positioning device 82 second positioning device 9 rear element 10 compressor housing L.sub.1 first length of the first muffler elements L.sub.2 second length of the second muffler elements L.sub.3 third length of the second muffler elements r radial direction x axial direction