EP4165292A1 - Intake device for a compressor - Google Patents
Intake device for a compressorInfo
- Publication number
- EP4165292A1 EP4165292A1 EP21730807.1A EP21730807A EP4165292A1 EP 4165292 A1 EP4165292 A1 EP 4165292A1 EP 21730807 A EP21730807 A EP 21730807A EP 4165292 A1 EP4165292 A1 EP 4165292A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- silencer elements
- struts
- silencer
- elements
- suction device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 21
- 230000003584 silencer Effects 0.000 claims description 86
- 238000013016 damping Methods 0.000 abstract description 11
- 239000007789 gas Substances 0.000 description 16
- 238000010521 absorption reaction Methods 0.000 description 5
- 239000003570 air Substances 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000002745 absorbent Effects 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000006261 foam material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1205—Flow throttling or guiding
- F02M35/1211—Flow throttling or guiding by using inserts in the air intake flow path, e.g. baffles, throttles or orifices; Flow guides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1015—Air intakes; Induction systems characterised by the engine type
- F02M35/10157—Supercharged engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1272—Intake silencers ; Sound modulation, transmission or amplification using absorbing, damping, insulating or reflecting materials, e.g. porous foams, fibres, rubbers, fabrics, coatings or membranes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1277—Reinforcement of walls, e.g. with ribs or laminates; Walls having air gaps or additional sound damping layers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1288—Intake silencers ; Sound modulation, transmission or amplification combined with or integrated into other devices ; Plurality of air intake silencers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/14—Combined air cleaners and silencers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/663—Sound attenuation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1283—Manufacturing or assembly; Connectors; Fixations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the invention relates to the field of exhaust gas turbochargers for supercharged internal combustion engines.
- the invention relates to an intake device for a compressor of an exhaust gas turbocharger.
- exhaust gas turbochargers are used as standard nowadays, with a turbine in the exhaust gas tract of the internal combustion engine and with a compressor upstream of the internal combustion engine.
- the exhaust gases from the internal combustion engine are expanded in the turbine.
- the work gained in this way is transmitted to the compressor by means of a shaft, which compresses the air supplied to the internal combustion engine.
- Filter silencers are known from the prior art, which are typically used on the suction side of a compressor, the the combustion air is compressed and fed to an internal combustion engine. Such a compressor is driven by the exhaust gas turbine of an exhaust gas turbocharger.
- the filter silencer are designed such that ambient air can be introduced through a filter arranged on the periphery of a filter silencer into an interior of the filter silencer equipped with damping elements, then flows past the damping elements, and thereby to the compressor wheel, from which sound waves counter to the air flow go out, is deflected by guide elements.
- the sound attenuation takes place dissipatively at the attenuation elements, in that the sound energy is converted into heat directly through porous or fibrous absorption materials from which the attenuation elements are essentially made up. It has been found that the sound-absorbing suction devices known from the prior art have certain disadvantages with regard to the required installation space size and also with regard to the pressure losses that occur.
- one object of the present invention is to provide an intake device for a compressor that is as compact as possible, for example a compressor of an exhaust gas turbocharger of an internal combustion engine, with which the lowest possible pressure loss can be achieved.
- One Another object of the present invention is to provide a suction device which meets the acoustic requirements with regard to the lowest possible noise development.
- a suction device for a compressor comprises a support structure with 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 suction device comprises a multiplicity of first silencer elements which are arranged in a radial extension of the multiplicity of struts. In addition, the suction device comprises a plurality of second silencer elements, which are each arranged between adjacent first silencer elements.
- a suction device is advantageously provided which is improved over the suction devices known from the prior art.
- the suction device according to the invention provides a suction device which is designed such that the flow can flow through the suction device at a largely constant flow rate.
- outflow vortices can be minimized and cross-sectional jumps can be kept small, so that pressure losses can advantageously be minimized.
- a suction device is provided which enables a compact installation space and inexpensive production and which meets the acoustic requirements with regard to the lowest possible Noise development met.
- an exhaust gas turbocharger is provided with an intake device according to one of the embodiments described herein, wherein the support structure of the intake device according to the invention is connected to a compressor housing of the exhaust gas turbocharger.
- An improved exhaust gas turbocharger can thus advantageously be provided.
- a third aspect of the invention relates to an internal combustion engine with an exhaust gas turbocharger according to one of the embodiments described herein.
- an improved internal combustion engine can advantageously be provided.
- FIG. 1 shows a schematic perspective sectional view of a suction device according to the embodiments described herein, which is arranged on a suction side of a compressor; and
- FIG. 2 shows a detail of a schematic axial sectional view of a suction device according to the embodiments described herein.
- Figure 1 shows a schematic perspective sectional view of a suction device 1 for a compressor according to the embodiments described herein.
- the compressor housing 10 of the compressor is indicated schematically.
- the suction device 1 is arranged on a suction side of a compressor.
- the suction device 1 comprises a support structure 2 with a plurality of struts 3.
- the plurality of struts 3 is arranged in the circumferential direction about an axis 4 of the support structure 2.
- the axis 4 of the support structure 2 extends in the axial direction x.
- the plurality of struts 3 extends in the radial direction r.
- the axis 4 of the support structure 2 is typically a central axis of the support structure 2.
- the suction device 1 comprises a multiplicity of first silencer elements 5.
- the multiplicity of first silencer elements 5 is arranged in a radial extension of the multiplicity of struts 3.
- the suction device 1 comprises a plurality of second silencer elements 6, which are each arranged between adjacent first silencer elements 5.
- the first silencer elements 5 and the second silencer elements 6 are arranged radially, in the circumferential direction, around the axis 4 of the support structure 2.
- the first silencer elements 5 and the second silencer elements 6 can be arranged distributed uniformly in the circumferential direction, in particular around the axis 4 of the support structure 2.
- the first silencer elements 5 and the second silencer elements 6 can be arranged alternately in the circumferential direction.
- third silencer elements 7 can be arranged between the first silencer elements 5 and the second silencer elements 6, as described herein and shown by way of example in FIGS. 1 and 2.
- the silencer elements described herein can also be referred to as scenes.
- the number of scenes increases from the inside (i.e. from the axis 4) to the outside, so that the flow cross-sections in the radial direction between the scenes is advantageously essentially constant.
- a suction device is advantageously provided which is improved over the suction devices known from the prior art.
- the suction device is advantageously designed in such a way that the flow can flow through the suction device at a largely constant flow rate.
- the suction device enables outflow vortices and cross-sectional jumps to be minimized, as a result of which pressure losses can advantageously be reduced.
- every element that is built into the flow leads to pressure losses. These arise due to various mechanisms, such as surface friction and outflow vortices. The pressure losses increase sharply with increasing flow velocity. From this point of view, the embodiments of the suction device described herein are fluidically improved.
- a suction device which enables a compact installation space and inexpensive production and meets the acoustic requirements with regard to the lowest possible noise development.
- struts 3 of the support structure 2 and the first silencer elements 5 thus form a common geometric shape, which has a positive effect on minimizing pressure losses, so that flow separations can be avoided.
- the radially inwardly directed ends 51 of the plurality of first silencer elements 5 can each be in positive contact with the radially outwardly directed ends 33 of the plurality of struts 3.
- the suction device 1 further comprises a plurality of third silencer elements 7, as is shown by way of example in FIGS. 1 and 2.
- the third silencer elements 7 are typically each arranged between a first silencer element 5 and a second silencer element 6.
- the third silencer elements 7 have a smaller radial extent than the second silencer elements 6.
- the third silencer elements 7 have a smaller radial extent than the second silencer elements 6.
- Silencer elements 7 can be arranged distributed uniformly in the circumferential direction, in particular around the axis 4 of the support structure 2.
- the support structure 2 comprises a central cone-like element 21, as is shown by way of example in FIG.
- the multiplicity of struts 3 is typically connected to an outer jacket surface 211 of the central cone-like element 21.
- the struts 3 can be integrally connected to the outer jacket surface 211 of the central cone-like element 21.
- the central cone-like element 21 and the plurality of struts 3 can be designed in the form of a cast part or a milled part.
- the struts 3 can be connected to the central cone-like element 21 by means of a screw connection or a welded connection.
- the central cone-like element 21 is a hollow-cone-like element.
- the outer circumferential surface 211 of the conical element 21 is typically concave, as is shown by way of example in FIG.
- the first struts 31 typically have a longer axial extent than the second struts 32.
- the first group of first struts 31 and the second group of second struts 32 can each have half the total number of struts 3.
- the first struts 31 and the second struts 32 are typically arranged alternately in the circumferential direction.
- the plurality of struts 3 each have a radially inner end 34 with a taper, as is shown by way of example in FIG. In other words, the thickness of the struts 3 is reduced towards the axis 4 of the support structure 2.
- Silencer elements 6 each have a radially inner end 61 with a taper, as is also shown in FIG. In other words, the thickness of the silencer elements 6 is reduced towards the axis 4 of the support structure 2. In other words, the silencer elements 6 have a tapering on the downstream side.
- the direction of flow of the flow between the muffler elements of the suction device is shown by way of example by the arrows 11 in FIG. 1.
- the third muffler elements 7 taper radially inward, as is shown by way of example in FIG. In other words, the third silencer elements 7 have a tapering on the downstream side.
- the second silencer elements 6 are each arranged at least partially between adjacent struts 3, as is shown by way of example in FIGS. 1 and 2.
- the suction device 1 further comprises a front element 8 and a rear element 9, as is shown by way of example in FIG.
- the front element 8 can be a front panel.
- the front plate can be designed in the form of a disk, in particular a circular disk, as is shown by way of example in FIG.
- the back element 9 can be a back plate, in particular a back plate with a central opening.
- the back plate can be designed in the form of a disk, in particular a circular disk, with a central opening, as shown in FIG.
- the first silencer elements 5 can be mounted radially inserted between the front element 8 and the rear element 9.
- the third silencer elements 7 can be mounted radially insertable between the front element 8 and the rear element 21.
- the second muffler elements 6 can be mounted such that they can be pushed in axially. Alternatively, the second can
- Muffler elements 6 can be mounted radially inserted between the front element 8 and the rear element 21.
- the front element 8 has a first positioning device 81 for the first silencer elements 5 and / or the second silencer elements (6) and / or the third silencer elements 7.
- the rear element 9 can have a second positioning device 82 for the first silencer elements 5 and / or the third silencer elements 7.
- the first guide device 81 is the second guide device opposite.
- the first silencer elements 5 have a first length LI
- the second silencer elements 6 have a second length L2
- the third silencer elements 7 have a third length L3.
- the third length L3 is typically smaller than the first length LI.
- the first length LI can be smaller than the second length.
- the second length L2 can be smaller than the first length LI.
- the first silencer elements 5 described herein and / or the second silencer elements 6 described herein and / or the third silencer elements 7 described herein each comprise an absorption element that is typically made of a damping material consists.
- the damping material can be a foam material, a felt or a fleece, in particular a polyester fleece.
- the absorption element is typically at least partially surrounded by a cushioning and absorbent protection.
- the damping and absorbing protection can be Be damping plate, which is designed, for example, such that a gap is formed between the side walls of a damping element. The absorption element can be introduced into this intermediate space.
- an intake device, an exhaust gas turbocharger and an internal combustion engine are advantageously provided, which are improved over the prior art.
- a compact suction device for a compressor is provided, with which a lower pressure loss can be achieved compared to the prior art, while the acoustic requirements with regard to the lowest possible noise development can be met.
- the flow velocity is advantageously kept almost constant in each cross section in the sound-absorbing area of the suction device, which leads to a minimization of the flow losses.
- the existing installation space can be optimally equipped with silencer elements so that optimal acoustic damping can be achieved.
- the suction device described here can also be used without sound absorber elements and only comprises the support structure 2 with the struts 3. This can be taken into account, for example, if the development of noise does not play a role and therefore no sound absorption is necessary.
- an intake device for a turbocharger can be provided, which meets the requirements of cost-effective manufacture, a small structural volume, a low pressure loss and optimal sound attenuation.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP20180315.2A EP3926155A1 (en) | 2020-06-16 | 2020-06-16 | Intake device for a compressor |
PCT/EP2021/064061 WO2021254749A1 (en) | 2020-06-16 | 2021-05-26 | Intake device for a compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
EP4165292A1 true EP4165292A1 (en) | 2023-04-19 |
Family
ID=71105259
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20180315.2A Withdrawn EP3926155A1 (en) | 2020-06-16 | 2020-06-16 | Intake device for a compressor |
EP21730807.1A Withdrawn EP4165292A1 (en) | 2020-06-16 | 2021-05-26 | Intake device for a compressor |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20180315.2A Withdrawn EP3926155A1 (en) | 2020-06-16 | 2020-06-16 | Intake device for a compressor |
Country Status (6)
Country | Link |
---|---|
US (1) | US20230213009A1 (en) |
EP (2) | EP3926155A1 (en) |
JP (1) | JP2023530117A (en) |
KR (1) | KR20230024365A (en) |
CN (1) | CN115997071A (en) |
WO (1) | WO2021254749A1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE59207544D1 (en) * | 1992-06-17 | 1997-01-02 | Asea Brown Boveri | Filter silencer |
GB2426555A (en) * | 2005-05-28 | 2006-11-29 | Siemens Ind Turbomachinery Ltd | Turbocharger air intake |
JP5843505B2 (en) * | 2011-07-12 | 2016-01-13 | 三菱重工業株式会社 | Silencer for supercharger, supercharger and hybrid supercharger equipped with the silencer |
DE102018100465A1 (en) * | 2018-01-10 | 2019-07-11 | Abb Turbo Systems Ag | Filter silencer for an exhaust gas turbocharger of an internal combustion engine |
-
2020
- 2020-06-16 EP EP20180315.2A patent/EP3926155A1/en not_active Withdrawn
-
2021
- 2021-05-26 EP EP21730807.1A patent/EP4165292A1/en not_active Withdrawn
- 2021-05-26 US US18/008,943 patent/US20230213009A1/en active Pending
- 2021-05-26 KR KR1020237001172A patent/KR20230024365A/en unknown
- 2021-05-26 WO PCT/EP2021/064061 patent/WO2021254749A1/en unknown
- 2021-05-26 JP JP2022576818A patent/JP2023530117A/en active Pending
- 2021-05-26 CN CN202180042831.3A patent/CN115997071A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
US20230213009A1 (en) | 2023-07-06 |
WO2021254749A1 (en) | 2021-12-23 |
EP3926155A1 (en) | 2021-12-22 |
JP2023530117A (en) | 2023-07-13 |
KR20230024365A (en) | 2023-02-20 |
CN115997071A (en) | 2023-04-21 |
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