TURBOCHARGER
20210054810 ยท 2021-02-25
Inventors
Cpc classification
F01M13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/4213
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
F01M2013/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/684
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/685
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10222
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/17
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M26/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A turbocharger is provided and includes a compressor housing and a recirculation slit and a recirculation passage provided at an inlet of the compressor housing to enable air flowing into the compressor to be recirculated. A gas supply part supplies blow-by gas towards the inlet of the compressor housing to allow blow-by gas to be joined with air recirculated through the recirculation slit and the recirculation passage and to guide recirculating air towards a compressor wheel.
Claims
1. A turbocharger, comprising: a compressor housing; a recirculation slit and a recirculation passage provided at an inlet of the compressor housing to enable air flowing into the compressor to be recirculated; and a gas supply part configured to supply blow-by gas towards the inlet of the compressor housing to allow blow-by gas to be joined with air recirculated through the recirculation slit and the recirculation passage and to guide recirculating air towards a compressor wheel.
2. The turbocharger of claim 1, wherein the gas supply part includes: a gas inlet through which blow-by gas is received; a guide passage configured to guide a flow of the blow-by gas in a direction opposite to a flow direction of air discharged from the recirculation passage; and a distribution passage configured to supply the blow-by gas supplied through the gas inlet, to the guide passage.
3. The turbocharger of claim 2, wherein the recirculation passage is formed in a cylindrical shape surrounding a perimeter of the inlet of the compressor, and the guide passage is formed in a cylindrical shape facing the recirculation passage and forming a concentric axis therewith.
4. The turbocharger according to claim 3, wherein the guide passage is formed in a conical cylinder shape with a diameter that gradually decreases towards the recirculation passage.
5. The turbocharger of claim 4, wherein the recirculation passage is formed to have a cross-sectional shape in which an inner surface of the recirculation passage is gradually inclined toward a center of the inlet of the compressor along the guide passage.
6. The turbocharger of claim 3, wherein the distribution passage is formed in a ring shape surrounding an outer side of the guide passage to be in communication with the gas inlet and to be in communication with the guide passage through a plurality of apertures.
7. The turbocharger of claim 3, wherein a guide protrusion, which guides air discharged through the recirculation passage and gas discharged through the guide passage to allow discharged air and gas to flow towards a center of the inlet of the compressor, is provided on a portion at which the recirculation passage and the guide passage intersect.
8. The turbocharger of claim 7, wherein the gas supply part and the guide protrusion are formed integrally on the compressor housing.
9. The turbocharger of claim 7, wherein the gas supply part and the guide protrusion are formed separately to be coupled to the compressor housing.
10. A vehicle having a turbocharger according to claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] The above and other objects, features and advantages of the present disclosure will be more clearly understood from the following detailed description taken in conjunction with the accompanying drawings, in which:
[0011]
[0012]
[0013]
[0014]
[0015]
[0016]
DETAILED DESCRIPTION
[0017] It is understood that the term vehicle or vehicular or other similar term as used herein is inclusive of motor vehicles in general such as passenger automobiles including sports utility vehicles (SUV), buses, trucks, various commercial vehicles, watercraft including a variety of boats and ships, aircraft, and the like, and includes hybrid vehicles, electric vehicles, combustion, plug-in hybrid electric vehicles, hydrogen-powered vehicles and other alternative fuel vehicles (e.g. fuels derived from resources other than petroleum).
[0018] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the disclosure. As used herein, the singular forms a, an and the are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms comprises and/or comprising, when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items.
[0019] Unless specifically stated or obvious from context, as used herein, the term about is understood as within a range of normal tolerance in the art, for example within 2 standard deviations of the mean. About can be understood as within 10%, 9%, 8%, 7%, 6%, 5%, 4%, 3%, 2%, 1%, 0.5%, 0.1%, 0.05%, or 0.01% of the stated value. Unless otherwise clear from the context, all numerical values provided herein are modified by the term about.
[0020] A turbocharger according to the exemplary embodiments of the present disclosure will be described below with reference to the accompanying drawings.
[0021]
[0022] Referring to
[0023] In the turbocharger 1 of the present disclosure, the recirculation slit 7 and the recirculation passage 9 may be formed to allow some of air flowing into the compressor to be recirculated when a surge occurs in the compressor, and a flow of air recirculated through the recirculation slit 7 and the recirculation passage 9 may be guided towards the compressor wheel 11, which is provided at the inlet of the compressor, by a flow of blow-by gas flowing thereinto through the gas supply unit 13.
[0024] Before the surge of the compressor occurs, blow-by gas may flow into the inlet of the compressor through the gas supply part 13 as shown in
[0025] In addition, as described above, blow-by gas forms a flow discharged from a location adjacent to the compressor wheel 11 towards the compressor wheel 11 through the gas supply part 13 as illustrated in
[0026] In this exemplary embodiment, the gas supply unit 13 may include a gas inlet 15 provided to receive blow-by gas; a guide passage 17 configured to guide a flow of blow-by gas in a direction opposite to a flow direction of air discharged from the recirculation passage 9; and a distribution passage 19 configured to supply blow-by gas supplied through the gas inlet 15, to the guide passage 17. In addition, the distribution passage 19 may be formed in a ring shape surrounding an outer side of the guide passage 17 to be in communication with the gas inlet 15 and in communication with the guide passage 17 through a plurality of apertures 21.
[0027] In other words, when blow-by gas is supplied to the gas inlet 15 through a separate blow-by gas hose or the like, the blow-by gas may be supplied to the guide passage 17 through the distribution passage 19 and the apertures 21. On the other hand, the recirculation passage 9 may be formed in a cylindrical shape surrounding a perimeter of the inlet of the compressor, and the guide passage 17 may be formed in a cylindrical shape facing the recirculation passage 9 and forming a concentric axis therewith.
[0028] The guide passage 17 may be formed in a conical cylinder shape that is gradually narrowed towards the recirculation passage 9 (e.g., with a gradually decreasing diameter towards the recirculation passage), and the recirculation passage 9 may be formed to have a cross-sectional shape in which an inner surface of the recirculation passage 9 is gradually inclined toward a center of the inlet of the compressor as it goes towards the guide passage 17. In addition, a guide protrusion 23 may be provided on a portion at which the recirculation passage 9 and the guide passage 17 meet or intersect, and the guide protrusion may guide air discharged through the recirculation passage 9 and gas discharged through the guide passage 17 to allow discharged air and gas to flow towards a center of the inlet of the compressor.
[0029] Therefore, as illustrated in
[0030] The present disclosure may suppress an occurrence of surge, or may rapidly solve a surge condition even when the surge of in the compressor is caused by a sudden increase in the pressure of an outlet side of the compressor. Furthermore, the present disclosure enables blow-by gas to prevent other components such as an air cleaner, an airflow sensor or the like, installed in the intake air pipe, from being contaminated.
[0031] Although the present disclosure has been illustrated and described with respect to the exemplary embodiments, it will be apparent to those skilled in the art that the present disclosure can be variously changed and modified without departing from the technical spirit of the present disclosure provided by the following claims