CN218376697U - Connecting pipeline, air intake system and engine - Google Patents
Connecting pipeline, air intake system and engine Download PDFInfo
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- CN218376697U CN218376697U CN202222480147.8U CN202222480147U CN218376697U CN 218376697 U CN218376697 U CN 218376697U CN 202222480147 U CN202222480147 U CN 202222480147U CN 218376697 U CN218376697 U CN 218376697U
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- 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
Abstract
The utility model provides a connecting line, air intake system and engine. The connecting pipeline comprises a first connecting section, a second connecting section and at least one turbulence rib, the first connecting section is communicated with the second connecting section, and an included angle is formed between the axis of the first connecting section and the axis of the second connecting section; the turbulence ribs are arranged on the inner wall of the first connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section; or the turbulence ribs are arranged on the inner wall of the second connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section. The utility model provides a connecting tube improves the mixing uniformity of air and gas.
Description
Technical Field
The utility model relates to the technical field of engines, especially, relate to a connecting line, air intake system and engine.
Background
The air and the fuel gas are mixed in the air inlet system and then enter the engine. The uniformity of air and gas mixing has a great influence on the dynamic performance, economy, emission and the like of the engine.
In the related art, the air intake system comprises a connecting pipeline, a first pipeline and a second pipeline, wherein one end of the connecting pipeline is communicated with an air source and a fuel gas source, the other end of the connecting pipeline is communicated with one end of the second pipeline, one end of the first pipeline is communicated with the connecting pipeline, the other end of the first pipeline is communicated with an air intake pipe of the engine, and the other end of the second pipeline is communicated with the air intake pipe of the engine. Wherein, connecting line includes first linkage segment, second linkage segment and changeover portion, and first linkage segment and second linkage segment pass through the even transition of changeover portion.
However, such a connection pipe tends to cause poor mixing uniformity of air and gas.
SUMMERY OF THE UTILITY MODEL
The utility model provides a connecting line, air intake system and engine improve the mixing uniformity of air and gas.
In a first aspect, the present invention provides a connecting pipeline for an air intake system of an engine, the connecting pipeline comprising a first connecting section, a second connecting section and at least one turbulence rib, the first connecting section being communicated with the second connecting section, an axis of the first connecting section and an axis of the second connecting section having an included angle;
the turbulence ribs are arranged on the inner wall of the first connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section;
or the turbulence ribs are arranged on the inner wall of the second connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the second connecting section.
In a possible implementation, the utility model provides a connecting tube, vortex muscle quantity is at least two, and two at least vortex muscle include at least one first vortex muscle and at least one second vortex muscle, and first vortex muscle sets up on the inner wall of first linkage segment, and second vortex muscle sets up on the inner wall of second linkage segment.
In a possible implementation, the utility model provides a connecting tube, the axis of first vortex muscle is perpendicular with the axis of first linkage segment, and the axis of second vortex muscle is perpendicular with the axis of second linkage segment.
In a possible implementation manner, the utility model provides a connecting pipeline, the internal diameter of first linkage segment equals with the internal diameter of second linkage segment, and the external diameter of vortex muscle is 0.3-0.5 times of the internal diameter of first linkage segment.
In a possible implementation, the utility model provides a connecting line, connecting line still include the changeover portion, the one end of first linkage segment and the first end intercommunication of changeover portion, the second end of changeover portion and the one end intercommunication of second linkage segment.
In a second aspect, the present invention provides an air intake system, comprising a first pipeline, a second pipeline and the connecting pipeline provided by the first aspect;
the first end of the connecting pipeline is used for being communicated with an air source and a fuel gas source, the second end of the connecting pipeline is communicated with the first end of the second pipeline, the first end of the first pipeline is communicated with the connecting pipeline, and the second end of the first pipeline and the second end of the second pipeline are both communicated with an air inlet pipe of the engine;
the vortex muscle of connecting tube way is located between the first end of connecting tube way and first pipeline.
In a possible implementation manner, the utility model provides an air intake system still includes the blender, the air inlet of blender be used for with air source and gas source intercommunication, the gas outlet of blender and connecting line's first end intercommunication.
In a possible implementation manner, the utility model provides an air intake system still includes first compressor and second compressor, and the air inlet of first compressor and the second end intercommunication of first pipeline, the air inlet of second compressor and the second end intercommunication of second pipeline, the gas outlet of first compressor and the gas outlet of second compressor all be used for with the intake pipe intercommunication of engine.
In a possible implementation manner, the utility model provides an air intake system still includes the intercooler, the gas outlet of first compressor and the gas outlet of second compressor all communicate with the air inlet of intercooler, the gas outlet of intercooler be used for with the intake pipe intercommunication of engine.
In a third aspect, the present invention provides an engine, comprising an engine body and an intake system provided by the above second aspect connected to the engine body.
The utility model provides a connecting line, air intake system and engine machine, connecting line are through setting up first linkage segment, second linkage segment and at least one vortex muscle, first linkage segment and second linkage segment intercommunication, and the axis of first linkage segment axis and second linkage segment has the contained angle. The vortex muscle sets up on the inner wall of first linkage segment, and the extending direction of vortex muscle has the contained angle with the axial of first linkage segment. Or the turbulence ribs are arranged on the inner wall of the second connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section. Therefore, the turbulence ribs can break the original flow field of the air and the fuel gas and enhance the turbulence intensity of the air and the fuel gas, so that the air and the fuel gas are mixed uniformly.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a schematic structural view of a connecting line in the related art;
FIG. 2 is a schematic view showing a configuration of an intake system in the related art;
fig. 3 is a schematic structural diagram of a connection pipeline according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram of an air intake system according to an embodiment of the present invention;
fig. 5 is a schematic structural diagram of another air intake system according to an embodiment of the present invention.
Description of the reference numerals:
10-connecting a pipeline; 11-a first connection section; 12-a second connection segment; 13-a transition section;
20-a first conduit;
30-a second conduit;
100-connecting lines; 110-a first connection segment; 120-a second connection segment; 130-flow disturbing ribs; 131-a first spoiler rib; 132-a second spoiler rib; 140-a transition section;
200-a first conduit;
300-a second conduit;
400-a mixer;
500-an air source;
600-a source of gas;
700-an air filter;
800-a first compressor;
900-a second compressor;
1000-intercooler;
1100-a first intake pipe;
1200-second intake duct.
Detailed Description
In the description of the present invention, it is to be noted that, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may include, for example, a fixed connection, an indirect connection via an intermediary, a connection between two elements, or an interaction between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
The terms "first," "second," and "third" (if any) in the description and claims of this invention and the above-described drawings are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged under appropriate circumstances such that, for example, embodiments of the invention described herein may be implemented in sequences other than those illustrated or described herein.
Moreover, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or maintenance tool that comprises a list of steps or elements is not necessarily limited to those steps or elements explicitly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or maintenance tool.
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
Fig. 1 is a schematic structural view of a connecting pipe in the related art, and fig. 2 is a schematic structural view of an intake system in the related art.
Referring to fig. 1 and 2, the engine intake system includes a connecting pipeline 10, a first pipeline 20 and a second pipeline 30, one end of the connecting pipeline 10 is communicated with an air source and a gas source, the other end of the connecting pipeline 10 is communicated with one end of the second pipeline 30, one end of the first pipeline 20 is communicated with the first pipeline 20, the other end of the first pipeline 20 is communicated with an intake pipe of the engine, and the other end of the second pipeline 30 is communicated with the intake pipe of the engine.
The connecting pipeline 10 includes a first connecting section 11, a second connecting section 12 and a transition section 13, and the first connecting section 11 and the second connecting section 12 are uniformly transited through the transition section 13. In this way, air and gas can flow along the inner cavities of the first and second connection sections 11 and 12.
However, because the density of the gas and the air is different, the first connection section 11 and the second connection section 12 are smoothly connected through the transition section 13, so that under the centrifugal action, more air with higher density flows along the outer side of the inner wall of the connection pipeline 10, and gas with lower density flows along the inner side of the inner wall, thereby causing the ratio of the air and the gas entering the first pipeline 20 and the second pipeline 30 to be different, and the concentration of the gas in the first pipeline 20 is greater than that in the second pipeline 30. The mass fraction of the fuel gas in the first pipeline 20 is 19.5% higher than that in the second pipeline 30, which is obtained by CFD (Computational Fluid Dynamics) analysis. Therefore, the mixing uniformity of the air and the gas is poor.
In order to solve the technical problem, the utility model provides a connecting line, air intake system and engine, connecting line includes first linkage segment, second linkage segment and at least one vortex muscle, first linkage segment and second linkage segment intercommunication, and the axis of first linkage segment axis and second linkage segment has the contained angle, and the vortex muscle sets up on the inner wall of first linkage segment, and the extending direction of vortex muscle has the contained angle with the axial of first linkage segment. Or the turbulence ribs are arranged on the inner wall of the second connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section. Therefore, the turbulence ribs can break the original flow field of the air and the fuel gas and enhance the turbulence intensity of the air and the fuel gas, so that the air and the fuel gas are mixed uniformly.
Fig. 3 is a schematic structural diagram of a connection pipeline provided in an embodiment of the present invention.
Referring to fig. 3, the present invention provides a connecting pipeline for an air intake system of an engine, the connecting pipeline 100 includes a first connecting section 110, a second connecting section 120 and at least one turbulence rib 130, the first connecting section 110 is communicated with the second connecting section 120, and an included angle is formed between an axis of the first connecting section 110 and an axis of the second connecting section 120.
The spoiler rib 130 is disposed on an inner wall of the first connecting section 110, and an extending direction of the spoiler rib 130 has an included angle with an axial direction of the first connecting section 110.
Or, the spoiler rib 130 is disposed on an inner wall of the second connecting section 120, and an extending direction of the spoiler rib 130 and an axial direction of the first connecting section 110 form an included angle.
When the air-fuel gas mixing device is used, air and fuel gas collide with the turbulence ribs 130 when flowing along the inner cavities of the first connecting section 110 and the second connecting section 120, the turbulence intensity of the air and the fuel gas is enhanced, and the mixing uniformity of the air and the fuel gas is improved.
Compared with the condition that the axis of the first connecting section 110 is parallel to the axis of the second connecting section 120, the occupied space of the connecting pipeline 100 can be reduced under the condition that the length of the first connecting section 110 and the length of the second connecting section 120 are ensured to be constant.
According to the connecting pipeline 100 provided by the embodiment, the first connecting section 110 is communicated with the second connecting section 120 by arranging the first connecting section 110, the second connecting section 120 and the at least one turbulence rib 130, and an included angle is formed between the axis of the first connecting section 110 and the axis of the second connecting section 120. The spoiler rib 130 is disposed on an inner wall of the first connecting section 110, and an extending direction of the spoiler rib 130 has an included angle with an axial direction of the first connecting section 110. Or, the turbulent rib 130 is disposed on the inner wall of the second connection section 120, and an extending direction of the turbulent rib 130 forms an included angle with the axial direction of the first connection section 110. Thus, the turbulence ribs 130 can break the original flow field of the air and the gas, and enhance the turbulence intensity of the air and the gas, thereby achieving the mixing uniformity of the air and the gas.
In a possible implementation manner, the number of the turbulence ribs 130 is at least two, the at least two turbulence ribs 130 include at least one first turbulence rib 131 and at least one second turbulence rib 132, the first turbulence rib 131 is disposed on the inner wall of the first connecting section 110, and the second turbulence rib 132 is disposed on the inner wall of the second connecting section 120.
It can be understood that the air and the gas collide with the first spoiler rib 131 when flowing along the inner cavity of the first connecting section 110 and then collide with the second spoiler rib 132 again when flowing along the inner cavity of the second connecting section 120, so that the turbulence intensity of the air and the gas is increased and the mixing uniformity of the air and the gas is improved.
In some embodiments, the axis of the first spoiler rib 131 is perpendicular to the axis of the first connecting section 110, and the axis of the second spoiler rib 132 is perpendicular to the axis of the second connecting section 120. In this way, the turbulence intensity of the air and the gas can be increased.
Specifically, two ends of the first spoiler rib 131 are correspondingly connected to two opposite sides of the inner wall of the first connecting section 110, and two ends of the second spoiler rib 132 are correspondingly connected to two opposite sides of the inner wall of the second connecting section 120.
In a possible implementation manner, the inner diameter of the first connection section 110 is equal to the inner diameter of the second connection section 120, and the outer diameter of the spoiler rib 130 is 0.3-0.5 times the inner diameter of the first connection section 110.
Illustratively, the turbulator 130 has a diameter that is 0.4 times the inner diameter of the first connection section 110. For example, the inner diameter of the first connection section 110 and the inner diameter of the second connection section 120 are both 250mm, and the outer diameter of the spoiler rib 130 is 100mm.
Specifically, the spoiler rib 130 may have a cylindrical shape.
When the outer diameter of the turbulent rib 130 is less than 0.3 times of the inner diameter of the first connection section 110, the degree of damage of the turbulent rib 130 to the original flow field of air and gas is low.
When the outer diameter of the spoiler rib 130 is greater than 0.5 times the inner diameter of the first connection section 110, pressure loss is large in the air and gas flowing process.
In one possible implementation, the connecting line 100 further includes a transition section 140, one end of the first connecting section 110 is in communication with a first end of the transition section 140, and a second end of the transition section 140 is in communication with an end of the second connecting section 120.
Specifically, the first connection section 110 and the second connection section 120 are uniformly transited by the transition section 140, so that pressure loss is small during the flow of air and gas.
Fig. 4 is a schematic structural diagram of an air intake system according to an embodiment of the present invention.
Referring to fig. 4, the present invention provides an air intake system, which includes a first pipeline 200, a second pipeline 300 and the connection pipeline 100 provided in the above embodiment.
The first end of connecting line 100 is used for communicating with air source and gas source, and the second end of connecting line 100 communicates with the first end of second pipeline 300, and the first end and the connecting line 100 intercommunication of first pipeline 200, the second end of first pipeline 200 and the second end of second pipeline 300 all communicate with the intake pipe of engine, and the vortex muscle 130 of connecting line 100 is located between the first end of connecting line 100 and first pipeline 200.
When the engine is used, air and fuel gas flow along the inner cavities of the first connecting section 110 and the second connecting section 120 and collide with the turbulence ribs 130, the turbulence intensity of the air and the fuel gas is enhanced, the mixing uniformity of the air and the fuel gas is improved, then one part of the air and the fuel gas enters the first pipeline 200, the other part of the air and the fuel gas enters the second pipeline 300, and finally the air and the fuel gas in the first pipeline 200 and the second pipeline 300 enter an air inlet pipe of the engine.
The CFD analysis is performed by taking as an example that the connecting duct 100 includes a first connecting section 110, a second connecting section 120, and a transition section 140. Wherein one end of the first connecting section 110 is communicated with a first end of the transition section 140, a second end of the transition section 140 is communicated with one end of the second connecting section 120, and the first connecting section 110 and the second connecting section 120 are smoothly transited. A first turbulent rib 131 is arranged on the inner wall of the first connection section 110, and the extending direction of the first turbulent rib 131 is perpendicular to the axial direction of the first connection section 110. Meanwhile, a second turbulence rib 132 is arranged on an inner wall of the second connection section 120, and an extending direction of the second turbulence rib 132 is perpendicular to an axial direction of the second connection section 120.
Through the CFD analysis, the mass fraction of the fuel gas in the first pipeline 200 is 0.1% higher than that in the second pipeline 300. Therefore, the mixing uniformity of air and fuel gas in the air inlet system of the engine is good. And the average pressure loss connecting the first end of line 100 to the second end of first line 200 and connecting the first end of line 100 to the second end of second line 300 was 3.3kPa, with a small pressure loss.
The air intake system provided by the present embodiment is formed by providing connecting pipe 100, first pipe 200, and second pipe 300. The first end of connecting line 100 is used for communicating with air source and gas source, and the second end of connecting line 100 communicates with the first end of second pipeline 300, and the first end and the connecting line 100 intercommunication of first pipeline 200, the second end of first pipeline 200 and the second end of second pipeline 300 all communicate with the intake pipe of engine, and the vortex muscle 130 of connecting line 100 is located between the first end of connecting line 100 and first pipeline 200. Thus, the turbulence ribs 130 can break the original flow field of the air and the gas, and enhance the turbulence intensity of the air and the gas, thereby achieving the mixing uniformity of the air and the gas.
Fig. 5 is a schematic structural diagram of another air intake system according to an embodiment of the present invention.
Referring to fig. 5, in some embodiments, the air intake system further comprises a mixer 400, an air inlet of the mixer 400 being adapted to communicate with an air source 500 and a gas source 600, and an air outlet of the mixer 400 being in communication with the first end of the first connecting section 110.
The mixer 400 is a device that mixes the gas and air in the intake system.
Illustratively, the mixer 400 may be a venturi mixer 400. The venturi mixer 400 utilizes the principle of the venturi effect. When air flows in the convergent-divergent nozzle, the speed reaches the maximum value at the throat of the minimum section of the pipeline, the dynamic pressure is the maximum, the static pressure is the minimum, and the gas enters the mixer 400 due to the pressure difference because the outlet of the gas source 600 is communicated with the throat.
In one possible implementation, the air intake system further comprises an air filter 700, an air inlet of the air filter 700 being adapted to communicate with the air source 500, and an air outlet of the air filter 700 being in communication with an air inlet of the mixer 400.
It will be appreciated that by providing air filter 700 to filter impurities in the air, the useful life of the engine may be increased.
In this embodiment, the air intake system further includes a first compressor 800 and a second compressor 900, an air inlet of the first compressor 800 is communicated with the second end of the first pipeline 200, an air inlet of the second compressor 900 is communicated with the second end of the second pipeline 300, and an air outlet of the first compressor 800 and an air outlet of the second compressor 900 are both used for being communicated with an air intake pipe of the engine.
The first compressor 800 compresses air and gas discharged from the first pipeline 200, and the second compressor 900 compresses air and gas discharged from the second pipeline 300. Thus, compression efficiency can be improved.
In some embodiments, the air intake system further comprises an intercooler 1000, an air outlet of the first compressor 800 and an air outlet of the second compressor 900 are both communicated with an air inlet of the intercooler 1000, and an air outlet of the intercooler 1000 is used for being communicated with an air inlet pipe of the engine.
It can be understood that the intercooler 1000 may cool the compressed air discharged from the first compressor 800 and the second compressor 900, so as to protect the engine and prolong the service life of the engine. Moreover, the compressed air discharged from the first compressor 800 and the second compressor 900 is mixed in the intercooler 1000 and then enters the intake pipe of the engine, so that the uniformity of mixing of air and fuel gas can be improved.
The utility model provides an engine, including engine body and the air intake system who provides with the above-mentioned embodiment that engine body is connected.
For example, the engine may be a V-type engine.
The air intake duct of the engine includes a first air intake duct 1100 and a second air intake duct 1200, and a part of air and fuel gas discharged from the air outlet of the intercooler 1000 enters the engine body through the first air intake duct 1100, and the other part enters the engine body through the second air intake duct 1200.
The structure and principle of the air intake system are described in detail in the above embodiments, which are not repeated herein.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.
Claims (10)
1. A connecting pipeline is used for an air inlet system of an engine and is characterized by comprising a first connecting section, a second connecting section and at least one turbulence rib, wherein the first connecting section is communicated with the second connecting section, and an included angle is formed between the axis of the first connecting section and the axis of the second connecting section;
the turbulence ribs are arranged on the inner wall of the first connecting section, and an included angle is formed between the extending direction of the turbulence ribs and the axial direction of the first connecting section;
or, the vortex muscle sets up on the inner wall of second linkage segment, the extending direction of vortex muscle with the axial of second linkage segment has the contained angle.
2. The connecting pipeline of claim 1, characterized in that, vortex muscle quantity is at least two, at least two the vortex muscle includes at least one first vortex muscle and at least one second vortex muscle, first vortex muscle sets up on the inner wall of first linkage segment, the second vortex muscle sets up on the inner wall of second linkage segment.
3. The connecting pipe according to claim 2, wherein the axis of the first spoiler rib is perpendicular to the axis of the first connecting section, and the axis of the second spoiler rib is perpendicular to the axis of the second connecting section.
4. The connecting pipe according to any one of claims 1 to 3, wherein the inner diameter of the first connecting section is equal to the inner diameter of the second connecting section, and the outer diameter of the spoiler rib is 0.3 to 0.5 times the inner diameter of the first connecting section.
5. The connecting line according to any one of claims 1 to 3, further comprising a transition section, wherein one end of the first connecting section communicates with a first end of the transition section, and wherein a second end of the transition section communicates with an end of the second connecting section.
6. An air intake system, characterized by comprising a first pipe, a second pipe, and the connecting pipe of any one of claims 1 to 5;
the first end of the connecting pipeline is used for being communicated with an air source and a fuel gas source, the second end of the connecting pipeline is communicated with the first end of the second pipeline, the first end of the first pipeline is communicated with the connecting pipeline, and the second end of the first pipeline and the second end of the second pipeline are both communicated with an air inlet pipe of an engine;
the turbulence rib of the connecting pipeline is located between the first end of the connecting pipeline and the first pipeline.
7. The air intake system of claim 6, further comprising a mixer having an air inlet for communication with the air source and the gas source, and an air outlet in communication with the first end of the connecting conduit.
8. The air intake system of claim 6, further comprising a first compressor and a second compressor, wherein an air inlet of the first compressor is communicated with the second end of the first pipeline, an air inlet of the second compressor is communicated with the second end of the second pipeline, and an air outlet of the first compressor and an air outlet of the second compressor are both used for being communicated with an air intake pipe of the engine.
9. The air intake system of claim 8, further comprising an intercooler, an air outlet of the first compressor and an air outlet of the second compressor both communicating with an air inlet of the intercooler, the air outlet of the intercooler being adapted to communicate with an air intake of the engine.
10. An engine comprising an engine block and the intake system of any one of claims 6 to 9 connected to the engine block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222480147.8U CN218376697U (en) | 2022-09-19 | 2022-09-19 | Connecting pipeline, air intake system and engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222480147.8U CN218376697U (en) | 2022-09-19 | 2022-09-19 | Connecting pipeline, air intake system and engine |
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| Publication Number | Publication Date |
|---|---|
| CN218376697U true CN218376697U (en) | 2023-01-24 |
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| CN202222480147.8U Active CN218376697U (en) | 2022-09-19 | 2022-09-19 | Connecting pipeline, air intake system and engine |
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