CN209539443U - A kind of engine turbine guide duct - Google Patents

A kind of engine turbine guide duct Download PDF

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Publication number
CN209539443U
CN209539443U CN201821349964.7U CN201821349964U CN209539443U CN 209539443 U CN209539443 U CN 209539443U CN 201821349964 U CN201821349964 U CN 201821349964U CN 209539443 U CN209539443 U CN 209539443U
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China
Prior art keywords
guide duct
ring body
engine turbine
guide
flow
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Active
Application number
CN201821349964.7U
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Chinese (zh)
Inventor
方立锋
蔡炳芳
饶聪超
吴文洋
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Shentong Technology Group Co Ltd
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Shentong Technology Group Co Ltd
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Priority to CN201821349964.7U priority Critical patent/CN209539443U/en
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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Abstract

The utility model provides a kind of engine turbine guide duct, is related to a kind of engine turbine device.It solves the problems, such as that the vibration of turbine guide duct is big in the prior art, noise is big.This engine turbine guide duct, the tube body including guide duct are provided with guide vane in the guide duct, and guide vane is uniformly distributed in guide duct inner circumferential, and guide vane is towards identical as flow direction of the air-flow in guide duct.Vibration and noise caused by air-flow is effectively reduced using the damped noise reduction device of setting in the utility model, and structure is simple, easy to operate, at low cost.

Description

A kind of engine turbine guide duct
Technical field
The utility model belongs to technical field of automobile engine, is related to a kind of engine turbine device, especially a kind of hair Motivation turbine guide duct.
Background technique
Engine turbine provides enough air using the exhaust gas-driven turbine being discharged using engine for engine combustion, But since the fluctuation for discharging into gas of engine is more violent, cause that vibration is big, noise is big.
Utility model content
The purpose of this utility model is in view of the above-mentioned problems existing in the prior art, to propose a kind of engine turbine wind-guiding Pipe, this engine turbine guide duct can be effectively reduced vibration and noise caused by air-flow.
The purpose of this utility model can be realized by the following technical scheme: a kind of engine turbine guide duct, including lead The tube body of air hose is provided with guide vane in the guide duct, and guide vane is uniformly distributed in guide duct inner circumferential, guide vane direction It is identical as flow direction of the air-flow in guide duct.
Setting guide vane makes high-speed flow and low speed flow part high-speed flow and low speed gas during mixing Stream is first mixed, to generate the lesser turbulent flow in part or generate the lesser turbulent flow in part inside high-speed flow, is made in this way Obtaining the energy that high-speed flow and low speed flow are discharged when being sufficiently mixed reduces, and avoids high-speed flow and low speed flow directly mixed Merging causes strong turbulent flow.
In above-mentioned engine turbine guide duct, the guide vane is arranged in ring body, before the guide vane The structure for holding small rear end big, so that the turbulence state of air-flow can be smoothly passed over and reduced to air-flow.
In above-mentioned engine turbine guide duct, the bending place of guide duct is arranged in the guide vane, to prevent The aggravation of turbulent flow.
In above-mentioned engine turbine guide duct, the ring body is rotatably assorted with wind-guiding inside pipe wall, sets in the ring body Magnet there are two setting, the magnetic pole of two magnet is in the same direction in the circumferential direction of ring body, is provided on the guide duct between two magnet Electromagnet attracts the magnet in ring body by electromagnet, to control by the pole orientation of the change control electromagnet of electric current The rotation of ring body, so that the position of guide vane is adjusted, so that guide vane is in the position of most suitable damping noise reduction.
In above-mentioned engine turbine guide duct, the ring body is flexible elastomer material, is provided with annular in ring body Chamber, feeder control the pressure of annular intracavity gas, the size of ring body are then controlled, to control guide duct breathing area Size, so that reaching the optimal of air inlet effect according to the size of operating conditions air-flow, not only having met air inflow but also reducing Shake noise.
In above-mentioned engine turbine guide duct, it is provided with shock sensor on the guide duct, to perceive constantly The vibrating state of guide duct.
Compared with prior art, this engine turbine guide duct has the advantage that
Vibration and noise caused by air-flow, structure letter is effectively reduced using the damped noise reduction device of setting in the utility model It is single, it is easy to operate, it is at low cost.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of embodiment one;
Fig. 2 is the schematic diagram of embodiment two;
Fig. 3 is the schematic diagram of embodiment three.
In figure, tube body 1, guide vane 2, shock sensor 3, ring body 4, magnet 5, electromagnet 6, feeder 7.
Specific embodiment
It is specific embodiment of the utility model below, and the technical solution of the utility model is made further in conjunction with attached drawing Description, but the utility model is not limited to these examples.
Embodiment one
As shown in Figure 1, a kind of engine turbine guide duct, the tube body 1 including guide duct is provided in the guide duct and leads To blade 2, guide vane is uniformly distributed in guide duct inner circumferential, flow direction phase of the guide vane direction with air-flow in guide duct Together.Setting guide vane makes high-speed flow with low speed flow, and part high-speed flow and low speed flow during mixing are advanced Row mixing, to generate the lesser turbulent flow in part or generate the lesser turbulent flow in part inside high-speed flow, so that high speed The energy that air-flow and low speed flow are discharged when being sufficiently mixed reduces, and high-speed flow is avoided directly to mix and make with low speed flow At strong turbulent flow.
The guide vane is arranged in ring body, the big structure in the small rear end in the front end of the guide vane, so as to air-flow It can smoothly pass over and reduce the turbulence state of air-flow.The bending place of guide duct is arranged in the guide vane, with Just the aggravation of turbulent flow is prevented.Shock sensor 3 is provided on the guide duct, to perceive the vibrating state of guide duct constantly.
Embodiment two
As shown in Fig. 2, the ring body 4 is rotatably assorted with wind-guiding inside pipe wall, and magnet 5 there are two settings in the ring body, two The magnetic pole of a magnet is in the same direction in the circumferential direction of ring body, is provided with electromagnet 6 on the guide duct between two magnet, passes through electric current Change control electromagnet pole orientation, attraction or repulsion by high-speed double electromagnet to magnet in ring body, so as to control ring The rotation of body, so that the position of guide vane is adjusted, so that guide vane is in the position of most suitable damping noise reduction.
Embodiment three
As shown in figure 3, the ring body is flexible elastomer material, annular chamber, 7 control ring of feeder are provided in ring body The pressure of shape intracavity gas, then controls the size of ring body, so that the size of guide duct breathing area is controlled, so that According to the size of operating conditions air-flow, reach the optimal of air inlet effect, not only met air inflow but also reduces vibration noise.
Although some terms are used more herein, it does not exclude the possibility of using other terms.Use these Term is used for the purpose of being more convenient to describe and explain the essence of the utility model;It is construed as any additional limit System is all contrary to the spirit of the present invention.
The specific embodiments described herein are merely examples of the spirit of the present invention.The utility model institute Belonging to those skilled in the art can make various modifications or additions to the described embodiments or using similar Mode substitute, but without departing from the spirit of the present application or beyond the scope of the appended claims.

Claims (6)

1. a kind of engine turbine guide duct, the tube body including guide duct, which is characterized in that be provided with guiding in the guide duct Blade, guide vane is uniformly distributed in guide duct inner circumferential, and guide vane direction is identical as flow direction of the air-flow in guide duct.
2. engine turbine guide duct according to claim 1, which is characterized in that the guide vane is arranged in ring body On, the big structure in the small rear end in the front end of the guide vane.
3. engine turbine guide duct according to claim 1, which is characterized in that the guide vane is arranged in guide duct Bending place.
4. engine turbine guide duct according to claim 2, which is characterized in that the ring body and wind-guiding inside pipe wall rotate Cooperate, there are two magnet for setting in the ring body, and the magnetic pole of two magnet is in the same direction in the circumferential direction of ring body, between two magnet Guide duct on be provided with electromagnet, pass through electric current change control electromagnet pole orientation.
5. engine turbine guide duct according to claim 2, which is characterized in that the ring body is flexible elastomer material Matter, annular chamber is provided in ring body, and feeder controls the pressure of annular intracavity gas, then controls the size of ring body.
6. engine turbine guide duct according to claim 1, which is characterized in that be provided with vibration on the guide duct and pass Sensor.
CN201821349964.7U 2018-08-21 2018-08-21 A kind of engine turbine guide duct Active CN209539443U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821349964.7U CN209539443U (en) 2018-08-21 2018-08-21 A kind of engine turbine guide duct

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821349964.7U CN209539443U (en) 2018-08-21 2018-08-21 A kind of engine turbine guide duct

Publications (1)

Publication Number Publication Date
CN209539443U true CN209539443U (en) 2019-10-25

Family

ID=68244828

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821349964.7U Active CN209539443U (en) 2018-08-21 2018-08-21 A kind of engine turbine guide duct

Country Status (1)

Country Link
CN (1) CN209539443U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114439606A (en) * 2020-10-30 2022-05-06 比亚迪股份有限公司 Air inlet mechanism of engine and engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114439606A (en) * 2020-10-30 2022-05-06 比亚迪股份有限公司 Air inlet mechanism of engine and engine
CN114439606B (en) * 2020-10-30 2023-01-06 比亚迪股份有限公司 Air inlet mechanism of engine and engine

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