CN206513463U - Nozzle overhead integrated form injection valve blender assembly - Google Patents

Nozzle overhead integrated form injection valve blender assembly Download PDF

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Publication number
CN206513463U
CN206513463U CN201720101140.7U CN201720101140U CN206513463U CN 206513463 U CN206513463 U CN 206513463U CN 201720101140 U CN201720101140 U CN 201720101140U CN 206513463 U CN206513463 U CN 206513463U
Authority
CN
China
Prior art keywords
nozzle
gas
combustion gas
track
gas mixer
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.)
Expired - Fee Related
Application number
CN201720101140.7U
Other languages
Chinese (zh)
Inventor
柏长宏
黄伟
陈智勋
彭川
冶雨航
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing Heavy Passenger Automotive Electronics Co Ltd
Original Assignee
Chongqing Heavy Passenger Automotive Electronics Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chongqing Heavy Passenger Automotive Electronics Co Ltd filed Critical Chongqing Heavy Passenger Automotive Electronics Co Ltd
Priority to CN201720101140.7U priority Critical patent/CN206513463U/en
Application granted granted Critical
Publication of CN206513463U publication Critical patent/CN206513463U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • Y02T10/30Use of alternative fuels, e.g. biofuels

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  • Fuel-Injection Apparatus (AREA)

Abstract

The utility model discloses a kind of nozzle overhead integrated form injection valve blender assembly, pole including inlet suction port, combustion gas guide rail, fuel gas temperature pressure sensor, nozzle and nozzle beam, blender and support and connection combustion gas track and gas mixer, the inlet end of nozzle is connected on combustion gas track, the outlet side of nozzle is connected on gas mixer, and is additionally provided with beam between nozzle and combustion gas track and between nozzle and gas mixer.The utility model is applied to the gas nozzle of 2~8 air intake structures from top to down, nozzle is directly connected with gas mixer, reduce the pipeline connection between combustion gas guide rail and gas mixer, improve the response speed of engine control system, improve engine transient control accuracy, improve discharge, optimize engine performance;And it is furnished with beam on nozzle, beam can absorb the vibration energy that engine passes to nozzle, it is to avoid gas mixer is damaged because of rigidity vibration, can extend nozzle life.

Description

Nozzle overhead integrated form injection valve blender assembly
Technical field
The utility model is related to a kind of gas engine technical field, more particularly to a kind of nozzle overhead integrated form injection Valve blender assembly.
Background technology
At present, in gas engine gas supply system, combustion gas enters injection apparatus by pipeline first, by injection apparatus Nozzle spray, nozzle spray gas enter back into gas mixer, realize that gas is uniformly mixed.
In the prior art, fuel gas ejecting device and gas mixer are two kinds of independent structures, pass through pipeline between the two Connection, pipeline connection can not only extend the combustion gas speed of response and engine transient control accuracy, can also increase the trouble point of gas leakage; And nozzle is directly rigidly connected with track in injection apparatus, nozzle is harmful to component effect by engine luggine for a long time, easily Damage, the life-span is shorter.
And gas mixer of the prior art uses cylindrical filter cartridge, gas mixing problem of non-uniform, shadow can be caused Ring function of the engine.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of nozzle overhead integrated form injection valve blender assembly, with Solve the combustion gas speed of response, engine transient control accuracy, integrated level, fuel gas ejecting device longevity that existing gas engine is present Order the technical problems such as the uneven influence function of the engine of short, gas mixing.
The utility model nozzle overhead integrated form injection valve blender assembly, including combustion gas guide rail, the combustion gas track One end is connected with inlet suction port, and the other end of combustion gas track is connected with the sensor of detection fuel gas temperature and pressure;
Also include nozzle, gas mixer and connection combustion gas track and gas mixer pole, it is described from top to down The nozzle of structure is vertical with combustion gas track, and the inlet end of nozzle is connected on combustion gas track, and the outlet side of nozzle is connected to gas On blender, and beam is additionally provided between nozzle and combustion gas track and between nozzle and gas mixer;
Also include the support being connected on gas mixer.
Further, there is axial air flue, the annular air channel concentric with axial air flue in the gas mixer and be located at Tubulose filter core in axial air flue, air flue is radially into annular air channel vertically at the two ends of the tubulose filter core.
Further, the tubulose filter core is wing.
Further, the support is L-shaped, and support is connected by screw with gas mixer.
The beneficial effects of the utility model:
1st, the utility model nozzle overhead integrated form injection valve blender assembly, is directly connected using nozzle with gas mixer Connect, reduce the pipeline connection between combustion gas guide rail and gas mixer, lift engine control system response speed, improve Engine transient control accuracy, improves discharge, optimizes engine performance.
2nd, it is furnished with beam, beam on the utility model nozzle overhead integrated form injection valve blender assembly, its nozzle The vibration energy that engine passes to nozzle can be absorbed, it is to avoid gas mixer is damaged because of rigidity vibration, can extend the nozzle longevity Life.
3rd, the utility model nozzle overhead integrated form injection valve blender assembly, the tubulose filter core of its gas mixer is used Wing-shaped structure, can make combustion gas and air is full and uniform mixes, can greatly improve function of the engine.
Brief description of the drawings
Fig. 1 is the structural representation of the present embodiment nozzle overhead integrated form injection valve blender assembly, and arrow is represented in figure The flow direction of gas;
Fig. 2 is the cross-sectional view of tubulose filter core.
Embodiment
The utility model is further described with reference to the accompanying drawings and examples.
As illustrated, the present embodiment nozzle overhead integrated form injection valve blender assembly, including combustion gas guide rail 2, the combustion One end of gas track is connected with inlet suction port 1, and the other end of combustion gas track is connected with the sensor of detection fuel gas temperature and pressure 3;
Also include the pole 4 of nozzle 5, gas mixer 7 and connection combustion gas track and gas mixer, it is described supreme And the nozzle of lower structure is vertical with combustion gas track, the inlet end of nozzle is connected on combustion gas track, and the outlet side of nozzle is connected to Beam 6 is additionally provided with gas mixer, and between nozzle and combustion gas track and between nozzle and gas mixer;
Also include the support 8 being connected on gas mixer.
The operation principle of the present embodiment nozzle overhead integrated form injection valve blender assembly is:Combustion gas is entered along fuel gas pipeline Enter combustion gas guide rail, the sensor of combustion gas rail end detects the temperature and pressure of combustion gas, and by the telecommunications of fuel gas temperature and pressure Number send controller to, controller sends instruction, acts on nozzle, accurate control jet amount, the combustion gas of ejection enters gas In body blender, uniformly mixed with air by filter core, into engine working cylinder.
The present embodiment nozzle overhead integrated form injection valve blender assembly, using structure from top to down nozzle directly and gas Body blender is connected, and is reduced the pipeline connection between combustion gas guide rail and gas mixer, is improved engine control system phase Speed is answered, engine transient control accuracy is improved, improves discharge, optimizes engine performance.
And it is furnished with beam, beam on the present embodiment nozzle overhead integrated form injection valve blender assembly, its nozzle The vibration energy that engine passes to nozzle can be absorbed, it is to avoid gas mixer is damaged because of rigidity vibration, can extend the nozzle longevity Life.
Have in the present embodiment, in the gas mixer axial air flue 9, the annular air channel 10 concentric with axial direction air flue, And the tubulose filter core 11 in axial air flue, air flue is radially into annular air channel vertically at the two ends of the tubulose filter core In, combustion gas enters tubulose filter core through annular air channel from two ends, is mixed in tubulose filter core with air, combustion gas mixing is uniform.And this Embodiment injection mixing control assembly, tubulose filter core can strengthen gas using the wing-shaped structure of similar aircraft wing as shown in Figure 2 Continuation mixed process of the body after tubulose cartridge surface is flowed through, can preferably be such that combustion gas is uniformly mixed with air, eliminate combustion gas The problem of mixing is uneven, can greatly improve function of the engine.
In the present embodiment, the support 8 is L-shaped, and support is connected by screw 12 with gas mixer, easy to assembly.
Finally illustrate, above example is only unrestricted to illustrate the technical solution of the utility model, although ginseng The utility model is described in detail according to preferred embodiment, it will be understood by those within the art that, can be to this The technical scheme of utility model is modified or equivalent substitution, without departing from the objective and model of technical solutions of the utility model Enclose, it all should cover among right of the present utility model.

Claims (4)

1. a kind of nozzle overhead integrated form injection valve blender assembly, it is characterised in that:Including combustion gas guide rail, the combustion gas track One end be connected with inlet suction port, the other end of combustion gas track is connected with the sensor of detection fuel gas temperature and pressure;
Also include the pole of nozzle, gas mixer and connection combustion gas track and gas mixer, the nozzle and combustion gas rail Road is vertical, and the inlet end of nozzle is connected on combustion gas track, and the outlet side of nozzle is connected on gas mixer, and nozzle and combustion Beam is additionally provided between gas track and between nozzle and gas mixer;
Also include the support being connected on gas mixer.
2. nozzle overhead integrated form injection valve blender assembly according to claim 1, it is characterised in that:The gas is mixed There is axial air flue, the annular air channel concentric with axial air flue and the tubulose filter core in axial air flue in clutch, it is described Air flue is radially into annular air channel vertically at the two ends of tubulose filter core.
3. nozzle overhead integrated form injection valve blender assembly according to claim 2, it is characterised in that:The tubular filter Core is wing.
4. nozzle overhead integrated form injection valve blender assembly according to claim 1, it is characterised in that:The support is L-shaped, and support is connected by screw with gas mixer.
CN201720101140.7U 2017-01-24 2017-01-24 Nozzle overhead integrated form injection valve blender assembly Expired - Fee Related CN206513463U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720101140.7U CN206513463U (en) 2017-01-24 2017-01-24 Nozzle overhead integrated form injection valve blender assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720101140.7U CN206513463U (en) 2017-01-24 2017-01-24 Nozzle overhead integrated form injection valve blender assembly

Publications (1)

Publication Number Publication Date
CN206513463U true CN206513463U (en) 2017-09-22

Family

ID=59865954

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720101140.7U Expired - Fee Related CN206513463U (en) 2017-01-24 2017-01-24 Nozzle overhead integrated form injection valve blender assembly

Country Status (1)

Country Link
CN (1) CN206513463U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112145319A (en) * 2019-06-28 2020-12-29 上海海能汽车电子有限公司 Integrated mixer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112145319A (en) * 2019-06-28 2020-12-29 上海海能汽车电子有限公司 Integrated mixer

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170922

Termination date: 20210124