CN114682405A - An internal swirl cross-hole injector - Google Patents
An internal swirl cross-hole injector Download PDFInfo
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- CN114682405A CN114682405A CN202011640930.5A CN202011640930A CN114682405A CN 114682405 A CN114682405 A CN 114682405A CN 202011640930 A CN202011640930 A CN 202011640930A CN 114682405 A CN114682405 A CN 114682405A
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- 230000008602 contraction Effects 0.000 claims 1
- 229910003460 diamond Inorganic materials 0.000 claims 1
- 239000010432 diamond Substances 0.000 claims 1
- 239000012530 fluid Substances 0.000 abstract description 14
- 238000000889 atomisation Methods 0.000 abstract description 11
- 230000000694 effects Effects 0.000 abstract description 7
- 238000002156 mixing Methods 0.000 abstract description 7
- 239000007921 spray Substances 0.000 abstract description 5
- 238000001704 evaporation Methods 0.000 abstract description 3
- 230000008020 evaporation Effects 0.000 abstract description 3
- 238000002347 injection Methods 0.000 abstract description 3
- 239000007924 injection Substances 0.000 abstract description 3
- 239000002245 particle Substances 0.000 abstract description 3
- 239000000446 fuel Substances 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 3
- 229920005591 polysilicon Polymers 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 238000003491 array Methods 0.000 description 2
- 239000003638 chemical reducing agent Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- -1 burning will occur Chemical compound 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- ZDHXKXAHOVTTAH-UHFFFAOYSA-N trichlorosilane Chemical compound Cl[SiH](Cl)Cl ZDHXKXAHOVTTAH-UHFFFAOYSA-N 0.000 description 1
- 239000005052 trichlorosilane Substances 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/02—Spray pistols; Apparatus for discharge
- B05B7/04—Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
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- Fuel-Injection Apparatus (AREA)
Abstract
本发明公开了一种内部旋流交叉孔喷射器。包括第一腔体、第二腔体、第一通道、第二通道、第三通道、第三腔体和第四腔体;第一腔体外侧依次设置有第二腔体、第三腔体;第一腔体下部设置有第四腔体;第一腔体与第二腔体通过第一通道相连通;第一腔体与第四腔体通过第二通道相连通;第三腔体与第四腔体通过第三通道相连通;第一腔体、第二腔体、第三腔体和第四腔体均同轴。本发明第二通道为第二流体提供空间旋流导向,形成旋流后迅速辅助第一流体破碎雾化,增强雾化效果;第三流体通过第三通道旋流后在第四腔体与喷雾碰撞,能够加强扰动效果;在相同喷射压力下喷雾粒径减小25%以上,流体蒸发、雾化及混合效率提升50%以上。The invention discloses an internal swirl cross-hole injector. It includes a first cavity, a second cavity, a first channel, a second channel, a third channel, a third cavity and a fourth cavity; the outside of the first cavity is sequentially provided with a second cavity and a third cavity The lower part of the first cavity is provided with a fourth cavity; the first cavity is communicated with the second cavity through the first channel; the first cavity and the fourth cavity are communicated through the second channel; the third cavity is connected with The fourth cavity is communicated through the third channel; the first cavity, the second cavity, the third cavity and the fourth cavity are all coaxial. The second channel of the present invention provides a space swirl guide for the second fluid, and after the swirl is formed, it quickly assists the first fluid to be broken and atomized to enhance the atomization effect; Collision can strengthen the disturbance effect; under the same injection pressure, the spray particle size is reduced by more than 25%, and the fluid evaporation, atomization and mixing efficiency is increased by more than 50%.
Description
技术领域technical field
本发明涉及喷射器及喷嘴技术领域,特别是一种内部旋流交叉孔喷射器。The invention relates to the technical field of injectors and nozzles, in particular to an internal swirl cross-hole injector.
背景技术Background technique
喷射器应用在很多种喷淋、喷雾、喷油、喷砂、喷涂等设备里,起着重要的作用,是影响流体雾化效果非常关键的一个部件。喷射器在行业中的应用非常广泛,但现有技术中喷射器流体混合均匀性差,在相同喷射压力下喷雾粒径大,流体蒸发、雾化及混合效率低。The ejector is used in many kinds of spraying, spraying, oil spraying, sandblasting, spraying and other equipment, plays an important role, and is a very critical component that affects the effect of fluid atomization. The ejector is widely used in the industry, but in the prior art, the fluid mixing uniformity of the ejector is poor, the spray particle size is large under the same injection pressure, and the fluid evaporation, atomization and mixing efficiency are low.
例如内燃机领域发动机缸内燃油雾化喷射过程中,燃油的雾化效果对于燃油燃烧效果的影响非常大,由此直接影响污染物的排放量。随着国家排放法规日益严苛,对于燃油喷射器的要求越来越严格。For example, in the process of in-cylinder fuel atomization in the field of internal combustion engines, the atomization effect of fuel has a great influence on the fuel combustion effect, which directly affects the emission of pollutants. With the increasingly stringent national emission regulations, the requirements for fuel injectors are becoming more and more stringent.
例如发动机后处理系统中为降低NOx排放量,向尾气中喷射还原剂,与NOx混合后在SCR系统中进行反应,降低排放。但是还原剂雾化效果有待提高,并且存在结晶问题。For example, in order to reduce NOx emissions in the engine aftertreatment system, a reducing agent is injected into the exhaust gas, mixed with NOx, and then reacted in the SCR system to reduce emissions. However, the atomization effect of the reducing agent needs to be improved, and there is a problem of crystallization.
例如多晶硅生产领域的三氯氢硅和氢气的混合气经由混合气喷嘴进入还原炉的炉腔内,在高温高压下完成反应,生成的硅沉积在硅芯棒上。但过程中会生成不合格形状多晶硅,严重时出现烧流等熔硅现象,大大降低了多晶硅的外观品质,不利于产品处理和销售。For example, the mixed gas of trichlorosilane and hydrogen in the field of polysilicon production enters the furnace cavity of the reduction furnace through the mixed gas nozzle, and the reaction is completed under high temperature and high pressure, and the generated silicon is deposited on the silicon mandrel. However, in the process, unqualified polysilicon will be generated, and in severe cases, the phenomenon of melting silicon such as burning will occur, which greatly reduces the appearance quality of polysilicon and is not conducive to product handling and sales.
发明内容SUMMARY OF THE INVENTION
本发明的目的是提供一种内部旋流交叉孔喷射器,以解决上述技术问题。The purpose of the present invention is to provide an internal swirl cross-hole injector to solve the above-mentioned technical problems.
为解决上述技术问题,本发明采取了如下技术方案:In order to solve the above-mentioned technical problems, the present invention has adopted the following technical solutions:
一种内部旋流交叉孔喷射器,包括第一腔体、第二腔体、第一通道、第二通道、第三通道、第三腔体和第四腔体;所述第一腔体外侧依次设置有第二腔体、第三腔体;所述第一腔体下部设置有第四腔体;所述第一腔体与第二腔体通过第一通道相连通;所述第一腔体与第四腔体通过第二通道相连通;所述第三腔体与第四腔体通过第三通道相连通;所述第一腔体、第二腔体、第三腔体和第四腔体均同轴。An internal swirl cross-hole injector, comprising a first cavity, a second cavity, a first channel, a second channel, a third channel, a third cavity and a fourth cavity; the outside of the first cavity A second cavity and a third cavity are arranged in sequence; a fourth cavity is arranged at the lower part of the first cavity; the first cavity is communicated with the second cavity through a first channel; the first cavity The body is communicated with the fourth cavity through the second channel; the third cavity is communicated with the fourth cavity through the third channel; the first cavity, the second cavity, the third cavity and the fourth cavity The cavities are all coaxial.
进一步的,所述第一通道和第三通道轴截面形状为直筒型、渐缩型、渐扩型、渐缩渐扩型、渐扩渐缩型中的一种。Further, the axial cross-sectional shape of the first channel and the third channel is one of a straight cylinder type, a tapered type, a gradually expanded type, a tapered and expanded type, and a gradually expanded and tapered type.
进一步的,第一通道和第三通道横截面形状为圆形、椭圆形、方形、菱形、狭缝形、间断式圆环形、三角形、圆角矩形中的一种。Further, the cross-sectional shape of the first channel and the third channel is one of a circle, an ellipse, a square, a rhombus, a slit, an intermittent circular ring, a triangle, and a rounded rectangle.
进一步的,所述第一通道和第三通道均倾斜设置,且所述第一通道靠近所述第一腔体的一端向所述第二通道一侧倾斜,所述第三通道靠近所述第四腔体的一端向所述第二通道相对的一侧倾斜。Further, both the first channel and the third channel are inclined, and one end of the first channel close to the first cavity is inclined to the side of the second channel, and the third channel is close to the first cavity. One end of the four-cavity body is inclined to the opposite side of the second channel.
进一步的,所述第一通道和第三通道均均阵列设置有多个,且所述第一通道和第三通道轴线均与第一腔体轴线不相交。Further, both the first channel and the third channel are provided with a plurality of arrays, and the axes of the first channel and the third channel do not intersect the axis of the first cavity.
进一步的,第二通道横截面形状为直筒型、渐缩型、渐扩型、渐缩渐扩型、渐扩渐缩型中的一种或几种的组合。Further, the cross-sectional shape of the second channel is one or a combination of straight cylinder, tapered, tapered, tapered tapered, tapered tapered.
进一步的,所述第二通道设有多个,多个所述第二通道的一端均匀分布在所述第一腔体的底部,另一端向所述第一腔体的轴线倾斜并交汇。Further, a plurality of second channels are provided, one end of the plurality of second channels is evenly distributed on the bottom of the first cavity, and the other end is inclined toward the axis of the first cavity and meets.
本发明用于加强流体破碎雾化混合的效果;采用高扰动交叉喷孔,能够有效增强扰动,促进喷雾破碎雾化;带有旋流的第二流体高速射向流体第一腔体,与第一腔体内的第一流体充分混合,第三流体通过第三通道射向第四腔体,加强混合并辅助其雾化。本发明提供的喷射器能够有效提高流体混合均匀性,在相同喷射压力下喷雾粒径减小25%以上,流体蒸发、雾化及混合效率提升50%以上。The present invention is used to strengthen the effect of fluid crushing, atomization and mixing; high-turbulence cross-spray holes are used, which can effectively enhance the turbulence and promote spray crushing and atomization; the second fluid with swirling flow shoots toward the fluid first cavity at high speed, and is connected with the first fluid cavity at high speed. The first fluid in a cavity is fully mixed, and the third fluid is ejected to the fourth cavity through the third channel to strengthen the mixing and assist its atomization. The injector provided by the invention can effectively improve the mixing uniformity of the fluid, the spray particle size is reduced by more than 25% under the same injection pressure, and the fluid evaporation, atomization and mixing efficiency is improved by more than 50%.
附图说明Description of drawings
图1为本发明整体结构图。Fig. 1 is the overall structure diagram of the present invention.
图2为本发明实施例中一种第二通道是直筒型的截面图。FIG. 2 is a cross-sectional view of a second channel in an embodiment of the present invention being a straight cylinder.
图3为本发明实施例中一种第二通道子孔道是直筒型的截面图。3 is a cross-sectional view of a second channel sub-channel in an embodiment of the present invention being a straight cylinder.
图4为本发明实施例中一种第二通道子孔道是渐缩型的截面图。4 is a cross-sectional view of a tapered type of second channel sub-channel according to an embodiment of the present invention.
图5为本发明实施例中一种第二通道子孔道是渐扩型的截面图。FIG. 5 is a cross-sectional view of a second channel sub-channel in an embodiment of the present invention being of a gradually expanding type.
图6为本发明实施例中一种第二通道子孔道是渐缩渐扩型的截面图。FIG. 6 is a cross-sectional view of a second channel sub-channel in an embodiment of the present invention that is tapered and expanded.
图7为本发明实施例中一种第二通道子孔道是渐扩渐缩型的截面图。FIG. 7 is a cross-sectional view of a second channel sub-channel in an embodiment of the present invention that is gradually expanding and tapering.
图8为本发明实施例中一种第一通道旋流孔的横截面形状是直筒型的截面图。8 is a cross-sectional view of a first channel swirl hole in an embodiment of the present invention having a straight cylindrical shape.
图9为本发明实施例中一种第一通道旋流孔的横截面形状是渐缩型的截面图。FIG. 9 is a cross-sectional view of a tapered cross-sectional shape of a first channel swirl hole in an embodiment of the present invention.
图10为本发明实施例中一种第一通道旋流孔的横截面形状是渐扩型的截面图。FIG. 10 is a cross-sectional view of a first channel swirl hole in an embodiment of the present invention with a gradually expanding cross-sectional shape.
图11为本发明实施例中一种第一通道旋流孔的横截面形状是渐缩渐扩型的截面图。FIG. 11 is a cross-sectional view of a first channel swirl hole in an embodiment of the present invention in which the cross-sectional shape is tapered and tapered.
图12为本发明实施例中一种第一通道旋流孔的横截面形状是渐扩渐缩型的截面图。FIG. 12 is a cross-sectional view of a first channel swirl hole in an embodiment of the present invention in which the cross-sectional shape is gradually expanding and tapering.
图13为本发明实施例中一种第一通道旋流孔横截面形状是直筒型的与第一腔体轴线不相交的截面图。FIG. 13 is a cross-sectional view of a first channel swirl hole in an embodiment of the present invention, wherein the cross-sectional shape is a straight cylinder and does not intersect with the axis of the first cavity.
图14为本发明实施例中一种第三通道旋流孔的横截面形状是直筒型的截面图。FIG. 14 is a cross-sectional view of a straight cylindrical shape of the cross-sectional shape of a third channel swirl hole in an embodiment of the present invention.
图15为本发明实施例中一种第三通道旋流孔的横截面形状是渐缩型的截面图。FIG. 15 is a cross-sectional view of a tapered cross-sectional shape of a third channel swirl hole in an embodiment of the present invention.
图16为本发明实施例中一种第三通道旋流孔的横截面形状是渐扩型的截面图。FIG. 16 is a cross-sectional view of a third channel swirl hole in an embodiment of the present invention in which the cross-sectional shape is gradually expanding.
图17为本发明实施例中一种第三通道旋流孔的横截面形状是渐缩渐扩型的截面图。Fig. 17 is a cross-sectional view of a third channel swirl hole in an embodiment of the present invention in which the cross-sectional shape is tapered and tapered.
图18为本发明实施例中一种第三通道旋流孔的横截面形状可以是渐扩渐缩型。FIG. 18 is a cross-sectional shape of a third channel swirl hole in an embodiment of the present invention, which may be a gradually expanding and tapering type.
图19为本发明实施例中一种第三通道旋流孔横截面形状是直筒型的与第一腔体轴线不相交的截面图。19 is a cross-sectional view of a third channel swirl hole in an embodiment of the present invention in which the cross-sectional shape is a straight cylinder and does not intersect the axis of the first cavity.
图中:1-第一腔体;2-第二腔体;3-第一通道;4-第二通道;5-第三通道;6-第三腔体;7-第四腔体。In the figure: 1-first cavity; 2-second cavity; 3-first channel; 4-second channel; 5-third channel; 6-third cavity; 7-fourth cavity.
具体实施方式Detailed ways
以下通过附图和实施例对本发明的技术方案作进一步说明。The technical solutions of the present invention will be further described below through the accompanying drawings and embodiments.
结合图1-2本实施例提供一种内部旋流交叉孔喷射器,包括第一腔体1、第二腔体2、第一通道3、第二通道4、第三通道5、第三腔体6和第四腔体7;所述第一腔体1外侧依次设置有第二腔体2、第三腔体6;所述第一腔体1下部设置有第四腔体7;所述第一腔体1与第二腔体2通过第一通道3相连通;所述第一腔体1与第四腔体7通过第二通道4相连通;所述第三腔体6与第四腔体7通过第三通道5相连通;所述第一腔体1、第二腔体2、第三腔体6和第四腔体7均同轴。1-2, the present embodiment provides an internal swirl cross-hole injector, including a first cavity 1, a second cavity 2, a
所述第一通道3和第三通道5轴截面形状为直筒型、渐缩型、渐扩型、渐缩渐扩型、渐扩渐缩型中的一种。The axial cross-sectional shape of the
第一通道3和第三通道5横截面形状为圆形、椭圆形、方形、菱形、狭缝形、间断式圆环形、三角形、圆角矩形中的一种。The cross-sectional shape of the
所述第一通道3和第三通道5均倾斜设置,且所述第一通道3靠近所述第一腔体1的一端向所述第二通道4一侧倾斜,所述第三通道5靠近所述第四腔体7的一端向所述第二通道4相对的一侧倾斜。Both the
所述第一通道3和第三通道5均均阵列设置有多个,且所述第一通道3和第三通道5轴线均与第一腔体1轴线不相交。Both the
第二通道4横截面形状为直筒型、渐缩型、渐扩型、渐缩渐扩型、渐扩渐缩型中的一种或几种的组合。The cross-sectional shape of the
所述第二通道4设有多个,多个所述第二通道4的一端均匀分布在所述第一腔体1的底部,另一端向所述第一腔体1的轴线倾斜并交汇。There are a plurality of
以上所述,仅是本发明较佳实施例而已,并非对本发明的技术范围作任何限制,故凡是依据本发明的技术实质对以上实施例所作的任何细微修改、等同变化与修饰,均仍属于本发明技术方案的范围内。The above are only preferred embodiments of the present invention, and do not limit the technical scope of the present invention. Therefore, any minor modifications, equivalent changes and modifications made to the above embodiments according to the technical essence of the present invention are still within the scope of the present invention. within the scope of the technical solution of the present invention.
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CN110805512A (en) * | 2018-08-05 | 2020-02-18 | 大连理工大学 | Nozzle with torsional composite hole |
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2020
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WO2007080084A1 (en) * | 2006-01-09 | 2007-07-19 | Dieter Wurz | Two-component nozzle |
CN201807473U (en) * | 2010-07-09 | 2011-04-27 | 中冶京诚工程技术有限公司 | New air mist nozzle without air resistance |
CN205413411U (en) * | 2016-03-21 | 2016-08-03 | 深圳市华兴四海机械设备有限公司 | Two -fluid spray tube |
CN110805512A (en) * | 2018-08-05 | 2020-02-18 | 大连理工大学 | Nozzle with torsional composite hole |
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