CN102716827B - Gas-liquid two-phase pressure-balanced wide-angle uniformly-distributed mist nozzle - Google Patents
Gas-liquid two-phase pressure-balanced wide-angle uniformly-distributed mist nozzle Download PDFInfo
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- 239000007788 liquid Substances 0.000 title claims abstract description 121
- 239000003595 mist Substances 0.000 title claims abstract description 27
- 241000237942 Conidae Species 0.000 claims 1
- 238000009826 distribution Methods 0.000 abstract description 3
- 238000007599 discharging Methods 0.000 abstract 2
- 238000000889 atomisation Methods 0.000 description 22
- 239000012071 phase Substances 0.000 description 14
- 230000000694 effects Effects 0.000 description 12
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- 239000007921 spray Substances 0.000 description 6
- 239000000243 solution Substances 0.000 description 5
- 230000005514 two-phase flow Effects 0.000 description 5
- 238000005520 cutting process Methods 0.000 description 4
- 238000002156 mixing Methods 0.000 description 3
- 238000009827 uniform distribution Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 238000006477 desulfuration reaction Methods 0.000 description 2
- 230000023556 desulfurization Effects 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000003513 alkali Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Abstract
Description
技术领域 technical field
本发明涉及适用于烟尘净化、脱硫脱硝、气体降温、喷涂和消防等领域的气液两相流雾化喷嘴,尤其是指一种气液两相压平衡广角均布细雾喷嘴。The invention relates to a gas-liquid two-phase flow atomizing nozzle suitable for the fields of smoke and dust purification, desulfurization and denitrification, gas cooling, spraying and fire protection, especially a gas-liquid two-phase pressure balanced wide-angle uniformly distributed fine mist nozzle.
技术背景 technical background
雾化喷嘴有两种:单液体雾化喷嘴和气液两相雾化喷嘴。There are two types of atomizing nozzles: single-liquid atomizing nozzles and gas-liquid two-phase atomizing nozzles.
单液体雾化喷嘴的雾化机理主要是丝状分裂,液体以很高的速度从喷孔射出,在表面张力和液体与外界静止空气间的摩擦力作用下,液柱变成蛇状振动的液丝,然后断裂成雾。单液体雾化喷嘴的雾化效果较差,如果要产生平均直径小于100微米的雾滴,必须采用小喷孔、高液压,这种结构的单液体雾化喷嘴存在的问题是:孔口易堵塞,雾化质量差。The atomization mechanism of the single-liquid atomizing nozzle is mainly filiform splitting. The liquid is ejected from the nozzle hole at a high speed. Under the action of surface tension and friction between the liquid and the still air outside, the liquid column becomes a snake-like vibration. Liquid filaments, then break into mist. The atomization effect of the single-liquid atomizing nozzle is poor. If you want to produce droplets with an average diameter of less than 100 microns, you must use small nozzle holes and high hydraulic pressure. The problem with this structure of the single-liquid atomizing nozzle is: the orifice is easy to Blockage, poor atomization quality.
气液两相雾化喷嘴主要是采用压缩空气冲击液流提高雾化质量,大幅度降低液压。由于气液两相雾化喷嘴比单液体雾化喷嘴有更好的雾化性能,因此,气液两相雾化喷嘴得到越来越广泛的使用。The gas-liquid two-phase atomizing nozzle mainly uses compressed air to impact the liquid flow to improve the atomization quality and greatly reduce the hydraulic pressure. Because gas-liquid two-phase atomizing nozzles have better atomization performance than single-liquid atomizing nozzles, gas-liquid two-phase atomizing nozzles are more and more widely used.
气液两相雾化喷嘴的雾化机理主要是膜状分裂,当气液混合流以相当高的速度从压力式喷嘴喷出时,能形成液包气的薄膜状雾滴群,气体膨胀使液膜破裂成雾,增大气压,降低液量可进一步提高雾化效果。气液两相雾化喷嘴有两种型式:引射型和气液碰撞型。The atomization mechanism of the gas-liquid two-phase atomizing nozzle is mainly film splitting. When the gas-liquid mixed flow is ejected from the pressure nozzle at a relatively high speed, it can form a film-like droplet group with gas in the liquid, and the gas expands to make it The liquid film breaks into fog, increasing the air pressure and reducing the liquid volume can further improve the atomization effect. There are two types of gas-liquid two-phase atomizing nozzles: ejection type and gas-liquid collision type.
引射型喷嘴所需的液压极低,可以是常压(环境大气压),仅靠高速气流在文丘里管喉部产生的负压就可能将液体吸入文丘里管中,使气液混合形成雾滴。引射型喷嘴存在的主要问题是雾化质量不稳定,原因有两种:The hydraulic pressure required by the injection nozzle is extremely low, which can be normal pressure (ambient atmospheric pressure), and the negative pressure generated by the high-speed airflow at the throat of the Venturi tube may suck the liquid into the Venturi tube, making the gas and liquid mix to form a mist drop. The main problem with ejector nozzles is that the atomization quality is not stable for two reasons:
一是液体不能吸入引射型喷嘴导致不能形成液雾:根据气体射流的扩散规律,当喉嘴距过大时,气体射流截面积在进入喉管之前已扩散到大于喉管面积,喉管对射流成为单纯的阻力,从而使喷射器无法抽吸液体不能形成液雾。另外,引射流气体喷射存在气流速度下限。如果喷口气速低于下限,所产生的负压不够,液体无法吸入喷头,不能形成液雾(参见:吴伟烽,冯全科,向清江,吕俊贤。气-液喷射器内两相流流型分析。核动力工程。2007,28(6),34-37)。One is that the liquid cannot be sucked into the injection nozzle, so that the liquid mist cannot be formed: according to the diffusion law of the gas jet, when the distance between the throat and mouth is too large, the cross-sectional area of the gas jet has diffused to be larger than the area of the throat before entering the throat, and the throat is relatively large. The jet flow becomes a mere drag, so that the injector cannot pump the liquid and form a liquid mist. In addition, there is a lower limit to the gas flow velocity of the jet flow gas injection. If the nozzle gas velocity is lower than the lower limit, the negative pressure generated is not enough, the liquid cannot be sucked into the nozzle, and the liquid mist cannot be formed (see: Wu Weifeng, Feng Quanke, Xiang Qingjiang, Lu Junxian. Analysis of the two-phase flow flow pattern in the gas-liquid injector. Kernel Power Engineering. 2007, 28(6), 34-37).
二是混合室中的回流作用导致无法正常喷雾:在气体喷口和文氏管之间是气液混合室,气体喷口产生的高速射流区外侧是回流区,回流区随着背压的升高不断向混合室入口处移动,当背压超过一定程度时,入口处将出现严重的回流现象,导致引射型喷嘴工作终止(参见:王厚庆,沈超,王晓娟,陈炳录,张鹤飞。气液两相流引射器的数值仿真及实验研究。石油机械。2005,33(9),21-23)。The second is that the backflow effect in the mixing chamber makes it impossible to spray normally: there is a gas-liquid mixing chamber between the gas nozzle and the Venturi tube, and the outside of the high-speed jet area generated by the gas nozzle is the backflow zone, and the backflow zone continues to flow with the increase of back pressure. The entrance of the mixing chamber moves, and when the back pressure exceeds a certain level, serious backflow will occur at the entrance, resulting in the termination of the injection nozzle (see: Wang Houqing, Shen Chao, Wang Xiaojuan, Chen Binglu, Zhang Hefei. Gas-liquid two-phase flow introduction Numerical simulation and experimental research of injector. Petroleum Machinery. 2005, 33(9), 21-23).
气液碰撞型喷嘴主要靠高速气液间的相互碰撞产生雾化,气液碰撞型喷嘴有较好的雾化稳定性,但也有不足之处:Gas-liquid collision nozzles mainly rely on high-speed gas-liquid collisions to generate atomization. Gas-liquid collision nozzles have better atomization stability, but there are also shortcomings:
1、液相喷口易堵塞。由于气液碰撞型喷嘴是靠高速气液间的相互碰撞产生雾化,因此就要求液相喷口的直径很小(通常小于1mm),使喷液成为很细的液柱,这样才容易在高速气流的冲击下破碎成雾(参见:杨立军,王维。两相流乳化型细水雾喷嘴雾化特性研究,北京航空航天大学学报,2002,28(4),413-416)。如果液体有杂质(如湿法脱硫喷碱液有固体颗粒,喷油雾有油垢等),细喷口极易堵塞。1. The liquid phase nozzle is easy to block. Since the gas-liquid collision nozzle is atomized by the collision between gas and liquid at high speed, the diameter of the liquid phase nozzle is required to be small (usually less than 1mm), so that the spray liquid becomes a very fine liquid column, so that it is easy to spray at high speed. Under the impact of the airflow, it breaks into fog (see: Yang Lijun, Wang Wei. Research on atomization characteristics of two-phase flow emulsified water mist nozzle, Journal of Beijing University of Aeronautics and Astronautics, 2002, 28 (4), 413-416). If the liquid has impurities (such as solid particles in the wet desulfurization spray alkali solution, oily dirt in the oil spray mist, etc.), the fine nozzles are easily blocked.
2、气液两相雾化作用没有得到充分发挥。碰撞型喷嘴仅有高速气液间的相互碰撞作用,没有利用气液两相流之间的剪切力。2. The gas-liquid two-phase atomization effect has not been fully exerted. Collision nozzles only have the collision effect between high-speed gas and liquid, and do not use the shear force between gas and liquid two-phase flow.
3、气液碰撞型喷嘴所需液压高于引射型喷嘴。3. The hydraulic pressure required by the gas-liquid collision type nozzle is higher than that of the ejection type nozzle.
为了克服引射型喷嘴雾化质量不稳定的问题,同时有效发挥气液碰撞型喷嘴的雾化潜力,中国发明专利ZL 2009 1 0063156.3,公开了一种采用下旋压缩气流,并利用高速气流对液柱的冲击作用,结合高速旋转气流对液柱的剪切作用,从而使液柱更易破碎形成液雾。尽管两相旋流大口径细雾喷嘴极大地改善了雾化效果,但仍有存在以缺陷:In order to overcome the problem of unstable atomization quality of ejection nozzles and effectively utilize the atomization potential of gas-liquid collision nozzles, Chinese invention patent ZL 2009 1 0063156.3 discloses a method that uses down-swirling compressed airflow and uses high-speed airflow to The impact of the liquid column, combined with the shearing effect of the high-speed rotating air flow on the liquid column, makes the liquid column more easily broken to form a liquid mist. Although the two-phase swirl large-diameter fine mist nozzle has greatly improved the atomization effect, there are still some defects:
1、所需的液压较高(通常大于0.2MPa)。1. The required hydraulic pressure is high (usually greater than 0.2MPa).
2、由于在气流和液体接触面上的压力不等,导致喷嘴末端的各个喷孔喷出的液量不等。2. Due to the unequal pressure on the contact surface between the air flow and the liquid, the amount of liquid ejected from each nozzle hole at the end of the nozzle is unequal.
3、对于所有多孔喷嘴,无论是多孔单液体雾化喷嘴还是多孔气液两相雾化喷嘴,两股雾化射流之间总存在喷雾分布不均的现象,该问题到目前为止还没有得到很好地解决。3. For all porous nozzles, whether it is a porous single-liquid atomizing nozzle or a porous gas-liquid two-phase atomizing nozzle, there is always a phenomenon of uneven spray distribution between the two atomizing jets. This problem has not been well understood so far. well resolved.
发明内容 Contents of the invention
本发明的目的就是要克服上述技术缺陷,提供一种雾化分布均匀性好、结构简单且不会发生堵塞的气液两相压平衡广角均布细雾喷嘴。The purpose of the present invention is to overcome the above-mentioned technical defects and provide a gas-liquid two-phase pressure balanced wide-angle uniform distribution fine mist nozzle with good atomization distribution uniformity, simple structure and no clogging.
为实现上述目的,本发明所设计的气液两相压平衡广角均布细雾喷嘴,包括喷嘴壳体,所述喷嘴壳体上设置有进液管和进气管,还包括由文丘里回转体和螺旋槽式内芯构成的文丘里喷射器,所述文丘里回转体嵌置固定在喷嘴壳体的内腔中,所述螺旋槽式内芯插入固定在文丘里回转体的中间空腔中;所述文丘里回转体上设置有环状均压室,所述环状均压室与进液管相连通,所述环状均压室的内侧开设有出液环缝;所述螺旋槽式内芯和文丘里回转体之间由内至外依次形成文丘里喷射器的环状渐缩段、环状喉管段和环状渐扩段,所述环状渐缩段与进气管相通,所述环状喉管段与出液环缝相通,所述环状渐扩段与外界相通。In order to achieve the above object, the gas-liquid two-phase pressure balance wide-angle uniform distribution fine mist nozzle designed by the present invention includes a nozzle housing, which is provided with a liquid inlet pipe and an air inlet pipe, and also includes a Venturi gyrator A Venturi injector composed of a spiral grooved inner core, the Venturi rotary body is embedded and fixed in the inner cavity of the nozzle housing, and the spiral grooved inner core is inserted and fixed in the middle cavity of the Venturi rotary body ; The Venturi gyrator is provided with an annular pressure equalizing chamber, the annular pressure equalizing chamber communicates with the liquid inlet pipe, and the inner side of the annular pressure equalizing chamber is provided with a liquid outlet annular seam; the spiral groove The annular tapering section, the annular throat section and the annular expanding section of the Venturi injector are sequentially formed between the inner core and the Venturi gyrator, and the annular tapering section communicates with the intake pipe. The annular throat section communicates with the liquid outlet annular seam, and the annular gradually expanding section communicates with the outside world.
上述技术方案中,所述环状均压室由文丘里回转体上的环形凹槽与喷嘴壳体的圆筒内壁围合而成。In the above technical solution, the annular pressure equalizing chamber is enclosed by the annular groove on the Venturi gyrator and the inner wall of the nozzle housing.
上述技术方案中,所述螺旋槽式内芯包括内侧圆锥段、中间螺柱段和外侧锥台段;所述文丘里回转体包括内侧倒锥筒段、中间圆筒段和外侧锥筒段;所述内侧圆锥段与内侧倒锥筒段之间形成环状渐缩段,所述中间螺柱段与中间圆筒段之间形成环状喉管段,所述外侧锥台段与外侧锥筒段之间形成环状渐扩段。In the above technical solution, the spiral groove type inner core includes an inner conical section, a middle stud section and an outer frustum section; the Venturi gyrator includes an inner inverted cone section, a middle cylinder section and an outer cone section; An annular tapering section is formed between the inner conical section and the inner inverted cone section, an annular throat section is formed between the middle stud section and the middle cylinder section, and the outer frustum section and the outer cone section are An annular gradually expanding segment is formed between them.
上述技术方案中,所述喷嘴壳体由锥筒段壳体和圆筒段壳体组合而成,所述进气管设置在锥筒段壳体的顶端上,所述文丘里回转体嵌置固定在圆筒段壳体的内腔中,所述进液管设置在圆筒段壳体的侧壁上。In the above technical solution, the nozzle housing is composed of a cone section casing and a cylinder section casing, the air inlet pipe is arranged on the top end of the cone section casing, and the Venturi rotator is embedded and fixed In the inner cavity of the cylinder section shell, the liquid inlet pipe is arranged on the side wall of the cylinder section shell.
上述技术方案中,所述螺旋槽式内芯的轴心线与进气管的轴心线重合、与进液管的轴心线垂直,且三者的轴心线位于同一平面内。In the above technical solution, the axis of the spiral grooved inner core coincides with the axis of the inlet pipe, is perpendicular to the axis of the liquid inlet pipe, and the axes of the three are located in the same plane.
本发明采用上述技术方案,具有以下显著技术进步和有益效果:The present invention adopts the above-mentioned technical scheme, and has the following significant technical progress and beneficial effects:
1、将文丘里引射雾化作用与流体动力旋切雾化作用相结合,一方面,利用引射型喷嘴的高速气流负压吸液作用,有效降低了供液压力,利用高速气流在文丘里喷射器中的负压引射作用,将环状均压室中的液体通过进液环缝吸入到螺旋沟槽中,使液流与高速气流混合雾化,因此所需的液压为常压或低压,具有节能功效;另一方面,利用气液旋流喷嘴的冲击旋切作用,使液体的雾化更加充分,产生的雾粒径更小。1. Combining Venturi injection atomization with hydrodynamic rotary cutting atomization, on the one hand, using the high-speed airflow negative pressure suction effect of the injection nozzle, effectively reducing the liquid supply pressure, using high-speed airflow in the Venturi The negative pressure injection in the inner injector sucks the liquid in the annular pressure equalizing chamber into the spiral groove through the liquid inlet annular gap, so that the liquid flow and the high-speed air flow are mixed and atomized, so the required hydraulic pressure is normal pressure Or low pressure, which has the effect of energy saving; on the other hand, the impact rotary cutting effect of the gas-liquid swirl nozzle is used to make the atomization of the liquid more sufficient and the particle size of the generated mist to be smaller.
2、本发明的进液管与环状均压室相通,环状均压室为大断面环状腔体,因环状均压室的断面积远远大于进液环缝的断面积,所以在环缝进口处的整个气液圆周接触面上压力相等,使液体从进液环缝流入每个螺旋沟槽中的流量相同,根据压平衡原理,环状均压室和进液环缝之间的整个环形圆周气液接触面上的压力处处相等,有效解决了进液压力不平衡问题,提高了喷雾均匀性。2. The liquid inlet pipe of the present invention communicates with the annular pressure equalizing chamber, which is a large-section annular cavity. Because the cross-sectional area of the annular pressure equalizing chamber is much larger than the cross-sectional area of the liquid inlet annular seam, the The pressure on the entire gas-liquid circumferential contact surface at the entrance of the annular seam is equal, so that the flow rate of the liquid flowing from the liquid inlet annular seam into each spiral groove is the same. According to the principle of pressure balance, the gap between the annular pressure equalization chamber and the liquid inlet annular seam The pressure on the gas-liquid contact surface of the entire annular circumference is equal everywhere, which effectively solves the problem of unbalanced liquid inlet pressure and improves the uniformity of spraying.
3、文丘里喷射器的喉管段采用螺旋沟槽设计,利用气流在沟槽中的高速旋切雾化作用,将液流剪切破碎,使液体雾化,雾化效果好。3. The throat section of the Venturi injector adopts a spiral groove design, and the high-speed rotary cutting atomization effect of the air flow in the groove is used to shear and break the liquid flow, so that the liquid is atomized, and the atomization effect is good.
4、本发明的液雾是从文丘里喷射器末端的环状渐扩喇叭口喷出,喇叭口的通道很宽,有效避免了堵塞的现象,并且喷出的液雾形态呈旋转伞状,提高了整个360°角范围内的雾化均匀性。4. The liquid mist of the present invention is sprayed from the annular gradually expanding bell mouth at the end of the Venturi injector. The channel of the bell mouth is very wide, which effectively avoids the phenomenon of clogging, and the shape of the sprayed liquid mist is in the shape of a rotating umbrella. Improved atomization uniformity over the entire 360° angle range.
5、本发明喷嘴组成的部件中,喷嘴壳体、文丘里回转体和螺旋槽式内芯均为回旋环状结构,加工制作简单,安装方便。5. Among the parts composed of the nozzle of the present invention, the nozzle shell, the Venturi gyrator and the spiral groove inner core are all convoluted ring structures, which are easy to manufacture and easy to install.
附图说明 Description of drawings
图1为一种气液两相压平衡广角均布细雾喷嘴的剖视结构图;Fig. 1 is a sectional structural view of a gas-liquid two-phase pressure balanced wide-angle uniformly distributed fine mist nozzle;
图2为图1的A-A向视图;Fig. 2 is the A-A direction view of Fig. 1;
图3为图1中螺旋槽式内芯的结构示意图;Fig. 3 is the schematic structural view of the spiral groove type inner core in Fig. 1;
图中,进液管1;环状均压室2;进液环缝3;进气管4;喷嘴壳体5(其中:圆锥段壳体5.1、圆柱段壳体5.2);环状渐缩段6;环状喉管段7;环状渐扩段8;螺旋槽式内芯9(其中:内侧圆锥段9.1、中间螺柱段9.2、外侧锥台段9.3);文丘里回转体10(其中:内侧倒锥筒段10.1、中间圆筒段10.2、外侧锥筒段10.3)。In the figure, liquid inlet pipe 1; annular pressure equalizing chamber 2; liquid inlet annular seam 3; air inlet pipe 4; nozzle housing 5 (among them: conical section housing 5.1, cylindrical section housing 5.2); annular tapering section 6; annular throat section 7; annular expanding section 8; spiral groove inner core 9 (among them: inner conical section 9.1, middle stud section 9.2, outer frustum section 9.3); Venturi gyrator 10 (among them: The inner inverted cone section 10.1, the middle cylinder section 10.2, and the outer cone section 10.3).
具体实施方式 Detailed ways
以下结合附图和具体实施例对本发明作进一步的详细说明:Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:
图中所示的气液两相压平衡广角均布细雾喷嘴,包括喷嘴壳体5,喷嘴壳体5上设置有进液管1和进气管4,还包括由文丘里回转体10和螺旋槽式内芯9构成的文丘里喷射器,文丘里回转体10嵌置固定在喷嘴壳体5的内腔中,螺旋槽式内芯9插入固定在文丘里回转体10的中间空腔中;文丘里回转体10上设置有环状均压室2,环状均压室2与进液管1相连通,环状均压室2的内侧开设有出液环缝3;螺旋槽式内芯9和文丘里回转体10之间由内至外依次形成文丘里喷射器的环状渐缩段6、环状喉管段7和环状渐扩段8,环状渐缩段6与进气管4相通,环状喉管段7与出液环缝3相通,环状渐扩段8与外界相通。The gas-liquid two-phase pressure balance wide-angle uniform fine mist nozzle shown in the figure includes a nozzle housing 5, which is provided with a liquid inlet pipe 1 and an air inlet pipe 4, and also includes a Venturi gyrator 10 and a spiral A Venturi injector composed of a grooved inner core 9, a Venturi rotary body 10 is embedded and fixed in the inner cavity of the nozzle housing 5, and a spiral grooved inner core 9 is inserted and fixed in the middle cavity of the Venturi rotary body 10; The Venturi gyrator 10 is provided with an annular pressure equalizing chamber 2, the annular pressure equalizing chamber 2 is connected with the liquid inlet pipe 1, and the inner side of the annular pressure equalizing chamber 2 is provided with a liquid outlet annular seam 3; the spiral groove inner core Between 9 and the Venturi gyrator 10, the annular tapering section 6, the annular throat section 7 and the annular expanding section 8 of the Venturi injector are sequentially formed from the inside to the outside, and the annular tapering section 6 and the intake pipe 4 In communication, the annular throat section 7 communicates with the liquid outlet annular seam 3, and the annular expanding section 8 communicates with the outside world.
具体地,环状均压室2由文丘里回转体10上的环形凹槽与喷嘴壳体5的圆筒内壁围合而成。螺旋槽式内芯9包括内侧圆锥段9.1、中间螺柱段9.2和外侧锥台段9.3;与螺旋槽式内芯9的三段结构相对应,文丘里回转体10也设有三段结构,包括内侧倒锥筒段10.1、中间圆筒段10.2和外侧锥筒段10.3。内侧圆锥段9.1与内侧倒锥筒段10.1之间形成环状渐缩段6,中间螺柱段9.2与中间圆筒段10.2之间形成环状喉管段7,外侧锥台段9.3与外侧锥筒段10.3之间形成环状渐扩段8。中间螺柱段9.2的外表面上分布有螺旋沟槽,螺旋沟槽与环状均压室2之间通过进液环缝3相通,螺旋沟槽和文丘里回转体10之间为静配合,具体地,螺旋沟槽与文丘里回转体10的内壁点焊,结构更加稳定。Specifically, the annular pressure equalizing chamber 2 is enclosed by an annular groove on the Venturi rotator 10 and the inner wall of the nozzle housing 5 . The spiral groove inner core 9 includes an inner conical section 9.1, a middle stud section 9.2 and an outer frustum section 9.3; corresponding to the three-section structure of the spiral groove inner core 9, the Venturi gyrator 10 is also provided with a three-section structure, including The inner inverted cone section 10.1, the middle cylindrical section 10.2 and the outer cone section 10.3. An annular tapered section 6 is formed between the inner conical section 9.1 and the inner inverted cone section 10.1, an annular throat section 7 is formed between the middle stud section 9.2 and the middle cylindrical section 10.2, and the outer frustum section 9.3 and the outer cone section An annular diverging section 8 is formed between the sections 10.3. There are spiral grooves distributed on the outer surface of the middle stud section 9.2, and the spiral grooves communicate with the annular pressure equalizing chamber 2 through the liquid inlet annular gap 3, and the spiral grooves and the Venturi rotor 10 are in static fit. Specifically, the spiral groove is spot-welded with the inner wall of the Venturi gyrator 10, and the structure is more stable.
本实施例中,螺旋槽式内芯9的轴心线与进气管4的轴心线重合、与进液管1的轴心线垂直,且三者的轴心线位于同一平面内,这样不仅使得气流和液流较为通畅,而且便于机械加工。In this embodiment, the axis line of the spiral groove type inner core 9 coincides with the axis line of the inlet pipe 4, is perpendicular to the axis line of the liquid inlet pipe 1, and the axis lines of the three are located in the same plane, so that not only It makes the air flow and liquid flow more smooth, and it is convenient for machining.
本实施例中,喷嘴壳体5由锥筒段壳体5.1和圆筒段壳体5.2组合而成,进气管4焊接在锥筒段壳体5.1的顶端上,文丘里回转体10嵌置固定在圆筒段壳体5.2的内腔中,进液管1焊接在圆筒段壳体5.2的侧壁上。In this embodiment, the nozzle housing 5 is composed of a cone section casing 5.1 and a cylinder section casing 5.2, the air inlet pipe 4 is welded on the top of the cone section casing 5.1, and the Venturi gyrator 10 is embedded and fixed In the inner cavity of the cylinder section housing 5.2, the liquid inlet pipe 1 is welded on the side wall of the cylinder section housing 5.2.
本发明的工作原理为:Working principle of the present invention is:
进液管1通过塑料管与常压水源连通,进气管4通过塑料管与0.2MPa-0.4MPa的压缩气流供气装置相连通。水通过进液管1流入环状均压室2,当压缩气流沿进气管4进入文丘里喷管环状渐缩段6,气流逐渐加速,当气流进入环状喉管段7时流速达到最大,气流沿螺旋槽式内芯9圆周上的螺旋沟槽高速流动。高速气流所产生的高负压将环状均压室2中的液体沿进液环缝3均匀吸入到螺旋沟槽中,当高速气流与液流在螺旋沟槽中相遇时,高速气流对液流产生强烈的冲击和旋切作用,将液流破碎雾化,形成气液混合流。随后,气液混合流沿螺旋沟槽流入到环状渐扩段8(即喇叭口),气液混合流在环状渐扩段8中进一步膨胀雾化。最后,液雾从环状渐扩段8喷出,形成广角均匀分布的细雾。The liquid inlet pipe 1 communicates with the normal pressure water source through the plastic pipe, and the air inlet pipe 4 communicates with the compressed air supply device of 0.2MPa-0.4MPa through the plastic pipe. Water flows into the annular pressure equalization chamber 2 through the liquid inlet pipe 1. When the compressed air flow enters the annular tapering section 6 of the Venturi nozzle along the inlet pipe 4, the airflow gradually accelerates. When the airflow enters the annular throat section 7, the flow velocity reaches the maximum. The air flow flows at a high speed along the spiral grooves on the circumference of the spiral groove type inner core 9 . The high negative pressure generated by the high-speed air flow sucks the liquid in the annular pressure equalization chamber 2 into the spiral groove evenly along the liquid inlet annular gap 3. When the high-speed air flow and the liquid flow meet in the spiral groove, the high-speed air flow will The flow produces strong impact and rotary cutting, which breaks and atomizes the liquid flow to form a gas-liquid mixed flow. Subsequently, the gas-liquid mixed flow flows into the annular diverging section 8 (that is, the bell mouth) along the spiral groove, and the gas-liquid mixed flow is further expanded and atomized in the annular diverging section 8 . Finally, the liquid mist is sprayed from the annular diverging section 8 to form a fine mist with a wide angle and uniform distribution.
Claims (4)
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