CN110801954A - Nozzle with partially twisted 8-shaped spray holes - Google Patents
Nozzle with partially twisted 8-shaped spray holes Download PDFInfo
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- CN110801954A CN110801954A CN201810881604.XA CN201810881604A CN110801954A CN 110801954 A CN110801954 A CN 110801954A CN 201810881604 A CN201810881604 A CN 201810881604A CN 110801954 A CN110801954 A CN 110801954A
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- 239000007921 spray Substances 0.000 title abstract description 23
- 238000002347 injection Methods 0.000 abstract description 18
- 239000007924 injection Substances 0.000 abstract description 18
- 239000012530 fluid Substances 0.000 abstract description 13
- 230000000694 effects Effects 0.000 abstract description 6
- 239000002245 particle Substances 0.000 abstract description 4
- 239000013618 particulate matter Substances 0.000 abstract description 3
- 238000009792 diffusion process Methods 0.000 abstract 2
- 239000011148 porous material Substances 0.000 abstract 1
- 230000007423 decrease Effects 0.000 description 12
- 238000010586 diagram Methods 0.000 description 8
- 239000007788 liquid Substances 0.000 description 8
- 239000000446 fuel Substances 0.000 description 7
- 239000000243 solution Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000010146 3D printing Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 2
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- 238000013459 approach Methods 0.000 description 1
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- 238000012545 processing Methods 0.000 description 1
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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
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/34—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
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Abstract
Description
技术领域technical field
本发明涉及流体喷射技术领域,具体而言,尤其涉及一种带部分扭转式8字形喷孔的喷嘴。The present invention relates to the technical field of fluid jetting, in particular, to a nozzle with a partially twisted 8-shaped jetting hole.
背景技术Background technique
在工业、农业、医疗卫生、国防科技等多个领域的应用实践中,均涉及到流体喷射技术,在一定压力下利用喷嘴喷射流体,以实现各自的目的。如在内燃机领域,采用液体燃料时,需要通过压力喷嘴将一定量的液体燃料在极短的时间内喷入进气管路或气缸,形成喷雾,以便燃料与空气快速、充分混合及燃烧,喷嘴作为实施喷射的载体,对液体燃料的喷雾特性有重要影响,进而影响内燃机的燃烧和排放特性。In the application practice in many fields such as industry, agriculture, medical and health, national defense technology, etc., fluid injection technology is involved, and the fluid is injected by nozzles under a certain pressure to achieve their respective purposes. For example, in the field of internal combustion engines, when using liquid fuel, a certain amount of liquid fuel needs to be injected into the intake pipeline or cylinder through a pressure nozzle in a very short time to form a spray, so that the fuel and air can be quickly and fully mixed and burned. The carrier that carries out the injection has an important influence on the spray characteristics of the liquid fuel, which in turn affects the combustion and emission characteristics of the internal combustion engine.
在流体喷嘴中一般需要设置喷孔,喷孔的几何结构及尺寸对喷射特性有重要影响。当前使用最多的是横截面为圆形的喷孔,如柱形喷孔、锥形喷孔,锥形喷孔包括渐缩锥形和渐扩锥形喷孔。Generally, nozzle holes need to be set in the fluid nozzle, and the geometry and size of the nozzle holes have an important influence on the spray characteristics. Currently, the most used nozzles are circular in cross-section, such as cylindrical nozzles and conical nozzles. Conical nozzles include tapered and tapered nozzles.
众所周知,流体喷嘴内部几何结构影响其内部流场特性。如在内燃机领域,液体燃料喷嘴内部几何结构影响其空化气泡生成特性、压力和速度分布特性,进而影响液体燃料的喷雾特性。通过流体喷嘴内部几何结构的创新设计改善流体喷射特性是一种重要的技术途径。It is well known that the internal geometry of a fluid nozzle affects its internal flow field properties. For example, in the field of internal combustion engines, the internal geometry of the liquid fuel nozzle affects its cavitation bubble generation characteristics, pressure and velocity distribution characteristics, and then affects the spray characteristics of the liquid fuel. Improving fluid ejection characteristics through innovative design of fluid nozzle internal geometry is an important technological approach.
本发明提供的带部分扭转式8字形喷孔的喷嘴,8字形的中间狭缝能够增强两个类圆形孔道内的流体干涉作用,增强扰动;沿喷孔轴线扭转后能够进一步提高喷孔内的扰动作用,增加空化气泡的生成,有利于喷雾破碎。但考虑到采用全扭转式会增加喷射阻力,因此提供一种部分扭转式8字形喷孔结构。In the nozzle with a partially twisted 8-shaped nozzle provided by the present invention, the 8-shaped middle slit can enhance the fluid interference effect in the two quasi-circular channels and enhance the disturbance; after twisting along the axis of the nozzle, it can further improve the internal flow of the nozzle. The disturbance effect increases the generation of cavitation bubbles, which is conducive to spray breakage. However, considering that the use of the full torsion type will increase the injection resistance, a partially torsion type 8-shaped nozzle structure is provided.
发明内容SUMMARY OF THE INVENTION
根据上述提出的技术问题,而提供一种能够产生适宜的内部湍流扰动,从而进一步改善液体喷雾特性的带部分扭转式8字形喷孔的喷嘴。According to the above-mentioned technical problem, there is provided a nozzle with a partially twisted 8-shaped orifice which can generate suitable internal turbulent disturbance to further improve the liquid spray characteristics.
本发明采用的技术手段如下:The technical means adopted in the present invention are as follows:
一种带部分扭转式8字形喷孔的喷嘴,包括喷嘴本体和在所述喷嘴本体上设置的一个或多个喷孔,其中至少一个喷孔包括非扭转的喷孔前段和扭转的横截面为8字形的喷孔后段,所述喷孔后段横截面8字形的长轴沿着喷孔轴线旋转,所述8字形的长宽比可沿着喷孔轴线变化。A nozzle with a partially twisted 8-shaped nozzle, comprising a nozzle body and one or more nozzle holes provided on the nozzle body, wherein at least one nozzle hole includes a non-twisted nozzle hole front section and a twisted cross section of In the rear section of the 8-shaped injection hole, the long axis of the 8-shaped cross section of the rear section of the injection hole rotates along the axis of the injection hole, and the aspect ratio of the 8-shaped shape can be changed along the axis of the injection hole.
进一步地,与所述喷孔前段相关联的喷嘴本体面面相交而形成的拐角全部为曲面过渡。Further, all the corners formed by the surface-to-surface intersection of the nozzle body associated with the front section of the nozzle hole are curved surface transitions.
进一步地,所述8字形的扭转方向为顺时针方向或逆时针方向。Further, the twisting direction of the figure 8 is clockwise or counterclockwise.
进一步地,所述喷孔前段从入口到出口面积为保持不变,先减小后增大,逐渐增大,逐渐减小和先增大后减小的任一种。Further, the area of the front section of the injection hole from the inlet to the outlet remains unchanged, first decreases and then increases, gradually increases, gradually decreases, and first increases and then decreases.
进一步地,所述喷孔后段从入口到出口面积为保持不变,先减小后增大,逐渐增大,逐渐减小和先增大后减小的任一种。Further, the area of the rear section of the injection hole from the inlet to the outlet remains unchanged, first decreases and then increases, gradually increases, gradually decreases, and first increases and then decreases.
进一步地,所述喷孔前段喷孔纵截面形状为矩形、渐缩型、渐扩型、渐缩-渐扩型和渐扩-渐缩型的任一种。Further, the longitudinal cross-sectional shape of the nozzle hole in the front section of the nozzle hole is any one of a rectangle, a tapered type, a gradually expanded type, a tapered-to-expanded type, and a gradually expanded-to-contracted type.
进一步地,所述喷孔后段喷孔纵截面形状为矩形、渐缩型、渐扩型、渐缩-渐扩型和渐扩-渐缩型的任一种。Further, the longitudinal cross-sectional shape of the nozzle hole at the rear section of the nozzle hole is any one of a rectangle, a tapered type, a gradually expanded type, a tapered-to-expanded type, and a gradually expanded-to-contracted type.
进一步地,所述喷嘴采用3D打印快速成型技术。Further, the nozzle adopts 3D printing rapid prototyping technology.
本发明适用于各种需采用喷嘴、喷头或喷射器等设备进行液体或气体喷射的领域。本发明与现有技术相比,可强化喷嘴的喷孔内部湍流扰动,在液体喷射条件下还可改善喷嘴内部空化气泡生成和速度分布,从而使喷嘴获得更好的喷射和混合特性,与全扭转式相比能减小部分喷射阻力,且8字形加工难度较低。如应用于直喷式柴油机的燃油喷嘴,可在相同喷射压力下使喷雾粒子平均直径减小12%,发动机热效率提高2.2%,颗粒物排放量降低22%。基于上述理由本发明可在流体喷射技术领域广泛推广。The present invention is applicable to various fields that need to use equipment such as nozzles, spray heads or injectors to spray liquid or gas. Compared with the prior art, the invention can strengthen the turbulent flow disturbance inside the nozzle hole, and can also improve the generation and velocity distribution of cavitation bubbles inside the nozzle under the condition of liquid injection, so that the nozzle can obtain better injection and mixing characteristics, and Compared with the full torsion type, part of the injection resistance can be reduced, and the figure-8 processing is less difficult. For example, it can reduce the average diameter of spray particles by 12% under the same injection pressure, increase the thermal efficiency of the engine by 2.2%, and reduce particulate matter emissions by 22%. For the above reasons, the present invention can be widely applied in the field of fluid ejection technology.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图做以简单地介绍,显而易见地,下面描述中的附图是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动性的前提下,还可以根据这些附图获得其他的附图。In order to illustrate the embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description These are some embodiments of the present invention, and for those of ordinary skill in the art, other drawings can also be obtained from these drawings without any creative effort.
图1为本发明实施例一种具备等面积型扭转段8字形喷孔的立体结构示意图。FIG. 1 is a schematic three-dimensional structural diagram of a figure-eight nozzle with an equal-area twisted segment according to an embodiment of the present invention.
图2为本发明一种流体喷嘴本体和喷孔的示意图。FIG. 2 is a schematic diagram of a fluid nozzle body and nozzle holes of the present invention.
图3为本发明图1所述喷孔的立体图扭转段右视图。FIG. 3 is a right side view of the twisted section of the perspective view of the nozzle hole shown in FIG. 1 of the present invention.
图4为本发明所述的扭转段为等面积型部分扭转式8字形喷孔的二维结构示意图。4 is a schematic diagram of a two-dimensional structure in which the twisted section according to the present invention is an equal-area partially twisted figure-eight nozzle hole.
图5为本发明所述的扭转段为渐缩渐扩型部分扭转式8字形喷孔的二维结构示意图。FIG. 5 is a two-dimensional structural schematic diagram of the torsion section according to the present invention, which is a tapered and expanded partially twisted figure-eight nozzle hole.
图6为本发明所述的扭转段为渐扩型部分扭转式8字形喷孔的二维结构示意图。6 is a schematic diagram of a two-dimensional structure in which the twisted section of the present invention is a gradually expanding partially twisted 8-shaped nozzle hole.
图7为本发明所述的扭转段为渐缩型部分扭转式8字形喷孔的二维结构示意图。FIG. 7 is a two-dimensional structural schematic diagram of the twisted section according to the present invention, which is a tapered partially twisted 8-shaped nozzle hole.
图8为本发明所述的扭转段为渐扩渐缩型部分扭转式8字形喷孔的二维结构示意图。FIG. 8 is a two-dimensional structural schematic diagram of the torsion section according to the present invention, which is a gradually expanding and tapering partially twisted figure-eight nozzle hole.
图中:1、喷嘴本体;2、3、9、15、21、27、8字形喷孔;4、10、16、22、28喷孔前段;5、11、17、23、29、喷孔前段入口;6、12、18、24、30喷孔前段出口、喷孔后段入口;7、13、19、25、31喷孔后段;8、14、20、26、32喷孔后段出口。In the figure: 1. Nozzle body; 2, 3, 9, 15, 21, 27, 8-shaped nozzle holes; 4, 10, 16, 22, 28 nozzle front section; 5, 11, 17, 23, 29, nozzle holes Front section inlet; 6, 12, 18, 24, 30 nozzle outlet front section, nozzle rear section inlet; 7, 13, 19, 25, 31 nozzle rear section; 8, 14, 20, 26, 32 nozzle rear section Export.
具体实施方式Detailed ways
需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。下面将参考附图并结合实施例来详细说明本发明。It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict. The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
为使本发明实施例的目的、技术方案和优点更加清楚,下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。以下对至少一个示例性实施例的描述实际上仅仅是说明性的,决不作为对本发明及其应用或使用的任何限制。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in 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. Obviously, the described embodiments It is only a part of the embodiments of the present invention, but not all of the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
需要注意的是,这里所使用的术语仅是为了描述具体实施方式,而非意图限制根据本发明的示例性实施方式。如在这里所使用的,除非上下文另外明确指出,否则单数形式也意图包括复数形式,此外,还应当理解的是,当在本说明书中使用术语“包含”和/或“包括”时,其指明存在特征、步骤、操作、器件、组件和/或它们的组合。It should be noted that the terminology used herein is for the purpose of describing specific embodiments only, and is not intended to limit the exemplary embodiments according to the present invention. As used herein, unless the context clearly dictates otherwise, the singular is intended to include the plural as well, furthermore, it is to be understood that when the terms "comprising" and/or "including" are used in this specification, it indicates that There are features, steps, operations, devices, components and/or combinations thereof.
除非另外具体说明,否则在这些实施例中阐述的部件和步骤的相对布置、数字表达式和数值不限制本发明的范围。同时,应当清楚,为了便于描述,附图中所示出的各个部分的尺寸并不是按照实际的比例关系绘制的。对于相关领域普通技术人员己知的技术、方法和设备可能不作详细讨论,但在适当情况下,所述技术、方法和设备应当被视为授权说明书的一部分。在这里示出和讨论的所有示例中,任向具体值应被解释为仅仅是示例性的,而不是作为限制。因此,示例性实施例的其它示例可以具有不同的值。应注意到:相似的标号和字母在下面的附图中表示类似项,因此,一旦某一项在一个附图中被定义,则在随后的附图中不需要对其进行进一步讨论。The relative arrangement of the components and steps, the numerical expressions and numerical values set forth in these embodiments do not limit the scope of the invention unless specifically stated otherwise. Meanwhile, it should be understood that, for convenience of description, the dimensions of various parts shown in the accompanying drawings are not drawn in an actual proportional relationship. Techniques, methods, and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods, and devices should be considered part of the authorized specification. In all examples shown and discussed herein, any specific values should be construed as illustrative only and not limiting. Accordingly, other examples of exemplary embodiments may have different values. It should be noted that like numerals and letters refer to like items in the following figures, so once an item is defined in one figure, it does not require further discussion in subsequent figures.
在本发明的描述中,需要理解的是,方位词如“前、后、上、下、左、右”、“横向、竖向、垂直、水平”和“顶、底”等所指示的方位或位置关系通常是基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,在未作相反说明的情况下,这些方位词并不指示和暗示所指的装置或元件必须具有特定的方位或者以特定的方位构造和操作,因此不能理解为对本发明保护范围的限制:方位词“内、外”是指相对于各部件本身的轮廓的内外。In the description of the present invention, it should be understood that the orientations indicated by orientation words such as "front, rear, top, bottom, left, right", "horizontal, vertical, vertical, horizontal" and "top, bottom" etc. Or the positional relationship is usually based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, and these orientation words do not indicate or imply the indicated device or element unless otherwise stated. It must have a specific orientation or be constructed and operated in a specific orientation, so it should not be construed as a limitation on the scope of protection of the present invention: the orientation words "inside and outside" refer to the inside and outside relative to the contour of each component itself.
为了便于描述,在这里可以使用空间相对术语,如“在……之上”、“在……上方”、“在……上表面”、“上面的”等,用来描述如在图中所示的一个器件或特征与其他器件或特征的空间位置关系。应当理解的是,空间相对术语旨在包含除了器件在图中所描述的方位之外的在使用或操作中的不同方位。例如,如果附图中的器件被倒置,则描述为“在其他器件或构造上方”或“在其他器件或构造之上”的器件之后将被定位为“在其他器件或构造下方”或“在其位器件或构造之下”。因而,示例性术语“在……上方”可以包括“在……上方”和“在……下方”两种方位。该器件也可以其他不同方式定位(旋转90度或处于其他方位),并且对这里所使用的空间相对描述作出相应解释。For ease of description, spatially relative terms, such as "on", "over", "on the surface", "above", etc., may be used herein to describe what is shown in the figures. The spatial positional relationship of one device or feature shown to other devices or features. It should be understood that spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "above" or "over" other devices or features would then be oriented "below" or "over" the other devices or features under its device or structure". Thus, the exemplary term "above" can encompass both an orientation of "above" and "below." The device may also be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptions used herein interpreted accordingly.
此外,需要说明的是,使用“第一”、“第二”等词语来限定零部件,仅仅是为了便于对相应零部件进行区别,如没有另行声明,上述词语并没有特殊含义,因此不能理解为对本发明保护范围的限制。In addition, it should be noted that the use of words such as "first" and "second" to define components is only for the convenience of distinguishing corresponding components. Unless otherwise stated, the above words have no special meaning and therefore cannot be understood to limit the scope of protection of the present invention.
如图1所示,本发明提供了一种带部分扭转式8字形喷孔的喷嘴,包括喷嘴本体1和在所述喷嘴本体上设置的一个或多个喷孔2,其中至少一个喷孔包括非扭转的喷孔前段和如图2、3所示的扭转的横截面为8字形的喷孔后段,所述喷孔后段横截面8字形的长轴沿着喷孔轴线旋转,所述8字形的长宽比可沿着喷孔轴线变化。As shown in FIG. 1 , the present invention provides a nozzle with a partially twisted 8-shaped nozzle, comprising a
与带变截面喷孔相关联的喷嘴本体面面相交而形成的拐角全部为曲面过渡。The corners formed by the face-to-face intersection of the nozzle body associated with the nozzle hole with variable cross-section are all curved surface transitions.
所述8字形的扭转方向为顺时针方向或逆时针方向。所述喷孔前段从入口到出口面积为保持不变,先减小后增大,逐渐增大,逐渐减小和先增大后减小的任一种。所述喷孔后段从入口到出口面积为保持不变,先减小后增大,逐渐增大,逐渐减小和先增大后减小的任一种。所述喷孔前段喷孔纵截面形状为矩形、渐缩型、渐扩型、渐缩-渐扩型和渐扩-渐缩型的任一种。所述喷孔后段喷孔纵截面形状为矩形、渐缩型、渐扩型、渐缩-渐扩型和渐扩-渐缩型的任一种。The twisting direction of the figure 8 is clockwise or counterclockwise. The area of the front section of the spray hole from the inlet to the outlet remains unchanged, first decreases and then increases, gradually increases, gradually decreases, and first increases and then decreases. The area of the rear section of the spray hole from the inlet to the outlet remains unchanged, first decreases and then increases, gradually increases, gradually decreases, and first increases and then decreases. The shape of the longitudinal section of the nozzle hole in the front section of the nozzle hole is any one of a rectangle, a tapered type, a gradually expanded type, a tapered-to-expanded type, and a gradually expanded-to-contracted type. The longitudinal section shape of the nozzle hole in the rear section of the nozzle hole is any one of a rectangle, a tapered type, a gradually expanded type, a tapered-to-expanded type, and a gradually expanded-to-contracted type.
所述喷嘴采用3D打印快速成型技术。The nozzle adopts 3D printing rapid prototyping technology.
实施例1Example 1
如图4所示,在本实施例中喷孔3喷孔前段(非扭转段)4入口5和出口6及喷孔后段(扭转段)7入口6、出口8的横截面的面积及长宽比保持一致,其纵截面形状都是直筒型,扭转段7其8字形横截面顺时针扭转了360°。相对于圆形直孔,本实例的喷孔内部产生了更加强烈的湍流扰动,在喷孔出口会产生更多的空化气泡,这两方面的影响都促进了喷嘴的一次雾化和混合气形成,8字形中间狭缝还能进一步加强两个类圆形孔道的流体干涉,且与全扭转式相比能降低部分喷射阻力。As shown in FIG. 4 , in this embodiment, the area and length of the
实施例2Example 2
如图5所示,在本实例中,喷孔9的喷孔前段(非扭转段)10入口11和出口12面积和形状完全一致,纵截面采用直筒型;喷孔后段(扭转段)13入口12和出口14面积和形状完全一致,但在中间段过程中横截面积和纵截面采用渐缩渐扩型,扭转段8字形顺时针旋转了360°。As shown in FIG. 5 , in this example, the area and shape of the
实施例3Example 3
如图6所示。在本实施例中,喷孔15的喷孔前段(非扭转段)16入口17比出口18面大,中间段过程中横截面积和纵截面采用渐缩型;喷孔后段(扭转段)19入口18比出口20小,中间段过程采用渐扩型,扭转段8字形逆时针旋转了360°;喷孔整体呈现渐缩渐扩型。As shown in Figure 6. In this embodiment, the
实施例4Example 4
如图7所示。在本实施例中,喷孔21的喷孔前段(非扭转段)22入口23和出口21面积和形状完全一致,中间段过程中横截面积和纵截面采用渐缩渐扩型;喷孔后段(扭转段)25入口24比出口26大,中间段过程采用渐缩型,扭转段8字形逆时针旋转了360°。As shown in Figure 7. In this embodiment, the area and shape of the
实施例5Example 5
如图8所示。在本实施例中,喷孔27的喷孔前段(非扭转段)28入口29与出口30一致,中间段过程中横截面积和纵截面采用渐扩渐缩型;喷孔后段(扭转段)31入口30与出口32一致,中间段过程采用渐扩渐缩型,扭转段8字形顺时针旋转了360°。As shown in Figure 8. In this embodiment, the
上述实例仅为部分结构示意图,8字形长宽比变化、横截面积变化及纵截面结构型式、扭转的角度可以随意组合。The above examples are only partial schematic diagrams of the structure, and the change of the aspect ratio of the figure-eight shape, the change of the cross-sectional area, the structural type of the longitudinal cross-section, and the angle of torsion can be combined arbitrarily.
相对于圆形直孔,本实例的喷孔具备扭转式8字形喷孔增强内部湍流扰动的特点,且8字形中间狭缝能增强两个类圆形孔道的流体干涉作用,加强扰动。还由于其具备渐缩-渐扩型的结构,因而本实例所述喷孔既具备渐缩型喷孔结构导致的较强的保压作用,使喷孔出口燃油的总能量增加,又具备渐扩型喷孔出口空化气泡数量较大的特点,同时与全扭转式喷孔相比能减小部分喷射阻力。通过数值计算发现,本发明应用于直喷式柴油机,可在相同喷射压力下使喷雾粒子平均直径减小12%,发动机热效率提高2.2%,颗粒物排放降低22%。Compared with the circular straight hole, the nozzle of this example has the characteristics of the twisted figure-eight nozzle to enhance the internal turbulent disturbance, and the middle slit of the figure-eight can enhance the fluid interference effect of the two quasi-circular orifices and enhance the disturbance. Also because it has a tapered-expanded structure, the nozzle hole described in this example not only has a strong pressure-holding effect caused by the tapered nozzle hole structure, which increases the total energy of the fuel at the nozzle outlet, but also has the ability to gradually increase the pressure. The large number of cavitation bubbles at the outlet of the expanded nozzle can reduce part of the injection resistance compared with the fully twisted nozzle. Through numerical calculation, it is found that the present invention can reduce the average diameter of spray particles by 12%, increase the thermal efficiency of the engine by 2.2%, and reduce the emission of particulate matter by 22% under the same injection pressure when applied to a direct injection diesel engine.
最后应说明的是:以上各实施例仅用以说明本发明的技术方案,而非对其限制;尽管参照前述各实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分或者全部技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的范围。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, but not to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: The technical solutions described in the foregoing embodiments can still be modified, or some or all of the technical features thereof can be equivalently replaced; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the technical solutions of the embodiments of the present invention. scope.
Claims (7)
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Application publication date: 20200218 |