CN114483653A - Volute, centrifugal fan and range hood - Google Patents

Volute, centrifugal fan and range hood Download PDF

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Publication number
CN114483653A
CN114483653A CN202111581138.1A CN202111581138A CN114483653A CN 114483653 A CN114483653 A CN 114483653A CN 202111581138 A CN202111581138 A CN 202111581138A CN 114483653 A CN114483653 A CN 114483653A
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China
Prior art keywords
volute
line segment
impeller
molded line
segment
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CN202111581138.1A
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卢宇轩
周骏尧
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Guangdong Vanward New Electric Co Ltd
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Guangdong Vanward New Electric Co Ltd
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Priority to CN202111581138.1A priority Critical patent/CN114483653A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226Fan casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/422Discharge tongues
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The application relates to the technical field of range hoods, and the embodiment of the application provides a volute, a centrifugal fan and a range hood. The molded line of the volute comprises a first molded line segment, a second molded line segment, a third molded line segment and a fourth molded line segment which are connected in sequence, and the two connected molded line segments are in smooth transition. The third molded line section forms a main body of the volute, the second molded line section forms a volute tongue of the volute, and the third molded line section is located on the logarithmic spiral curve. The logarithmic spiral curve where the third molded line segment is located is an arc line segment generated by the same circle center, the curvature of the third molded line segment is continuous, and meanwhile, the radial clearance between the logarithmic spiral curve and the reference circle is gradually increased by designing the reference circle, so that the change of the polar radius of the third molded line segment is continuous, the molded line error of the volute is reduced, vortex can be prevented from being generated in the volute to reduce the noise of the volute, gas in the volute can be concentrated, and the smoke exhaust efficiency of the volute is improved.

Description

蜗壳、离心风机以及吸油烟机Volutes, centrifugal fans and range hoods

技术领域technical field

本申请涉及吸油烟机技术领域,特别是涉及一种蜗壳、离心风机以及吸油烟机。The present application relates to the technical field of range hoods, in particular to a volute, a centrifugal fan and a range hood.

背景技术Background technique

相关技术中,蜗壳型线设计多采用四段不同圆心的圆弧来生成蜗壳型线。在此过程中,由于弧形半径与叶轮转速正相关,会导致风轮速度越大,蜗壳型线的误差也越大。如此,使得蜗壳型线与叶轮不匹配,造成蜗壳排烟效率低,噪音高。同时,在该生成蜗壳型线的方法中,相邻的圆弧的弧形半径的变化较大,会导致蜗壳内产生旋涡,使风机的风量、风压和效率都大幅度下降,蜗壳内会形成较大的压力梯度,从而导致涡流噪音增大。In the related art, the volute profile design mostly uses four arcs with different centers to generate the volute profile. In this process, since the arc radius is positively related to the impeller speed, the greater the speed of the impeller, the greater the error of the volute profile. In this way, the profile line of the volute does not match the impeller, resulting in low smoke exhaust efficiency and high noise of the volute. At the same time, in the method of generating the volute profile, the arc radius of the adjacent arcs changes greatly, which will cause vortexes to be generated in the volute, so that the air volume, wind pressure and efficiency of the fan will be greatly reduced, and the volute will be greatly reduced. Large pressure gradients develop in the shell, resulting in increased vortex noise.

发明内容SUMMARY OF THE INVENTION

基于此,有必要针对上述技术问题,提供一种蜗壳、离心风机以及吸油烟机,以提高蜗壳排烟效率和降低蜗壳的噪音。Based on this, it is necessary to provide a volute, a centrifugal fan and a range hood to improve the smoke exhaust efficiency of the volute and reduce the noise of the volute in view of the above technical problems.

根据本申请的一个方面,本申请实施例提供了一种蜗壳,所述蜗壳的型线包括依次连接的第一型线段、第二型线段、第三型线段以及第四型线段,相连的两个型线段之间平滑过渡;所述第三型线段构成所述蜗壳的主体,所述第二型线段构成所述蜗壳的蜗舌,所述第一型线段和所述第四型线段构成所述蜗壳的出风口,所述第三型线段位于对数螺旋曲线上;According to one aspect of the present application, an embodiment of the present application provides a volute, and the profile of the volute includes a first profile segment, a second profile segment, a third profile segment, and a fourth profile segment connected in sequence. The smooth transition between the two profile segments; the third profile segment constitutes the main body of the volute, the second profile segment constitutes the volute tongue of the volute, the first profile segment and the fourth profile segment The profile segment constitutes the air outlet of the volute, and the third profile segment is located on the logarithmic spiral curve;

所述第三型线段与所述第二型线段相切于第一切点,所述第三型线段与所述第四型线段相切于第二切点,从所述第一切点沿着所述第三型线段至所述第二切点的方向为第一路径方向;定义以所述对数螺旋曲线的极点为圆心、位于所述蜗壳内的叶轮半径r为半径得到的圆为参考圆,所述对数螺旋曲线与所述参考圆相交于第一交点,所述参考圆的轮廓与位于所述第一交点与所述第二切点之间的所述对数螺旋曲线之间构造出径向间隙;The third-type line segment and the second-type line segment are tangent to the first tangent point, the third-type line segment and the fourth-type line segment are tangent to the second tangent point, and from the first tangent point along the The direction from the third type line segment to the second tangent point is the first path direction; define a circle with the pole of the logarithmic spiral curve as the center and the radius r of the impeller located in the volute as the radius is a reference circle, the logarithmic spiral curve intersects with the reference circle at a first intersection point, and the contour of the reference circle is located between the first intersection point and the second tangent point of the logarithmic spiral curve A radial gap is constructed between;

其中,在所述第一路径方向上,所述径向间隙逐渐增大,且所述第三型线段的曲率连续。Wherein, in the direction of the first path, the radial gap gradually increases, and the curvature of the third-shaped line segment is continuous.

上述蜗壳中,由于第三型线段所在的对数螺旋曲线是以同一圆心生成的弧线段,第三型线段的曲率是连续的,同时通过设计参考圆,构造对数螺旋曲线与参考圆之间的径向间隙逐渐增大,如此,使得第三型线段的极半径的变化是连续的,降低了蜗壳型线的误差,不仅可以防止蜗壳内产生涡流以降低蜗壳的噪音,还可以使得蜗壳内的气体更集中,提高蜗壳的排烟效率。In the above volute, since the logarithmic spiral curve where the third-shaped line segment is located is an arc segment generated by the same circle center, the curvature of the third-shaped line segment is continuous. At the same time, by designing the reference circle, the logarithmic spiral curve and the reference circle are constructed. The radial gap between them gradually increases, so that the change of the pole radius of the third profile line segment is continuous, which reduces the error of the volute profile, not only can prevent the eddy current from being generated in the volute to reduce the noise of the volute, It can also make the gas in the volute more concentrated, and improve the smoke exhaust efficiency of the volute.

在其中一个实施例中,所述极点与所述第一切点之间的连线与所述参考圆的轮廓相交于第二交点,所述第二交点与所述第一切点连线的长度为d1;其中,r与d1的比值为5.73-8.8。如此,可以限定第三型线段与参考圆之间的距离,即是限定了该蜗壳的蜗舌与所配套使用的叶轮之间的最小距离,也就是蜗壳与所配套使用的叶轮之间的最小距离,防止蜗舌处因流体分流而产生风噪,避免风噪通过蜗舌传播到外部而影响用户的使用感受。In one of the embodiments, the line connecting the pole and the first tangent point and the outline of the reference circle intersect at a second intersection point, and the line connecting the second intersection point and the first tangent point intersects at a second intersection point. The length is d1; wherein, the ratio of r to d1 is 5.73-8.8. In this way, the distance between the third-shaped line segment and the reference circle can be defined, that is, the minimum distance between the volute tongue of the volute and the matched impeller, that is, between the volute and the matched impeller The minimum distance to prevent wind noise at the volute tongue due to fluid shunting, and prevent wind noise from being transmitted to the outside through the volute tongue and affecting the user's experience of use.

在其中一个实施例中,所述第二型线段为圆弧。如此,可以通过圆弧形状降低蜗舌处的风阻。In one of the embodiments, the second-shaped line segment is an arc. In this way, the wind resistance at the volute tongue can be reduced by the arc shape.

在其中一个实施例中,所述第二型线段的圆弧半径为R;其中,r与R的比值为7.33-10.15。如此,可以限定第二型线段的圆弧半径的大小,即是限定了蜗舌拐角处的大小,可以进一步降低蜗舌处的风噪。In one of the embodiments, the arc radius of the second shaped line segment is R; wherein, the ratio of r to R is 7.33-10.15. In this way, the size of the arc radius of the second-shaped line segment can be limited, that is, the size of the corner of the volute tongue can be limited, and the wind noise at the volute tongue can be further reduced.

在其中一个实施例中,所述对数螺旋曲线的极点与所述第二型线段的弧心的连线为第一连线,所述极点和所述第一交点的连线与所述第一连线的夹角为α1;其中,76°≤α1≤86°。如此,可以限定得到第二型线段的圆弧长度,可以构造得到预设形状的蜗舌,以进一步提高流体流经蜗舌时的动力特性。In one embodiment, a line connecting the pole of the logarithmic spiral curve and the arc center of the second-shaped line segment is a first connecting line, and the connecting line between the pole and the first intersection point and the first connecting line The included angle of a connecting line is α1; among them, 76°≤α1≤86°. In this way, the arc length of the second-shaped line segment can be defined, and the volute tongue with a preset shape can be constructed to further improve the dynamic characteristics of the fluid flowing through the volute tongue.

在其中一个实施例中,所述第四型线段为直线,且所述第四型线段与所述极点和所述第二交点的连线的夹角为α2;其中,80°≤α2≤90°。如此,可以得到合理的蜗壳扩压角度,防止蜗壳内部的气体回流到蜗壳内部,提高了排气效率。In one embodiment, the fourth-shaped line segment is a straight line, and the included angle between the fourth-shaped line segment and the line connecting the pole and the second intersection is α2; wherein, 80°≤α2≤90 °. In this way, a reasonable expansion angle of the volute can be obtained, the gas inside the volute is prevented from flowing back into the volute, and the exhaust efficiency is improved.

在其中一个实施例中,所述第一交点与所述第二切点连线的长度为d2;其中,r与d2的比值为1.38-1.56。如此,可以对第三型线段进行限定,进而对第三型线段的曲率进行限定,进一步降低了蜗壳型线的误差。In one embodiment, the length of the line connecting the first intersection point and the second tangent point is d2; wherein, the ratio of r to d2 is 1.38-1.56. In this way, the third-shaped line segment can be limited, and further the curvature of the third-shaped line segment can be limited, which further reduces the error of the volute molding line.

在其中一个实施例中,所述对数螺旋曲线的方程为:In one embodiment, the equation of the logarithmic spiral curve is:

Figure BDA0003426077250000031
Figure BDA0003426077250000031

其中,r为所述叶轮的半径,e为自然对数的底数,a为所述叶轮的叶片的后流角,b为所述叶轮的出口宽度,B为所述蜗壳的高度,

Figure BDA0003426077250000032
为所述对数螺旋曲线的极半径与所述极点和所述第一交点的连线的夹角,
Figure BDA0003426077250000033
为R的修正值。如此,通过设置修正值,对螺旋曲线进行修正,可以降低蜗壳型线的误差。Wherein, r is the radius of the impeller, e is the base of the natural logarithm, a is the back flow angle of the blade of the impeller, b is the outlet width of the impeller, B is the height of the volute,
Figure BDA0003426077250000032
is the angle between the pole radius of the logarithmic spiral curve and the line connecting the pole and the first intersection,
Figure BDA0003426077250000033
is the corrected value of R. In this way, by setting the correction value to correct the helical curve, the error of the volute profile can be reduced.

在其中一个实施例中,所述叶轮的最大转速为800r/min-1000r/min,l为10mm-15mm;In one embodiment, the maximum rotational speed of the impeller is 800r/min-1000r/min, and l is 10mm-15mm;

所述叶轮的最大转速为600r/min-800r/min,l为5mm-10mm。如此,可以根据不同转速的叶轮,进行不同程度上的修正。The maximum rotational speed of the impeller is 600r/min-800r/min, and l is 5mm-10mm. In this way, different degrees of correction can be made according to the impellers of different rotational speeds.

根据本申请的另一个方面,本申请实施例提供了一种离心风机,包括叶轮和上述所述的蜗壳;According to another aspect of the present application, an embodiment of the present application provides a centrifugal fan, comprising an impeller and the above-mentioned volute;

其中,所述叶轮设于所述蜗壳内,所述叶轮的中心与所述对数螺旋曲线的极点重合。如此,可以使得该离心风机的排烟效率高、噪音低。Wherein, the impeller is arranged in the volute, and the center of the impeller coincides with the pole of the logarithmic spiral curve. In this way, the centrifugal fan can have high smoke exhaust efficiency and low noise.

在其中一个实施例中,所述叶轮的叶片数量为64叶-70叶。如此,可以使得蜗壳型线与叶轮更为匹配,提高蜗壳排烟效率,降低噪音。In one embodiment, the number of blades of the impeller ranges from 64 blades to 70 blades. In this way, the profile of the volute and the impeller can be more matched, the smoke exhaust efficiency of the volute is improved, and the noise is reduced.

根据本申请的又一个方面,本申请实施例提供了一种吸油烟机,包括上述所述的离心风机。如此,可以使得吸油烟机排烟效率高,噪音低。According to another aspect of the present application, an embodiment of the present application provides a range hood, including the centrifugal fan described above. In this way, the smoke exhausting efficiency of the range hood can be high and the noise is low.

本申请实施例的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本申请实施例的实践了解到。Additional aspects and advantages of embodiments of the present application will be set forth, in part, in the following description, and in part will be apparent from the following description, or learned by practice of embodiments of the present application.

附图说明Description of drawings

图1为相关技术一实施例中蜗壳型线的示意图;1 is a schematic diagram of a volute profile in an embodiment of the related art;

图2为相关技术另一实施例中蜗壳型线的示意图;2 is a schematic diagram of a volute profile in another embodiment of the related art;

图3为本申请一实施例中蜗壳的结构示意图;3 is a schematic structural diagram of a volute in an embodiment of the application;

图4为本申请一实施例中蜗壳的剖视结构示意图;4 is a schematic cross-sectional structural diagram of a volute in an embodiment of the application;

图5为本申请一实施例中蜗壳型线的示意图;5 is a schematic diagram of a volute profile in an embodiment of the application;

图6为本申请的图5中第二型线段的局部放大示意图;Fig. 6 is the partial enlarged schematic diagram of the second type line segment in Fig. 5 of the application;

图7为本申请一实施例中蜗壳型线的构造示意图;7 is a schematic structural diagram of a volute profile in an embodiment of the application;

图8为本申请一实施例中提供的蜗壳的声压云图示意图;8 is a schematic diagram of a sound pressure cloud diagram of a volute provided in an embodiment of the application;

图9为本申请又一实施例中提供的蜗壳的声压云图示意图;9 is a schematic diagram of a sound pressure cloud diagram of a volute provided in another embodiment of the application;

图10为本申请另一实施例中提供的蜗壳的声压云图示意图。FIG. 10 is a schematic diagram of a sound pressure cloud diagram of a volute provided in another embodiment of the present application.

元件符号简单说明:Simple description of component symbols:

第一型线段L1、第二型线段L2、第三型线段L3、第四型线段L4、第一连线L5、第二连线L6;a first-type line segment L1, a second-type line segment L2, a third-type line segment L3, a fourth-type line segment L4, a first connecting line L5, and a second connecting line L6;

极点O、参考圆P、径向间隙t;Pole O, reference circle P, radial clearance t;

第一切点T1、第二切点T2、第三切点T3;The first tangent point T1, the second tangent point T2, and the third tangent point T3;

第一交点C1、第二交点C2;The first intersection point C1, the second intersection point C2;

蜗舌100、出风口200、蜗壳上板300、蜗壳底板400、蜗壳围板500、进风口600、导风圈700;The volute tongue 100, the air outlet 200, the volute upper plate 300, the volute bottom plate 400, the volute surrounding plate 500, the air inlet 600, and the air guide ring 700;

叶轮20;Impeller 20;

电机30。Motor 30.

具体实施方式Detailed ways

为使本申请的上述目的、特征和优点能够更加明显易懂,下面结合附图对本申请实施例的具体实施方式做详细的说明。在下面的描述中阐述了很多具体细节以便于充分理解本申请实施例。应当理解,此处描述的具体实施例仅仅用以解释本申请,并不用于限定本申请。本申请实施例能够以很多不同于在此描述的其它方式来实施,本领域技术人员可以在不违背本发明内涵的情况下做类似改进,因此,本申请实施例不受下面公开的具体实施例的限制。In order to make the above objects, features and advantages of the present application more clearly understood, the specific implementations of the embodiments of the present application will be described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to facilitate a thorough understanding of the embodiments of the present application. It should be understood that the specific embodiments described herein are only used to explain the present application, but not to limit the present application. The embodiments of the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without departing from the connotation of the present invention. Therefore, the embodiments of the present application are not subject to the specific embodiments disclosed below. limits.

可以理解,本申请所使用的术语“第一”、“第二”、“第三”、“第四”等可在本文中用于描述各种专业名词,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。但除非特别说明,这些专业名词不受这些术语限制。这些术语仅用于将一个专业名词与另一个专业名词区分。举例来说,在不脱离本申请的范围的情况下,第一型线段、第二型线段、第三型线段和第四型线段为不同的型线段,第一切点、第二切点和第三切点为不同的切点。在本申请实施例的描述中,“多个”、“若干”的含义是至少两个,例如两个,三个等,除非另有明确具体的限定。It can be understood that the terms "first", "second", "third", "fourth", etc. used in this application can be used to describe various technical terms in this document, and cannot be understood as indicating or implying relative importance. nature or implicitly indicate the number of technical features indicated. However, unless otherwise specified, these professional terms are not limited by these terms. These terms are only used to distinguish one professional term from another. For example, without departing from the scope of the present application, the first type line segment, the second type line segment, the third type line segment and the fourth type line segment are different type line segments, the first tangent point, the second tangent point and the The third tangent point is a different tangent point. In the description of the embodiments of the present application, "plurality" and "several" mean at least two, such as two, three, etc., unless otherwise expressly and specifically defined.

在本申请实施例的描述中,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系,除非另有明确的限定。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本申请实施例中的具体含义。In the description of the embodiments of the present application, unless otherwise expressly specified and limited, terms such as "installation", "connection", "connection", and "fixation" should be understood in a broad sense. For example, it may be a fixed connection or a It can be a detachable connection, or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between the two elements, unless otherwise expressly qualified. Those of ordinary skill in the art can understand the specific meanings of the above terms in the embodiments of the present application according to specific situations.

在本申请实施例的描述中,除非另有明确的规定和限定,第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触,或第一和第二特征通过中间媒介间接接触。而且,第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方,或仅仅表示第一特征水平高度高于第二特征水平高度。第一特征在第二特征“之下”、“下方”和“下面”可以是第一特征在第二特征正下方或斜下方,或仅仅表示第一特征水平高度小于第二特征水平高度。In the description of the embodiments of the present application, unless otherwise expressly specified and limited, the first feature "on" or "under" the second feature may be in direct contact with the first and second features, or the first and second features Indirect contact through an intermediary. Also, the first feature is "above", "above" and "above" the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the level of the first feature is higher than the level of the second feature . The first feature being "below", "below" and "below" the second feature may mean that the first feature is directly or diagonally below the second feature, or simply means that the first feature level is less than the second feature level.

需要说明的是,当元件被称为“固定于”或“设置于”另一个元件,它可以直接在另一个元件上或者也可以存在居中的元件。当一个元件被认为是“连接”另一个元件,它可以是直接连接到另一个元件或者可能同时存在居中元件。It should be noted that when an element is referred to as being "fixed to" or "disposed on" another element, it can be directly on the other element or an intervening element may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present.

除非另有定义,本申请所使用的所有的技术和科学术语与属于本申请的技术领域的技术人员通常理解的含义相同。本申请中在本申请的说明书中所使用的术语只是为了描述具体的实施例的目的,不是旨在于限制本申请。Unless otherwise defined, all technical and scientific terms used in this application have the same meaning as commonly understood by one of ordinary skill in the technical field to which this application belongs. The terms used in this application in the specification of this application are for the purpose of describing specific embodiments only, and are not intended to limit the application.

离心蜗壳是吸油烟机的核心部件之一,其可以将蜗壳进风口附近的气体集中,通过驱动电机带动叶轮转动,从而将气体从蜗壳出口排出。在此过程中,离心蜗壳的型线不但决定了蜗壳的形状,还对吸油烟机整机的风量、风压、效率和噪音有影响。The centrifugal volute is one of the core components of the range hood, which can concentrate the gas near the air inlet of the volute, and drive the impeller to rotate through the drive motor, thereby discharging the gas from the outlet of the volute. In this process, the profile of the centrifugal volute not only determines the shape of the volute, but also affects the air volume, air pressure, efficiency and noise of the entire range hood.

图1示出了相关技术一实施例中蜗壳型线的示意图;图2示出了相关技术另一实施例中蜗壳型线的示意图;为了便于说明,仅示出了与相关技术中的实施例相关的部分。Fig. 1 shows a schematic diagram of a volute profile in an embodiment of the related art; Fig. 2 shows a schematic diagram of a volute profile in another embodiment of the related art; Example relevant part.

请参照图1和图2,相关技术中,蜗壳型线由多段弧形所组成,多采用四段不同圆心的圆弧来生成蜗壳型线。由此,该段曲线具有R1、R2、R3和R4四种圆弧半径。本申请发明人注意到,相邻的圆弧的圆弧半径变化较大,会导致蜗壳内产生旋涡,使风机的风量、风压和效率都大幅度下降,蜗壳内会形成较大的压力梯度,从而导致涡流噪音增大。另外,由于弧形半径与叶轮转速正相关,会导致风轮速度越大,蜗壳型线的误差也越大。如此,使得蜗壳型线与叶轮不匹配,造成蜗壳排烟效率低,噪音高。Referring to FIG. 1 and FIG. 2 , in the related art, the volute profile is composed of multiple arcs, and four arcs with different centers are often used to generate the volute profile. Therefore, this segment of the curve has four arc radii of R1, R2, R3 and R4. The inventor of the present application has noticed that the arc radius of the adjacent arcs varies greatly, which will cause vortices to be generated in the volute, and the air volume, air pressure and efficiency of the fan will be greatly reduced, and a large vortex will be formed in the volute. pressure gradient, resulting in increased vortex noise. In addition, since the arc radius is positively related to the impeller speed, the greater the speed of the impeller, the greater the error of the volute profile. In this way, the profile line of the volute does not match the impeller, resulting in low smoke exhaust efficiency and high noise of the volute.

基于以上考虑,发明人经过深入研究,设计了一种蜗壳,通过限定蜗壳型线的形状,可以提高蜗壳排烟效率和降低蜗壳的噪音。下面结合一些实施例的相关描述,对本申请实施例提供的蜗壳进行相关说明。Based on the above considerations, the inventor has designed a volute after in-depth research. By defining the shape of the volute profile, the smoke exhaust efficiency of the volute can be improved and the noise of the volute can be reduced. The volute provided by the embodiments of the present application will be described below with reference to the relevant descriptions of some embodiments.

本申请实施例公开的蜗壳可以用于离心风机中,离心风机可以用于吸油烟机中,也可以用于以其它需要用到此蜗壳形成的风道结构的风力系统中。以下以一些实施例中的蜗壳的具体构造为例进行说明,但并不以此为限。需要说明的是,本申请实施例公开的蜗壳的型线可以是顺时针方向的,也可以是逆时针方向的,可以根据使用情况进行选择,本申请实施例对此不作具体限制。The volute disclosed in the embodiments of the present application can be used in a centrifugal fan, the centrifugal fan can be used in a range hood, and can also be used in other wind power systems that need to use the air duct structure formed by the volute. The following description takes the specific structure of the volute in some embodiments as an example, but it is not limited thereto. It should be noted that, the molding line of the volute disclosed in the embodiment of the present application may be clockwise or counterclockwise, which may be selected according to the usage, which is not specifically limited in the embodiment of the present application.

图3示出了本申请一实施例中蜗壳的结构示意图;图4示出了本申请一实施例中蜗壳的剖视结构示意图;为了便于说明,仅示出了与本申请实施例中相关的部分。Fig. 3 shows a schematic structural diagram of a volute in an embodiment of the present application; Fig. 4 shows a cross-sectional structural schematic diagram of a volute in an embodiment of the present application; relevant part.

为便于理解,如图4所示,图纸的上方向外定义为上方,图纸的下方向内定义为下方,图纸的左方向内定义为左侧,图纸的右方向外定义为右侧,图纸的左方向外定义为前侧,图纸的右方向内定义为后侧。其余图示沿用图4的定义。可以理解,上述定义仅为了说明,并不能理解为对本申请的限定。可以理解,上述定义仅为了说明,并不能理解为对本申请的限定。For ease of understanding, as shown in Figure 4, the top of the drawing is defined as the upper side, the lower side of the drawing is defined as the bottom, the left side of the drawing is defined as the left side, the right side of the drawing is defined as the right side, and the drawing is defined as the right side. The left side is defined as the front side, and the right side of the drawing is defined as the back side. The rest of the illustrations follow the definition in Figure 4. It can be understood that the above definitions are only for illustration, and should not be construed as limitations on the present application. It can be understood that the above definitions are only for illustration, and should not be construed as limitations on the present application.

请参照图3和图4,本申请一实施例提供了一种蜗壳,该蜗壳包括蜗壳上板300、蜗壳底板400以及蜗壳围板500。蜗壳上板300上设有进风口600。蜗壳底板400与蜗壳上板300间隔设置,蜗壳底板400上设有用于安装电机30的安装孔。蜗壳围板500连接在蜗壳上板300和蜗壳底板400之间,蜗壳围板500、蜗壳上板300以及蜗壳底板400之间围成容纳空间以及位于后侧的出风口200,进风口600、安装孔(图示为标出)以及出风口200连通容纳空间。容纳空间用以容纳叶轮20。蜗壳围板500上靠近出风口200的一侧形成有蜗舌100。蜗舌100的作用是将蜗壳出口的气流进行分流,蜗舌100处的流场较复杂,蜗舌100处也是离心蜗壳噪声产生的地方。Referring to FIGS. 3 and 4 , an embodiment of the present application provides a volute, the volute includes a volute upper plate 300 , a volute bottom plate 400 and a volute surrounding plate 500 . An air inlet 600 is provided on the upper plate 300 of the volute. The volute bottom plate 400 is spaced apart from the volute upper plate 300 , and the volute bottom plate 400 is provided with a mounting hole for mounting the motor 30 . The volute casing 500 is connected between the volute upper plate 300 and the volute bottom plate 400, and the volute casing 500, the volute upper plate 300 and the volute bottom plate 400 enclose an accommodation space and an air outlet 200 on the rear side , the air inlet 600, the installation hole (marked in the figure) and the air outlet 200 communicate with the accommodating space. The accommodating space is used to accommodate the impeller 20 . A volute tongue 100 is formed on the side of the volute enclosure plate 500 close to the air outlet 200 . The function of the volute tongue 100 is to divide the airflow at the outlet of the volute. The flow field at the volute tongue 100 is relatively complex, and the volute tongue 100 is also the place where the centrifugal volute noise is generated.

下面以上述一些实施例中的蜗壳的结构为例,对蜗壳的型线进行说明。The shape of the volute is described below by taking the structure of the volute in some of the above embodiments as an example.

图5示出了本申请一实施例中蜗壳型线的示意图;图6示出了本申请的图5中第二型线段L2的局部放大示意图;为了便于说明,仅示出了与本申请实施例中相关的部分。Fig. 5 shows a schematic diagram of a volute profile in an embodiment of the present application; Fig. 6 shows a partially enlarged schematic diagram of the second profile line segment L2 in Fig. 5 of the present application; Relevant parts in the examples.

请参照图5和图6,本申请实施例提供了一种蜗壳,蜗壳的型线包括依次连接的第一型线段L1、第二型线段L2、第三型线段L3以及第四型线段L4。相连的两个型线段之间平滑过渡。第三型线段L3构成蜗壳的主体,第二型线段L2构成蜗壳的蜗舌100,第一型线段L1和第四型线段L4构成蜗壳的出风口200,第三型线段L3位于对数螺旋曲线上。Referring to FIGS. 5 and 6, an embodiment of the present application provides a volute, and the profile of the volute includes a first profile segment L1, a second profile segment L2, a third profile segment L3, and a fourth profile segment connected in sequence L4. Smooth transition between two connected line segments. The third-shaped line segment L3 constitutes the main body of the volute, the second-shaped line segment L2 constitutes the volute tongue 100 of the volute, the first-shaped line segment L1 and the fourth-shaped line segment L4 constitute the air outlet 200 of the volute, and the third-shaped line segment L3 is located on the opposite side of the volute. number on the spiral curve.

第三型线段L3与第二型线段L2相切于第一切点T1,第三型线段L3与第四型线段L4相切于第二切点T2,从第一切点T1沿着第三型线段L3至第二切点T2的方向为第一路径方向;定义以对数螺旋曲线的极点O为圆心、位于蜗壳内的叶轮20半径r为半径得到的圆为参考圆P,对数螺旋曲线与参考圆P相交于第一交点C1,参考圆P的轮廓与位于第一交点C1与第二切点T2之间的对数螺旋曲线之间构造出径向间隙t。其中,在第一路径方向上,径向间隙t逐渐增大,且第三型线段L3的曲率连续。也就是说,对数螺旋曲线的极半径与叶轮20半径之间的差值,在第一路径方向上逐渐增大。以图5为例,第一路径方向为沿着第三型线段L3的顺时针方向。The third-type line segment L3 and the second-type line segment L2 are tangent to the first tangent point T1, and the third-type line segment L3 and the fourth-type line segment L4 are tangent to the second tangent point T2. From the first tangent point T1 along the third The direction from the profile line segment L3 to the second tangent point T2 is the first path direction; the circle obtained by taking the pole O of the logarithmic spiral curve as the center and the radius r of the impeller 20 located in the volute as the radius is the reference circle P, and the logarithm The helical curve intersects the reference circle P at the first intersection point C1, and a radial gap t is formed between the contour of the reference circle P and the logarithmic helical curve located between the first intersection point C1 and the second tangent point T2. Wherein, in the first path direction, the radial gap t gradually increases, and the curvature of the third-shaped line segment L3 is continuous. That is, the difference between the pole radius of the logarithmic spiral curve and the radius of the impeller 20 gradually increases in the first path direction. Taking FIG. 5 as an example, the first path direction is a clockwise direction along the third-shaped line segment L3.

需要说明的是,“蜗壳的主体”指的是在蜗壳内放置有叶轮20后,叶轮20与蜗壳围板500相对应的部分,蜗壳围板500弯曲形成与叶轮20相适配的形状的部分,相对应地,蜗壳上板300和蜗壳底板400在此部分的形状也与蜗壳围板500相适配。“径向间隙t”是从第一交点C1处从零开始变化的,且终止于第二切点T2对应的位置处。It should be noted that "the main body of the volute" refers to the part of the impeller 20 corresponding to the volute enclosure plate 500 after the impeller 20 is placed in the volute case, and the volute enclosure plate 500 is bent to fit the impeller 20 Correspondingly, the shape of the volute upper plate 300 and the volute bottom plate 400 in this part is also adapted to the volute surrounding plate 500 . The "radial clearance t" starts from zero at the first intersection point C1 and ends at the position corresponding to the second tangent point T2.

由于第三型线段L3所在的对数螺旋曲线是以同一圆心生成的弧线段,第三型线段的曲率是连续的,同时通过设计参考圆P,构造对数螺旋曲线与参考圆P之间的径向间隙t逐渐增大,如此,使得第三型线段L3的极半径的变化是连续的。也就是说,通过径向间隙t与第三型线段L3的曲率共同约束第三型线段L3的构造,使得第三型线段L3更加平稳光滑,第三型线段L3的极半径的变化是连续的,降低了蜗壳型线的误差,不仅可以防止蜗壳内产生涡流以降低蜗壳的噪音,还可以使得蜗壳内的气体更集中,提高蜗壳的排烟效率。Since the logarithmic spiral curve where the third-type line segment L3 is located is an arc segment generated by the same circle center, the curvature of the third-type line segment is continuous. At the same time, by designing the reference circle P, the logarithmic spiral curve and the reference circle P are constructed The radial gap t gradually increases, so that the change of the pole radius of the third type line segment L3 is continuous. That is to say, the radial gap t and the curvature of the third-type line segment L3 constrain the structure of the third-type line segment L3, so that the third-type line segment L3 is more stable and smooth, and the change of the polar radius of the third-type line segment L3 is continuous. , reducing the error of the volute shape line, not only can prevent the vortex from being generated in the volute to reduce the noise of the volute, but also make the gas in the volute more concentrated and improve the smoke exhaust efficiency of the volute.

在一些实施例中,请继续参考图5和图6,极点O与第一切点T1之间的连线与参考圆P的轮廓相交于第二交点C2,第二交点C2与第一切点T1连线的长度为d1。其中,r与d1的比值为5.73-8.8。如此,可以限定第三型线段L3与参考圆P之间的距离,即是限定了该蜗壳的蜗舌100与所配套使用的叶轮20之间的最小距离,也就是蜗壳与所配套使用的叶轮20之间的最小距离。蜗舌100可以防止部分气体在蜗壳内循环流动。当叶轮20的叶片通道出口处的气流掠过蜗舌100附近时,蜗舌100会对气流进行分流,大部分气流顺着通道流向了出风口200。少部分气流则通过蜗舌100、叶轮20之间的间隙流回蜗壳内,在蜗壳内随叶轮20旋转达一周后重返蜗舌100处参与新的分流。蜗舌100、叶轮20之间的间隙过小时,虽然回流蜗壳内的气流会变少,但是流向出风口200处的气流会变多,风噪会变大。蜗舌100、叶轮20之间的间隙过大时,流向出风口200处的气流会变少,回流蜗壳内的气流会变多,会导致蜗壳的排气效率低。如此,通过限定该蜗壳的蜗舌100与所配套使用的叶轮20之间的最小距离,不仅可以防止蜗舌100处因流体分流而产生风噪,避免风噪通过蜗舌100传播到外部而影响用户的使用感受,还可以得到良好的排气效率。In some embodiments, please continue to refer to FIG. 5 and FIG. 6 , the line between the pole O and the first tangent point T1 intersects the outline of the reference circle P at the second intersection point C2 , and the second intersection point C2 and the first tangent point The length of the T1 connection is d1. Among them, the ratio of r to d1 is 5.73-8.8. In this way, the distance between the third-shaped line segment L3 and the reference circle P can be defined, that is, the minimum distance between the volute tongue 100 of the volute and the impeller 20 used in the volute, that is, the volute and the supporting impeller 20 can be defined. The minimum distance between the impellers 20. The volute tongue 100 can prevent part of the gas from circulating in the volute. When the air flow at the outlet of the blade passage of the impeller 20 passes near the volute tongue 100 , the volute tongue 100 divides the air flow, and most of the air flow flows to the air outlet 200 along the passage. A small part of the airflow flows back into the volute through the gap between the volute tongue 100 and the impeller 20, and returns to the volute tongue 100 after rotating with the impeller 20 for one week in the volute to participate in a new branch flow. If the gap between the volute tongue 100 and the impeller 20 is too small, although the air flow in the backflow volute will be less, the air flow towards the air outlet 200 will increase, and the wind noise will increase. When the gap between the volute tongue 100 and the impeller 20 is too large, the air flow to the air outlet 200 will decrease, and the air flow back into the volute will increase, resulting in low exhaust efficiency of the volute. In this way, by defining the minimum distance between the volute tongue 100 of the volute and the impeller 20 used therewith, not only can the volute tongue 100 be prevented from generating wind noise due to fluid shunting, but also the wind noise can be prevented from being transmitted to the outside through the volute tongue 100 . Affect the user's experience, but also can get good exhaust efficiency.

在一些实施例中,请继续参考图5和图6,第二型线段L2为圆弧。如此,可以通过圆弧形状降低蜗舌100处的风阻。具体至一些实施例中,第二型线段L2的圆弧半径为R;其中,r与R的比值为7.33-10.15。如此,可以限定第二型线段L2的圆弧半径R的大小,即是限定了蜗舌100拐角处的大小,不仅可以进行光滑地分流,还可以进一步降低蜗舌100处的风噪。In some embodiments, please continue to refer to FIG. 5 and FIG. 6 , the second type line segment L2 is an arc. In this way, the wind resistance at the volute tongue 100 can be reduced by the arc shape. Specifically, in some embodiments, the arc radius of the second-shaped line segment L2 is R; wherein, the ratio of r to R is 7.33-10.15. In this way, the size of the arc radius R of the second type line segment L2 can be limited, that is, the size of the corner of the volute tongue 100 can be limited, which can not only smoothly divide the flow, but also further reduce the wind noise at the volute tongue 100 .

在一些实施例中,请继续参考图5和图6,对数螺旋曲线的极点O与第二型线段L2的弧心O2的连线为第一连线L5,极点O和第一交点C1的连线为第二连线L6,第一连线L5与第二连线L6的夹角为α1。其中,76°≤α1≤86°。也就是说,构造第三型线段L3的构造起点位于参考圆P上,第三型线段L3的构造起点和第三型线段L3的起点之间的线段,在得到第三型线段L3的起点后,可以去掉,这样进一步限定了第三型线段L3的形状以与叶轮20进行匹配,提高蜗壳排烟效率。如此,通过限定第一连线L5与第二连线L6的夹角,不仅可以限定得到第二型线段L2的圆弧长度,构造得到预设形状的蜗舌100,降低风噪,还可以得到第三型线段L3的起点,以进一步提高流体流经蜗舌100时的动力特性。In some embodiments, please continue to refer to FIG. 5 and FIG. 6 , the connection line between the pole O of the logarithmic spiral curve and the arc center O2 of the second type line segment L2 is the first connection line L5, and the connection between the pole O and the first intersection C1 The connecting line is the second connecting line L6, and the included angle between the first connecting line L5 and the second connecting line L6 is α1. Among them, 76°≤α1≤86°. That is to say, the construction starting point of the third type line segment L3 is located on the reference circle P, and the line segment between the construction starting point of the third type line segment L3 and the starting point of the third type line segment L3, after obtaining the starting point of the third type line segment L3 , can be removed, which further defines the shape of the third-shaped line segment L3 to match the impeller 20 and improve the smoke exhaust efficiency of the volute. In this way, by defining the included angle between the first connecting line L5 and the second connecting line L6, not only the arc length of the second-shaped line segment L2 can be limited, the volute tongue 100 of the preset shape can be constructed, and the wind noise can be reduced. The starting point of the third-shaped line segment L3 to further improve the dynamic characteristics of the fluid flowing through the volute tongue 100 .

在一些实施例中,请继续参考图5,第四型线段L4为直线,且第四型线段L4与第二连线L6的夹角为α2。其中,80°≤α2≤90°。以图5为例,示意出夹角α2为90°的情形。如此,可以得到合理的蜗壳扩压角度,防止蜗壳内部的气体回流到蜗壳内部,提高了排气效率。In some embodiments, please continue to refer to FIG. 5 , the fourth-type line segment L4 is a straight line, and the included angle between the fourth-type line segment L4 and the second connecting line L6 is α2 . Among them, 80°≤α2≤90°. Taking FIG. 5 as an example, the case where the included angle α2 is 90° is illustrated. In this way, a reasonable expansion angle of the volute can be obtained, the gas inside the volute is prevented from flowing back into the volute, and the exhaust efficiency is improved.

在一些实施例中,请继续参考图5,第一交点C1与第二切点T2连线的长度为d2。其中,r与d2的比值为1.38-1.56。也就是说,第一交点C1为第三型线段L3的构造起点,第二切点T2为第三型线段L3的构造终点,通过限定第三型线段L3的构造起点与第三型线段L3的构造终点之间的距离,可以对第三型线段L3进行限定,进而对第三型线段L3的曲率进行限定,进一步降低了蜗壳型线的误差。另外,对流向出风口200的气流流量进行了限定,既不影响排烟效率,又可以降低噪音。In some embodiments, please continue to refer to FIG. 5 , the length of the line connecting the first intersection point C1 and the second tangent point T2 is d2 . Among them, the ratio of r to d2 is 1.38-1.56. That is to say, the first intersection point C1 is the construction start point of the third type line segment L3, and the second tangent point T2 is the construction end point of the third type line segment L3. By defining the construction start point of the third type line segment L3 and the third type line segment L3 The distance between the construction end points can limit the third-shaped line segment L3, and further limit the curvature of the third-shaped line segment L3, which further reduces the error of the volute molding line. In addition, the flow rate of the air flow to the air outlet 200 is limited, which does not affect the exhaust efficiency and reduces noise.

在一些实施例中,对数螺旋曲线的方程为:In some embodiments, the equation of the logarithmic spiral curve is:

Figure BDA0003426077250000091
Figure BDA0003426077250000091

其中,r为叶轮20的半径,e为自然对数的底数,a为叶轮20的叶片的后流角,b为叶轮20的出口宽度(即图4示意出的叶轮20在上下方向上的高度),B为蜗壳的高度(即图4示意出的蜗壳在上下方向上的高度,也就是蜗壳上板300与蜗壳底板400之间的距离),

Figure BDA0003426077250000101
为对数螺旋曲线的极半径与第二连线L6的夹角,
Figure BDA0003426077250000102
为R的修正值。如此,通过设置修正值,对螺旋曲线进行修正,可以降低蜗壳型线的误差。Wherein, r is the radius of the impeller 20, e is the base of the natural logarithm, a is the back flow angle of the blades of the impeller 20, b is the outlet width of the impeller 20 (that is, the height of the impeller 20 shown in FIG. 4 in the up-down direction) ), B is the height of the volute (that is, the height of the volute shown in FIG. 4 in the up-down direction, that is, the distance between the upper plate 300 of the volute and the bottom plate 400 of the volute),
Figure BDA0003426077250000101
is the angle between the pole radius of the logarithmic spiral curve and the second connecting line L6,
Figure BDA0003426077250000102
is the corrected value of R. In this way, by setting the correction value to correct the helical curve, the error of the volute profile can be reduced.

在一些实施例中,叶轮20的最大转速为800r/min-1000r/min,l为10mm-15mm。而在另一些实施例中,叶轮20的最大转速为600r/min-800r/min,l为5mm-10mm。如此,可以根据不同转速的叶轮20,进行不同程度上的修正。In some embodiments, the maximum rotational speed of the impeller 20 is 800r/min-1000r/min, and l is 10mm-15mm. In other embodiments, the maximum rotational speed of the impeller 20 is 600r/min-800r/min, and l is 5mm-10mm. In this way, different degrees of correction can be performed according to the impellers 20 with different rotational speeds.

基于同一发明构思,本申请实施例提供了一种离心风机,包括叶轮20和上述实施例中的蜗壳。其中,叶轮20设于蜗壳内,叶轮20的中心与对数螺旋曲线的极点O重合。如此,可以使得该离心风机的排烟效率高、噪音低。Based on the same inventive concept, the embodiment of the present application provides a centrifugal fan, which includes an impeller 20 and the volute in the above embodiment. Wherein, the impeller 20 is arranged in the volute, and the center of the impeller 20 coincides with the pole O of the logarithmic spiral curve. In this way, the centrifugal fan can have high smoke exhaust efficiency and low noise.

在一些实施例中,叶轮20的叶片数量为64叶-70叶。如此,可以使得蜗壳型线与叶轮20更为匹配,提高蜗壳排烟效率,降低噪音。In some embodiments, the number of blades of the impeller 20 is 64-70 blades. In this way, the profile of the volute and the impeller 20 can be more matched, the smoke exhaust efficiency of the volute can be improved, and the noise can be reduced.

基于同一发明构思,本申请实施例提供了一种吸油烟机,包括上述实施例中的离心风机。如此,可以使得吸油烟机排烟效率高,噪音低。Based on the same inventive concept, an embodiment of the present application provides a range hood, including the centrifugal fan in the above embodiment. In this way, the smoke exhausting efficiency of the range hood can be high and the noise is low.

图7示出了本申请一实施例中蜗壳型线的构造示意图;为了便于说明,仅示出了与本申请实施例中相关的部分。FIG. 7 shows a schematic diagram of the structure of the volute profile in an embodiment of the present application; for the convenience of description, only the parts related to the embodiment of the present application are shown.

下面对本申请实施例提供的蜗壳的蜗壳型线的构造方法进行举例说明,请参考图7,该步骤如下:The following will illustrate the construction method of the volute profile of the volute provided by the embodiment of the present application. Please refer to FIG. 7 , and the steps are as follows:

S100、构建对数螺旋曲线:以任意一点作为对数螺旋曲线的极点,确定叶轮20的半径r,并以叶轮20的半径r为初始半径,以在该初始半径上端点A作为对数螺旋曲线的起点,根据对数螺旋曲线的方程

Figure BDA0003426077250000103
形成螺旋曲线S;S100. Construct a logarithmic spiral curve: take any point as the pole of the logarithmic spiral curve, determine the radius r of the impeller 20, and take the radius r of the impeller 20 as the initial radius, and take the endpoint A on the initial radius as the logarithmic spiral curve The starting point of , according to the equation of the logarithmic spiral curve
Figure BDA0003426077250000103
form a spiral curve S;

S200、构建第二型线段L2:在夹角

Figure BDA0003426077250000104
角度76°-86°的位置确定第二型线段L2,且第二型线段L2与参考圆P之间最小距离为15mm-23mm,第二型线段L2的圆弧半径为13mm-18mm;S200, constructing the second type line segment L2: at the included angle
Figure BDA0003426077250000104
The position of the angle 76°-86° determines the second type line segment L2, and the minimum distance between the second type line segment L2 and the reference circle P is 15mm-23mm, and the arc radius of the second type line segment L2 is 13mm-18mm;

S300、构建第三型线段L3:以第二型线段L2的终点作为第三型线段L3的起点,以螺旋曲线S上的距离端点A距离为85mm-95mm的点B作为第三型线段L3的终点,且第三型线段L3与第二型线段L2相切;S300, constructing a third-shaped line segment L3: take the end point of the second-shaped line segment L2 as the starting point of the third-shaped line segment L3, and use the point B on the spiral curve S with a distance of 85 mm-95 mm from the end point A as the third-shaped line segment L3 The end point, and the third-type line segment L3 is tangent to the second-type line segment L2;

S400、构建第四型线段L4:第四型线段L4与线段OA的夹角为80°-90°,且第四型线段L4与第三型线段L3相切;S400, constructing a fourth-type line segment L4: the included angle between the fourth-type line segment L4 and the line segment OA is 80°-90°, and the fourth-type line segment L4 is tangent to the third-type line segment L3;

S500、构建第一型线段L1:第一型线段L1与第二型线段L2相切于第二型线段L2的起点。S500 , constructing a first-type line segment L1 : the first-type line segment L1 and the second-type line segment L2 are tangent to the starting point of the second-type line segment L2 .

图8示出了本申请一实施例中提供的蜗壳的声压云图示意图;图9示出了本申请又一实施例中提供的蜗壳的声压云图示意图;图10示出了本申请另一实施例中提供的蜗壳的声压云图示意图;为了便于说明,仅示出了与本申请实施例中相关的部分。Fig. 8 shows a schematic diagram of a sound pressure nephogram of a volute provided in an embodiment of the present application; Fig. 9 shows a schematic diagram of a sound pressure nephogram of a volute provided in another embodiment of the present application; Fig. 10 shows the present application Another embodiment provides a schematic diagram of a sound pressure nephogram of a volute; for the convenience of description, only the parts related to the embodiments of the present application are shown.

设定上述实施例中d2=90mm,α2=90°,蜗舌100的圆弧半径R为15mm,l=10mm,叶轮20的叶片数量为64叶,叶轮20的半径r为132mm,下面采用Ansys的fluent仿真软件对本申请实施例提供的蜗壳进行气动仿真,分别以蜗壳与叶轮20外缘之间最小距离(也即是第二交点C2与第一切点T1连线的长度)为15mm、19mm、23mm为例进行模拟。需要说明的是,图8至图10中,U1代表不同区域中与声压强度相对应的颜色,U2代表具体的声压强度,单位为dB。不同的声压强度具有不同的颜色,随着声压强度的变化,颜色也会跟随变化。该颜色的变化是指随着声压强度越来越大,颜色由冷色调向暖色调渐变过渡。如图8至图10所示,颜色的变化表现为从蜗舌100处沿顺时针方向,由冷色调向暖色调渐变过渡,而在图8至图10中,大部分均为冷色调。图8中所示意处的蜗壳中,蜗壳与叶轮20外缘之间最小距离为15mm,在夹角

Figure BDA0003426077250000111
为80°的蜗舌100处的声压强度分别为59db,图9中所示意处的蜗壳中,蜗壳与叶轮20外缘之间最小距离为19mm,在夹角
Figure BDA0003426077250000112
为80°的蜗舌100处的声压强度分别为53db,图10中所示意处的蜗壳中,蜗壳与叶轮20外缘之间最小距离为23mm,在夹角
Figure BDA0003426077250000113
为80°的蜗舌100处的声压强度分别为49db。由此可见,蜗壳的蜗舌100处气动噪声有明显改善。In the above embodiment, d2=90mm, α2=90°, the arc radius R of the volute tongue 100 is 15mm, l=10mm, the number of blades of the impeller 20 is 64, the radius r of the impeller 20 is 132mm, and Ansys is used below. The fluent simulation software of the present application performs aerodynamic simulation on the volute provided by the embodiment of the application, and the minimum distance between the volute and the outer edge of the impeller 20 (that is, the length of the connecting line between the second intersection C2 and the first tangent point T1) is 15mm. , 19mm, 23mm as examples to simulate. It should be noted that, in FIGS. 8 to 10 , U1 represents the color corresponding to the sound pressure intensity in different regions, and U2 represents the specific sound pressure intensity, and the unit is dB. Different sound pressure intensities have different colors, and as the sound pressure intensity changes, the color will also change. The color change refers to the gradual transition of the color from a cool tone to a warm tone as the sound pressure intensity increases. As shown in FIGS. 8 to 10 , the color changes appear as a gradual transition from cool to warm colors in a clockwise direction from the volute tongue 100 , and in FIGS. 8 to 10 , most of the colors are cool colors. In the volute shown in Fig. 8, the minimum distance between the volute and the outer edge of the impeller 20 is 15mm, at the included angle
Figure BDA0003426077250000111
The sound pressure intensity at the volute tongue 100 with an angle of 80° is 59db, respectively. In the volute shown in Fig. 9, the minimum distance between the volute and the outer edge of the impeller 20 is 19mm.
Figure BDA0003426077250000112
The sound pressure intensity at the volute tongue 100 with an angle of 80° is 53db respectively. In the volute case shown in Figure 10, the minimum distance between the volute case and the outer edge of the impeller 20 is 23mm.
Figure BDA0003426077250000113
The sound pressure intensity at the volute tongue 100 at 80° is 49db, respectively. It can be seen that the aerodynamic noise at the volute tongue 100 of the volute is significantly improved.

综上所述,本申请实施例提供的蜗壳的蜗壳型线中,由于第三型线段L3所在的对数螺旋曲线是以同一圆心生成的弧线段,第三型线段的曲率是连续的,同时通过设计参考圆P,构造对数螺旋曲线与参考圆P之间的径向间隙t逐渐增大,如此,使得第三型线段L3的极半径的变化是连续的,降低了蜗壳型线的误差,不仅可以防止蜗壳内产生涡流以降低蜗壳的噪音,还可以使得蜗壳内的气体更集中,提高蜗壳的排烟效率。通过对蜗舌100的形状以及蜗舌100与叶轮20外援之间的距离的限定,防止蜗舌100处因流体分流而产生的风噪通过蜗舌100传播到外部,影响用户使用感受。通过限定第四型线段L4的角度,防止导致蜗壳内部更多的气体回流到蜗壳内部,提高了排气效率。To sum up, in the volute profile of the volute provided by the embodiment of the present application, since the logarithmic spiral curve where the third profile line segment L3 is located is an arc segment generated by the same circle center, the curvature of the third profile segment is continuous. At the same time, by designing the reference circle P, the radial gap t between the logarithmic spiral curve and the reference circle P is gradually increased, so that the change of the polar radius of the third type line segment L3 is continuous, reducing the volute case. The error of the profile line can not only prevent eddy currents in the volute to reduce the noise of the volute, but also make the gas in the volute more concentrated and improve the smoke exhaust efficiency of the volute. By limiting the shape of the volute tongue 100 and the distance between the volute tongue 100 and the impeller 20, the wind noise generated by the fluid shunt at the volute tongue 100 is prevented from being transmitted to the outside through the volute tongue 100, which affects the user's experience. By defining the angle of the fourth-shaped line segment L4, more gas inside the volute is prevented from flowing back into the volute, thereby improving the exhaust efficiency.

以上实施例的各技术特征可以进行任意的组合,为使描述简洁,未对上述实施例中的各个技术特征所有可能的组合都进行描述,然而,只要这些技术特征的组合不存在矛盾,都应当认为是本说明书记载的范围。The technical features of the above embodiments can be combined arbitrarily. For the sake of brevity, all possible combinations of the technical features in the above embodiments are not described. However, as long as there is no contradiction in the combination of these technical features, all It is considered to be the range described in this specification.

以上所述实施例仅表达了本申请的几种实施方式,其描述较为具体和详细,但并不能因此而理解为对发明专利范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本申请构思的前提下,还可以做出若干变形和改进,这些都属于本申请的保护范围。因此,本申请专利的保护范围应以所附权利要求为准。The above-mentioned embodiments only represent several embodiments of the present application, and the descriptions thereof are specific and detailed, but should not be construed as a limitation on the scope of the invention patent. It should be pointed out that for those skilled in the art, without departing from the concept of the present application, several modifications and improvements can be made, which all belong to the protection scope of the present application. Therefore, the scope of protection of the patent of the present application shall be subject to the appended claims.

Claims (11)

1. A volute is characterized in that the molded line of the volute comprises a first molded line segment (L1), a second molded line segment (L2), a third molded line segment (L3) and a fourth molded line segment (L4) which are connected in sequence, and the two connected molded line segments are in smooth transition; the third type line segment (L3) forms the main body of the volute, the second type line segment (L2) forms the volute tongue (100) of the volute, the first type line segment (L1) and the fourth type line segment (L4) form the air outlet (200) of the volute, and the third type line segment (L3) is located on a logarithmic spiral curve;
the third type line segment (L3) and the second type line segment (L2) are tangent to a first tangent point (T1), the third type line segment (L3) and the fourth type line segment (L4) are tangent to a second tangent point (T2), and a direction from the first tangent point (T1) to the second tangent point (T2) along the third type line segment (L3) is a first path direction; defining a circle with the pole (O) of the logarithmic spiral as the center and the radius r of an impeller (20) in the volute as the radius as a reference circle (P), wherein the logarithmic spiral intersects the reference circle (P) at a first intersection point (C1), and a radial gap (T) is constructed between the outline of the reference circle (P) and the logarithmic spiral between the first intersection point (C1) and the second tangent point (T2);
wherein, in the first path direction, the radial gap (t) gradually increases and the curvature of the third type line segment (L3) is continuous.
2. A spiral casing according to claim 1, characterized in that a line connecting the pole (O) and the first tangent point (T1) intersects the profile of the reference circle (P) at a second intersection point (C2), the length of the line connecting the second intersection point (C2) and the first tangent point (T1) being d 1;
wherein the ratio of r to d1 is 5.73-8.8.
3. The spiral casing as claimed in claim 1, wherein the second profile segment (L2) is a circular arc, the circular arc radius of the second profile segment (L2) being R;
wherein the ratio of R to R is 7.33-10.15.
4. A spiral casing according to any of claims 1-3, characterized in that the line connecting the pole (O) of the logarithmic spiral with the arc center (O2) of the second type segment (L2) is a first line (L5), the line connecting the pole (O) and the first intersection point (C1) makes an angle α 1 with the first line (L5);
wherein alpha 1 is more than or equal to 76 degrees and less than or equal to 86 degrees.
5. The spiral casing according to any of the claims 1-3, characterized in that the fourth type line segment (L4) is a straight line and the fourth type line segment (L4) has an angle α 2 with the line connecting the pole (O) and the second intersection point (C2);
wherein alpha 2 is more than or equal to 80 degrees and less than or equal to 90 degrees.
6. The spiral casing of any of claims 1-3 wherein the first intersection point (C1) is connected to the second tangent point (T2) with a length d 2;
wherein the ratio of r to d2 is 1.38-1.56.
7. The spiral casing of any of claims 1 to 3 wherein the equation for the logarithmic spiral is:
Figure FDA0003426077240000021
wherein r is the radius of the impeller (20), e is the base of the natural logarithm, a is the back flow angle of the blades of the impeller (20), B is the outlet width of the impeller (20), and B is the height of the volute,
Figure FDA0003426077240000022
is the angle between the polar radius of the logarithmic spiral and the line connecting the pole (O) and the first intersection point (C1),
Figure FDA0003426077240000023
is a correction value for R.
8. The spiral casing according to claim 7, wherein the impeller (20) has a maximum rotational speed of 800r/min-1000r/min, l being 10mm-15 mm;
the maximum rotating speed of the impeller (20) is 600r/min-800r/min, and l is 5mm-10 mm.
9. A centrifugal fan comprising an impeller (20) and a volute according to any of claims 1-8;
wherein the impeller (20) is arranged in the volute, and the center of the impeller (20) is superposed with the pole (O) of the logarithmic spiral curve.
10. The centrifugal fan according to claim 9, wherein the impeller (20) has a number of blades of 64-70 blades.
11. A range hood comprising a centrifugal fan according to claim 9 or 10.
CN202111581138.1A 2021-12-22 2021-12-22 Volute, centrifugal fan and range hood Pending CN114483653A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024055614A1 (en) * 2022-09-15 2024-03-21 佛山市顺德区美的电热电器制造有限公司 Range hood assembly and integrated cooker

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011149328A (en) * 2010-01-21 2011-08-04 Mitsubishi Heavy Ind Ltd Multiblade centrifugal fan and air conditioner using the same
CN102182707A (en) * 2011-05-09 2011-09-14 美的集团有限公司 Centrifugal fan for range hood and volute profile generation method thereof
CN108105160A (en) * 2017-12-29 2018-06-01 广东海信家电有限公司 A kind of spiral case of centrifugal blower, centrifugal blower and range hood
CN110905854A (en) * 2019-12-11 2020-03-24 青岛海尔智能技术研发有限公司 Volute for centrifugal fan, centrifugal fan and range hood
CN217207020U (en) * 2021-12-22 2022-08-16 广东万和新电气股份有限公司 Volute, centrifugal fan and range hood

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011149328A (en) * 2010-01-21 2011-08-04 Mitsubishi Heavy Ind Ltd Multiblade centrifugal fan and air conditioner using the same
CN102182707A (en) * 2011-05-09 2011-09-14 美的集团有限公司 Centrifugal fan for range hood and volute profile generation method thereof
CN108105160A (en) * 2017-12-29 2018-06-01 广东海信家电有限公司 A kind of spiral case of centrifugal blower, centrifugal blower and range hood
CN110905854A (en) * 2019-12-11 2020-03-24 青岛海尔智能技术研发有限公司 Volute for centrifugal fan, centrifugal fan and range hood
CN217207020U (en) * 2021-12-22 2022-08-16 广东万和新电气股份有限公司 Volute, centrifugal fan and range hood

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024055614A1 (en) * 2022-09-15 2024-03-21 佛山市顺德区美的电热电器制造有限公司 Range hood assembly and integrated cooker

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