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CN220319900U - A sheet metal centrifugal wind wheel - Google Patents

A sheet metal centrifugal wind wheel Download PDF

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Publication number
CN220319900U
CN220319900U CN202322028316.9U CN202322028316U CN220319900U CN 220319900 U CN220319900 U CN 220319900U CN 202322028316 U CN202322028316 U CN 202322028316U CN 220319900 U CN220319900 U CN 220319900U
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blade
wheel
wind wheel
sheet metal
curve
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陆訄
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Zhongshan Yibisi Technology Co ltd
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Zhongshan Yibisi Technology Co ltd
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Priority to US18/767,954 priority patent/US20250043798A1/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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • 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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers

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

Abstract

The utility model discloses a sheet metal centrifugal wind wheel, which comprises a wheel disc (200), a wheel cover (300) and a plurality of blades (100), wherein the blades (100) are arranged between the wheel disc (200) and the wheel cover (300), and the blades (100) comprise an inlet edge (1), an outlet edge (2), a blade root (3) and a blade top (4), and are characterized in that: the angle position bending part (101) is formed on the angle position of the top of the outlet edge (2), the angle position bending part (101) bends towards the center of the wind wheel rotating shaft L, the blade structure model is stabilized, the rebound effect is restrained, the deviation between the actual blade molded line and the designed blade molded line is reduced, the air flow angle of the blade after rebound is ensured to conform to the original design, the number of times of correcting the die is reduced, the manufacturing cost and the die cost are saved, uncontrollable factors are reduced, and the final blade performance and the finished product delivery period are ensured.

Description

一种钣金离心风轮A sheet metal centrifugal wind wheel

技术领域:Technical areas:

本实用新型涉及一种钣金离心风轮。The utility model relates to a sheet metal centrifugal wind wheel.

背景技术:Background technique:

如图1,现有钣金类后向离心风轮,由轮盘1a、轮盖2a、若干叶片3a组成钣金冲压工艺的叶片,在完成冲压后,因为材料的弹性属性,会存在回弹现象这会使得实际的叶片型线偏移原来设计的叶片型线,详细描述见如下:As shown in Figure 1, the existing sheet metal backward centrifugal wind wheel consists of a disk 1a, a wheel cover 2a, and a number of blades 3a. The blades are formed by the sheet metal stamping process. After the stamping is completed, there will be rebound due to the elastic properties of the material. This phenomenon will cause the actual blade profile to deviate from the originally designed blade profile. The detailed description is as follows:

离心风轮的叶片是一个关键零部件,直接影响风轮的效率,而叶片型线是表征风轮叶片性能的重要几何概念。对于离心式风轮,用靠近风轮底部的任一垂直于旋转轴的平面,截取风轮,可得到叶片截面,见图2所示,则在叶片截面内,可画出无数个叶型轮廓线的内切圆,所有内切圆的圆心连线,就是叶片型线(或者称叶片中线),见图3所示,叶片型线是叶片的基本几何单位,叶片可以看成是无数个截面上的不同叶片型线从叶根到叶顶堆积而成。The blade of a centrifugal wind rotor is a key component, which directly affects the efficiency of the wind rotor, and the blade profile is an important geometric concept that characterizes the performance of the wind rotor blade. For centrifugal wind rotors, cut the rotor using any plane perpendicular to the rotation axis near the bottom of the rotor, and the blade cross section can be obtained, as shown in Figure 2. Countless blade profiles can be drawn within the blade cross section. The inscribed circle of the line and the line connecting the centers of all inscribed circles is the blade profile line (or blade center line), as shown in Figure 3. The blade profile line is the basic geometric unit of the blade, and the blade can be regarded as countless cross-sections. The different blade lines on the blade are accumulated from the blade root to the blade tip.

如图4所示,叶片几何参数的定义:空气来流方向的端点为叶片型线起点,空气离去方向的端点为叶片型线终点。跟据理论物理中绝对速度、相对速度、牵连速度的概念,可知空气将沿着叶片型线在风轮中做相对运动。以大地为绝对坐标系参考,将空气的绝对速度矢量,按平行四边形定理分解,可以很容易画出叶片型线起点、终点以及过程中的各个速度矢量关系。叶片型线起点、终点的空气速度矢量直接决定叶片的做功能力。对于叶片型线起点:C1是叶片进口气流的绝对速度,W1是叶片进口气流的相对速度,U1是叶片型线起点的牵连速度,即该点的圆周速度。对于叶片型线终点:C2是叶片出口气流的绝对速度,W2是叶片出口气流的相对速度,U2是叶片型线终点的牵连速度,即该点的圆周速度。则:W1与U1的反向夹角即为叶片进口角;W2与U2的反向夹角即为叶片出口角。叶片回弹现象:叶片是钣金冲压工艺而成,钣金冲压是一种金属加工方法,它是建立在金属塑性变形的基础上,利用模具和冲压设备对板料施加压力,使板料产生塑性变形或分离,从而获得具有一定形状、尺寸和性能的零件(冲压件)。由于板料的弹性模量(固有物理属性),塑性变形后的冲压件存在内部应力。冲压件在静置一段时间后,内部应力将得到释放,塑性变形量小的地方,会有向板料原状态“回溯”的趋势,这一现象就是回弹现象。对于钣金冲压工艺的叶片,其本身的塑性形变量小,回弹现象非常明显。回弹现象使叶片形状偏离设计形状,本质上是叶片型线偏离了原设计。As shown in Figure 4, the definition of blade geometric parameters: the end point of the air inflow direction is the starting point of the blade profile line, and the end point of the air leaving direction is the end point of the blade profile line. According to the concepts of absolute speed, relative speed and implicated speed in theoretical physics, it can be seen that the air will make relative motion in the wind wheel along the blade profile. Using the earth as the reference of the absolute coordinate system and decomposing the absolute velocity vector of the air according to the parallelogram theorem, we can easily draw the starting point and end point of the blade profile line and the relationship between each velocity vector in the process. The air velocity vector at the starting point and end point of the blade profile directly determines the blade's performance. For the starting point of the blade profile line: C1 is the absolute speed of the blade inlet airflow, W1 is the relative speed of the blade inlet airflow, and U1 is the implicated speed of the starting point of the blade profile line, that is, the circumferential speed at that point. For the end point of the blade profile line: C2 is the absolute speed of the blade outlet airflow, W2 is the relative speed of the blade outlet airflow, and U2 is the implicated speed at the end point of the blade profile line, that is, the circumferential speed at that point. Then: the reverse angle between W1 and U1 is the blade inlet angle; the reverse angle between W2 and U2 is the blade outlet angle. Blade rebound phenomenon: Blades are made by sheet metal stamping process. Sheet metal stamping is a metal processing method. It is based on the plastic deformation of metal. It uses molds and stamping equipment to exert pressure on the sheet metal to cause the sheet metal to produce Plastic deformation or separation to obtain parts (stamping parts) with certain shapes, sizes and properties. Due to the elastic modulus (inherent physical property) of the sheet material, there is internal stress in the stamped parts after plastic deformation. After the stamped parts have been left standing for a period of time, the internal stress will be released, and where the amount of plastic deformation is small, there will be a tendency to "go back" to the original state of the sheet. This phenomenon is called springback. For blades made by sheet metal stamping process, their plastic deformation is small and the rebound phenomenon is very obvious. The springback phenomenon causes the blade shape to deviate from the designed shape. Essentially, the blade profile deviates from the original design.

如图5所示,虚线叶片型线是设计的形状,实线叶片型线表示的是回弹后的形状。结合上文对叶片几何参数的定义可知,回弹后的叶片型线起点、终点的绝对位置发生改变。宏观表现为叶片进口角变小,叶片出口角变大。As shown in Figure 5, the dotted blade profile line is the designed shape, and the solid blade profile line represents the shape after rebound. Combined with the above definition of blade geometric parameters, it can be seen that the absolute positions of the starting point and end point of the blade profile change after rebound. The macroscopic manifestation is that the blade inlet angle becomes smaller and the blade outlet angle becomes larger.

叶片出口角偏大将会增大风轮的做功能力,超出原有设计范围。虽然做功能力变大对于风轮的属性是正向变化,但这也意味着风轮所配电机的输入、输出功率也将增加。对于既定的设计目标,额外增加的输入、输出功率可能会超过电机允许的限制范围,造成电机温升过高、电机输出效率下降、电机零配件加速失效等一系列恶化问题,最终表现为整机效率、整机运行可靠性变差、整机寿命下降。A larger blade exit angle will increase the power of the wind rotor beyond the original design range. Although the increase in working capacity is a positive change for the properties of the wind wheel, it also means that the input and output power of the motor equipped with the wind wheel will also increase. For the established design goals, the additional input and output power may exceed the allowable limit range of the motor, causing a series of deteriorating problems such as excessive temperature rise of the motor, reduction of motor output efficiency, accelerated failure of motor parts, etc., which will ultimately manifest as the failure of the entire machine. The efficiency and overall machine operation reliability deteriorate, and the overall machine life decreases.

为了尽可能使生产出来的产品实际叶片型线与原本设计相符,需要结合材料的弹性属性与冲压形变量,多次修正冲压模具。整个修正过程十分依赖相应的工艺经验,且修正结果仍会存在一定偏差。因为材料的弹性属性、冲压形变量、回弹量之间关系复杂,无法通过计算、仿真模拟等手段进行预测。因此,在实际生产过程中,现有技术手段难以保证叶片性能与设计性能完全一致。另外,修正过程耗时长且不完全可控,也使得成品交期难以保证。In order to make the actual blade profile of the produced product consistent with the original design as much as possible, it is necessary to combine the elastic properties of the material and the amount of stamping deformation to modify the stamping die multiple times. The entire correction process relies heavily on corresponding process experience, and there will still be certain deviations in the correction results. Because the relationship between the material's elastic properties, stamping deformation amount, and springback amount is complex, it cannot be predicted through calculations, simulations, etc. Therefore, in the actual production process, it is difficult to ensure that the blade performance is completely consistent with the design performance by existing technical means. In addition, the correction process is time-consuming and not completely controllable, making it difficult to guarantee the delivery of finished products.

发明内容:Contents of the invention:

本实用新型的一个目的是提供一种钣金离心风轮,解决现有技术中叶片在完成冲压后,因为材料的弹性属性,会存在回弹现象,使得实际的叶片型线偏移原来设计的叶片型线,导致叶片出口角变大影响整个风机效率和运行可靠性,因此需要多次修正冲压模具,修正模具过程耗时长且不完全可控,也使得成品交付期难以保证的技术问题。One purpose of this utility model is to provide a sheet metal centrifugal wind wheel that solves the problem in the prior art that after the blade is stamped, there will be a rebound phenomenon due to the elastic properties of the material, causing the actual blade profile to deviate from the original design. The blade profile causes the blade exit angle to become larger, affecting the efficiency and operational reliability of the entire fan. Therefore, the stamping mold needs to be corrected multiple times. The mold correction process is time-consuming and not completely controllable. It also makes it difficult to guarantee the delivery date of the finished product.

本实用新型的目的是通过下述技术方案予以实现的。The purpose of the present utility model is achieved through the following technical solutions.

一种钣金离心风轮,包括轮盘、轮盖、若干叶片组成,若干叶片安装在轮盘与轮盖之间,叶片包括进口边、出口边、叶根和叶顶,其特征在于:在出口边的顶部的角位上形成角位弯折部,角位弯折部向风轮旋转轴L中心折弯。A sheet metal centrifugal wind wheel consists of a wheel disc, a wheel cover, and several blades. The several blades are installed between the wheel disc and the wheel cover. The blades include an inlet side, an outlet side, a blade root, and a blade top. It is characterized by: A corner bending portion is formed on the top corner of the outlet side, and the corner bending portion is bent toward the center of the rotor rotation axis L.

上述的角位弯折部是由曲线AG、曲线AH和折痕线GH围成,上述曲线AG是出口边上的一段,曲线AG长度小于或者等于1/2的出口边的长度。The above-mentioned angular bending part is surrounded by a curve AG, a curve AH and a crease line GH. The above-mentioned curve AG is a section on the exit side, and the length of the curve AG is less than or equal to 1/2 of the length of the exit side.

上述用垂直于风轮旋转轴L且与曲线AG相交的若干平面截取风轮得到若干条叶片型线,折痕线GH和出口边与若干条叶片型线相交,每一条叶片型线与折痕线GH和出口边相交形成曲线VO,曲线VO的长度从点G到顶点A逐渐增大。The above-mentioned method uses several planes perpendicular to the rotor rotation axis L and intersecting the curve AG to intercept the wind rotor to obtain several blade profile lines. The crease line GH and the exit edge intersect with several blade profile lines. Each blade profile line and crease The intersection of the line GH and the exit edge forms a curve VO, and the length of the curve VO gradually increases from point G to vertex A.

一种钣金离心风轮,包括轮盘、轮盖、若干叶片组成,若干叶片安装在轮盘与轮盖之间,叶片包括进口边、出口边、叶根和叶顶,其特征在于:与出口边等距偏移一段距离形成折痕线NR,折痕线NR与出口边围成等距弯折部,等距弯折部向风轮旋转轴L中心折弯。A sheet metal centrifugal wind wheel consists of a wheel disc, a wheel cover, and several blades. The several blades are installed between the wheel disc and the wheel cover. The blades include an inlet side, an outlet side, a blade root, and a blade top. It is characterized by: The outlet edge is equidistantly offset to form a crease line NR. The crease line NR and the outlet edge form an equidistant bending part, and the equidistant bending part is bent toward the center of the rotor rotation axis L.

上述的等距偏移是指出口边上的每一个点沿着对应的叶片型线偏移相当距离E。The above-mentioned equidistant offset means that each point on the outlet edge is offset by a considerable distance E along the corresponding blade profile line.

本实用新型与现有技术相比,具有如下效果:Compared with the existing technology, this utility model has the following effects:

一、通过本实用新型钣金离心风轮,可以稳固了叶片结构造型,抑制因材料应力释放而产生的回弹效果,使生产出来的产品中的实际叶片型线与设计的叶片型线偏差量减小。1. Through the sheet metal centrifugal wind wheel of this utility model, the blade structural shape can be stabilized, the rebound effect caused by the release of material stress can be suppressed, and the actual blade profile in the produced product can deviate from the designed blade profile. decrease.

二、通过本实用新型钣金离心风轮,改变叶片型线起点参数,减少了叶片出口角,可以保证让回弹后的叶片出口气流角符合原始设计,降低风轮超出原有设计范围的幅值,避免风轮所配电机的输入、输出功率增加,超过电机允许的限制范围。进而避免因此造成的电机温升过高、电机输出效率下降、电机零配件加速失效等一系列恶化问题。2. Through the sheet metal centrifugal wind wheel of this utility model, the starting point parameters of the blade profile are changed, and the blade outlet angle is reduced. This ensures that the blade outlet airflow angle after rebound conforms to the original design, and reduces the amplitude of the wind wheel beyond the original design range. value to prevent the input and output power of the motor equipped with the wind wheel from increasing beyond the allowable limit range of the motor. This will avoid a series of deteriorating problems such as excessive motor temperature rise, reduced motor output efficiency, and accelerated failure of motor parts.

三、通过本实用新型钣金离心风轮,减少修正模具的次数,节约制造成本和模具成本,大大增加开模工作效率,减少不可控因素,保证最终叶片性能与成品交付期。3. Through the sheet metal centrifugal wind wheel of this utility model, the number of mold modifications is reduced, manufacturing costs and mold costs are saved, mold opening efficiency is greatly increased, uncontrollable factors are reduced, and final blade performance and finished product delivery time are guaranteed.

四、本实用新型的其它优点在实施例部分展开详细描述。4. Other advantages of the present utility model are described in detail in the embodiment section.

附图说明:Picture description:

图1是现有技术中的风轮的结构示意图;Figure 1 is a schematic structural diagram of a wind wheel in the prior art;

图2是现有技术中垂直于旋转轴的平面截取风轮的截面图;Figure 2 is a cross-sectional view of the wind wheel taken on a plane perpendicular to the axis of rotation in the prior art;

图3是图2的A部分局部放大图;Figure 3 is a partial enlarged view of part A of Figure 2;

图4是现有技术中叶片型线的几何参数定义示意图;Figure 4 is a schematic diagram of the geometric parameter definition of blade profile in the prior art;

图5是现有技术中叶片型线在回弹后与原设计的对比图;Figure 5 is a comparison diagram of the blade profile in the prior art after rebound and the original design;

图6是本实用新型实施例一的钣金离心风轮的一个角度的立体图;Figure 6 is a perspective view of the sheet metal centrifugal wind wheel according to Embodiment 1 of the present invention;

图7是本实用新型实施例一的钣金离心风轮的另一个角度的立体图;Figure 7 is a perspective view of the sheet metal centrifugal wind wheel from another angle according to Embodiment 1 of the present utility model;

图8是本实用新型实施例一的钣金离心风轮的分解图;Figure 8 is an exploded view of the sheet metal centrifugal wind wheel according to Embodiment 1 of the present utility model;

图9是本实用新型实施例一的钣金离心风轮的叶片的立体图;Figure 9 is a perspective view of the blades of the sheet metal centrifugal wind wheel according to Embodiment 1 of the present utility model;

图10是本实用新型实施例一将叶片四等分后的示意图;Figure 10 is a schematic diagram of the blades divided into four equal parts according to Embodiment 1 of the present invention;

图11是图10在出口边标记的示意图;Figure 11 is a schematic diagram of Figure 10 marked on the exit side;

图12是本实用新型实施例一的叶片上画出M曲面的示意图;Figure 12 is a schematic diagram of an M-curved surface drawn on the blade of Embodiment 1 of the present utility model;

图13是本实用新型实施例一的叶片在G点上进行扫描与法平面相交的示意图;Figure 13 is a schematic diagram of the blade scanning at point G and intersecting the normal plane according to Embodiment 1 of the present invention;

图14是本实用新型实施例一的叶片在G点上进行扫描得到M曲面与法平面相交的一段线示意图;Figure 14 is a schematic diagram of a line intersection between the M curved surface and the normal plane obtained by scanning the blade at G point according to Embodiment 1 of the present invention;

图15是本实用新型实施例一中M曲面绕轴线转动后的示意图;Figure 15 is a schematic diagram of the M-curved surface rotated around the axis in Embodiment 1 of the present utility model;

图16是本实用新型实施例一中叶片与延伸后的M曲面相交后的示意图;Figure 16 is a schematic diagram of the intersection of the blade and the extended M-curved surface in Embodiment 1 of the present invention;

图17是本实用新型实施例一中叶片型线与角位弯折部相交的示意图。Figure 17 is a schematic diagram of the intersection of the blade profile line and the angular bending portion in Embodiment 1 of the present invention.

图18是本实用新型实施例二钣金离心风轮的立体图;Figure 18 is a perspective view of a sheet metal centrifugal wind wheel according to the second embodiment of the present utility model;

图19是本实用新型实施例二钣金离心风轮的叶片示意图。Figure 19 is a schematic diagram of the blades of the sheet metal centrifugal wind wheel in Embodiment 2 of the present utility model.

具体实施方式:Detailed ways:

下面通过具体实施例并结合附图对本实用新型作进一步详细的描述。The utility model will be described in further detail below through specific embodiments and in conjunction with the accompanying drawings.

实施例一:Example one:

如图6、图7、图8、图9所示,本实施例提供的是一种钣金离心风轮,包括轮盘200、轮盖300、若干叶片100组成,若干叶片100安装在轮盘200与轮盖300之间,叶片100包括进口边1、出口边2、叶根3和叶顶4,其特征在于:在出口边2上从顶点A至点G的位置形成曲线AG,在叶顶4上从顶点A至点H是曲线AH,在叶片100上点H与点G的连线形成折痕线102,曲线AG、曲线AH和折痕线GH在叶片100上围成角位弯折部101,角位弯折部101向风轮旋转轴L中心折弯。As shown in Figures 6, 7, 8, and 9, this embodiment provides a sheet metal centrifugal wind wheel, which includes a wheel disk 200, a wheel cover 300, and a plurality of blades 100. The plurality of blades 100 are installed on the wheel disk. 200 and the wheel cover 300, the blade 100 includes an inlet edge 1, an outlet edge 2, a blade root 3 and a blade tip 4. It is characterized in that: a curve AG is formed on the outlet edge 2 from the vertex A to the point G. There is a curve AH from vertex A to point H on the top 4. The line connecting point H and point G on the blade 100 forms a crease line 102. The curve AG, the curve AH and the crease line GH form an angular bend on the blade 100. The bending portion 101 and the angular bending portion 101 are bent toward the center of the rotor rotation axis L.

上述曲线AG的长度小于或者等于1/2的出口边2的长度。The length of the above-mentioned curve AG is less than or equal to 1/2 of the length of the exit side 2 .

下面详细叙述角位弯折部101向向风轮旋转轴L中心折弯的过程:1:如图10所示,叶片100由进口边、出口边、叶根和叶顶四条边围成,从叶顶至叶根,可以定义5条将叶片 等分的叶片型线,分别为:a叶片型线(位于叶顶),b叶片型线(位于叶片1/4处),c叶片型线(位于叶片2/4处),d叶片型线(位于叶片的3/4处),e叶片型线(位于叶根)。见图11所示,下面定义:The process of bending the angular bending portion 101 toward the center of the rotor rotation axis L is described in detail below: 1: As shown in Figure 10, the blade 100 is surrounded by four sides: the inlet side, the outlet side, the blade root and the blade top. From the blade tip to the blade root, 5 blade profile lines can be defined that divide the blade into four equal parts , namely: a blade profile line (located at the blade tip), b blade profile line (located at 1/4 of the blade), c blade profile line (located at 2/4 of the blade), d blade profile line (located at 3/4 of the blade), e blade profile line (located at the blade root). See Figure 11, defined below:

a叶片型线的终点在出口边上为点AaThe end point of the blade profile is point A on the exit edge;

b叶片型线的终点在出口边上为点Bb The end point of the blade profile is point B on the exit edge;

c叶片型线的终点在出口边上为点Cc The end point of the blade profile is point C on the exit edge.

2:以在曲线BC上的某点G为起点,以顶点A为终点,作扫描路径GA,画一个曲面M(见下面第3点描述),如图12所示,所谓扫描路径就是以G为起点,以顶点A为终点用垂直于风轮旋转轴L的若干个平面,不断截取风轮,可得到对应的不同叶片截面和叶片型线;2: Taking a certain point G on the curve BC as the starting point and vertex A as the end point, draw a scanning path GA and draw a surface M (see point 3 below), as shown in Figure 12. The so-called scanning path starts with G. As the starting point, with the vertex A as the end point, use several planes perpendicular to the rotor rotation axis L to continuously intercept the wind rotor, and the corresponding different blade sections and blade profiles can be obtained;

3:在扫描路径GA的法平面(法平面垂直于风轮旋转轴L),以叶片型线终点为坐标原点,叶片型线终点的切线方向为X轴正向,见如图13所示,图13是在扫描路径的起点G的法平面上,图13中G点为坐标原点,上述所述曲面M的特征为:其在扫描路径GA的法平面上的截面图形为一线段,长度任意;线段一端点在坐标原点,线段与X轴正向的夹角为f,对应图13在扫描路径的起点G的法平面上得到线段为GY,线段GY与X轴正向的夹角为f,在实际实施中,f的值依据风轮大小的变化而变化,通常取值范围3-10度。3: On the normal plane of the scanning path GA (the normal plane is perpendicular to the rotor rotation axis L), the end point of the blade profile line is the coordinate origin, and the tangent direction of the end point of the blade profile line is the positive direction of the X-axis, as shown in Figure 13. Figure 13 is on the normal plane of the starting point G of the scanning path. In Figure 13, point G is the coordinate origin. The characteristics of the above-mentioned curved surface M are: its cross-sectional figure on the normal plane of the scanning path GA is a line segment with any length. ; One endpoint of the line segment is at the origin of the coordinates, and the angle between the line segment and the positive direction of the , in actual implementation, the value of f changes according to the change of the size of the wind wheel, and usually ranges from 3 to 10 degrees.

4:以曲面M的G点所在起始边为轴(即以线段GY为转轴),向风轮转轴L中心方向旋转i度角,如图15所示,则将曲面M延伸至与叶片100相交,可得折痕线GH,点H在a叶片型线上,如图16所示,在实际实施中,i的值依据风轮大小的变化而变化,通常取值范围3-6度。4: Taking the starting edge of point G of the curved surface M as the axis (that is, taking the line segment GY as the axis of rotation), rotate an angle i degrees toward the center direction of the rotor axis L, as shown in Figure 15, then extend the curved surface M to be in contact with the blade 100 By intersecting, the crease line GH can be obtained, and the point H is on the blade profile line a, as shown in Figure 16. In actual implementation, the value of i changes according to the change of the size of the wind wheel, and usually ranges from 3 to 6 degrees.

5:如图16所示,将叶片出口边靠近叶顶处的AGH区域(即角位弯折部101),折向曲面M,并完全与曲面M重合,则此时得到的叶片造型就是本专利方案。5: As shown in Figure 16, fold the AGH area (i.e. the angular bending part 101) of the blade outlet edge close to the blade top to the curved surface M, and completely coincide with the curved surface M, then the blade shape obtained at this time is the original Patented solution.

本实用新型的实质是折弯区域的叶片出口角减小f度;而曲线GA上,不同点对应的叶片型线的折弯长度不同。这个原因是曲线GA处的叶片形变量大,产生的“叶片作功能力增加”的效果也大。在实践中发现,越靠近A点形变量越大,所以越靠近A点,叶片型线的折弯长度越长。具体表现在如图17所示,用垂直于风轮旋转轴L且与曲线AG相交的若干平面截取风轮得到若干条叶片型线,折痕线GH和出口边2与若干条叶片型线相交,每一条叶片型线与折痕线GH和出口边2相交形成曲线VO,曲线VO的长度从点G到顶点A逐渐增大。The essence of this utility model is that the blade exit angle in the bending area is reduced by f degrees; and on the curve GA, the bending lengths of the blade profiles corresponding to different points are different. The reason for this is that the deformation of the blade at the curve GA is large, and the effect of "increasing the working capacity of the blade" is also large. In practice, it is found that the closer to point A, the greater the deformation, so the closer to point A, the longer the bending length of the blade profile. Specifically, as shown in Figure 17, several planes perpendicular to the rotor rotation axis L and intersecting the curve AG are used to intercept the wind rotor to obtain several blade profile lines. The crease line GH and the exit edge 2 intersect with several blade profile lines. , each blade profile line intersects with the crease line GH and the exit edge 2 to form a curve VO. The length of the curve VO gradually increases from point G to vertex A.

一、通过本实用新型钣金离心风轮,可以稳固了叶片结构造型,抑制因材料应力释放而产生的回弹效果,使生产出来的产品中的实际叶片型线与设计的叶片型线偏差量减小。1. Through the sheet metal centrifugal wind wheel of this utility model, the blade structural shape can be stabilized, the rebound effect caused by the release of material stress can be suppressed, and the actual blade profile in the produced product can deviate from the designed blade profile. decrease.

二、通过本实用新型钣金离心风轮,改变叶片型线起点参数,减少了叶片出口角,可以保证让回弹后的叶片出口气流角符合原始设计,降低风轮超出原有设计范围的幅值,避免风轮所配电机的输入、输出功率增加,超过电机允许的限制范围。进而避免因此造成的电机温升过高、电机输出效率下降、电机零配件加速失效等一系列恶化问题。2. Through the sheet metal centrifugal wind wheel of this utility model, the starting point parameters of the blade profile are changed, and the blade outlet angle is reduced. This ensures that the blade outlet airflow angle after rebound conforms to the original design, and reduces the amplitude of the wind wheel beyond the original design range. value to prevent the input and output power of the motor equipped with the wind wheel from increasing beyond the allowable limit range of the motor. This will avoid a series of deteriorating problems such as excessive motor temperature rise, reduced motor output efficiency, and accelerated failure of motor parts.

三、通过本实用新型钣金离心风轮,减少修正模具的次数,节约制造成本和模具成本,大大增加开模工作效率,减少不可控因素,保证最终叶片性能与成品交付期。3. Through the sheet metal centrifugal wind wheel of this utility model, the number of mold modifications is reduced, manufacturing costs and mold costs are saved, mold opening efficiency is greatly increased, uncontrollable factors are reduced, and final blade performance and finished product delivery time are guaranteed.

实施例二:Example 2:

如图18、图19所示,一种钣金离心风轮,包括轮盘200、轮盖300、若干叶片100组成,若干叶片100安装在轮盘200与轮盖300之间,叶片100包括进口边1、出口边2、叶根3和叶顶4,其特征在于:与出口边2等距偏移一段距离形成折痕线NR,折痕线NR与出口边2围成等距弯折部103,等距弯折部103向风轮旋转轴L中心折弯。As shown in Figures 18 and 19, a sheet metal centrifugal wind wheel includes a wheel disk 200, a wheel cover 300, and a plurality of blades 100. The plurality of blades 100 are installed between the wheel disk 200 and the wheel cover 300. The blades 100 include an inlet. The edge 1, the exit edge 2, the blade root 3 and the blade top 4 are characterized in that: they are equidistantly offset from the exit edge 2 to form a crease line NR, and the crease line NR and the exit edge 2 form an equidistant bending part 103. The equidistant bending portion 103 is bent toward the center of the rotor rotation axis L.

上述等距偏移是指出口边上的每一个点沿着对应的叶片型线5偏移相当距离。The above-mentioned equidistant offset means that each point on the outlet edge is offset by a considerable distance along the corresponding blade profile line 5 .

该实施例也能稳固了叶片结构造型,抑制因材料应力释放而产生的回弹效果,使生产出来的产品中的实际叶片型线与设计的叶片型线偏差量减小。This embodiment can also stabilize the blade structural shape, suppress the rebound effect caused by the release of material stress, and reduce the deviation between the actual blade profile and the designed blade profile in the produced product.

以上实施例为本实用新型的较佳实施方式,但本实用新型的实施方式不限于此,其他任何未背离本实用新型的精神实质与原理下所作的改变、修饰、替代、组合、简化,均为等效的置换方式,都包含在本实用新型的保护范围之内。The above embodiments are preferred embodiments of the present utility model, but the embodiments of the present utility model are not limited thereto. Any other changes, modifications, substitutions, combinations, and simplifications that do not deviate from the spirit and principles of the present utility model shall be considered. Equivalent replacement methods are included in the protection scope of the present utility model.

Claims (5)

1.一种钣金离心风轮,包括轮盘(200)、轮盖(300)、若干叶片(100)组成,若干叶片(100)安装在轮盘(200)与轮盖(300)之间,叶片(100)包括进口边(1)、出口边(2)、叶根(3)和叶顶(4),其特征在于:在出口边(2)的顶部的角位上形成角位弯折部(101),角位弯折部(101)向风轮旋转轴L中心折弯。1. A sheet metal centrifugal wind wheel, consisting of a wheel disk (200), a wheel cover (300), and several blades (100). The several blades (100) are installed between the wheel disk (200) and the wheel cover (300) , the blade (100) includes an inlet edge (1), an outlet edge (2), a blade root (3) and a blade tip (4), and is characterized in that: an angular bend is formed at the angle of the top of the outlet edge (2). The folding portion (101) and the angular bending portion (101) are bent toward the center of the rotor rotation axis L. 2.根据权利要求1所述的一种钣金离心风轮,其特征在于:角位弯折部(101)是由曲线AG、曲线AH和折痕线GH围成,上述曲线AG是出口边(2)上的一段,曲线AG长度小于或者等于1/2的出口边(2)的长度。2. A sheet metal centrifugal wind wheel according to claim 1, characterized in that: the angular bending part (101) is surrounded by a curve AG, a curve AH and a crease line GH, and the curve AG is the outlet edge. For a section on (2), the length of the curve AG is less than or equal to 1/2 of the length of the exit side (2). 3.根据权利要求1或2所述的一种钣金离心风轮,其特征在于:用垂直于风轮旋转轴L且与曲线AG相交的若干平面截取风轮得到若干条叶片型线,折痕线GH和出口边(2)与若干条叶片型线相交,每一条叶片型线与折痕线GH和出口边相交形成曲线VO,曲线VO的长度从点G到顶点A逐渐增大。3. A sheet metal centrifugal wind wheel according to claim 1 or 2, characterized in that: the wind wheel is intercepted by several planes perpendicular to the rotor rotation axis L and intersecting with the curve AG to obtain several blade profile lines. The mark line GH and the outlet edge (2) intersect with several blade profile lines. Each blade profile line intersects the crease line GH and the outlet edge to form a curve VO. The length of the curve VO gradually increases from point G to vertex A. 4.一种钣金离心风轮,包括轮盘(200)、轮盖(300)、若干叶片(100)组成,若干叶片(100)安装在轮盘(200)与轮盖(300)之间,叶片(100)包括进口边(1)、出口边(2)、叶根(3)和叶顶(4),其特征在于:与出口边(2)等距偏移一段距离形成折痕线NR,折痕线NR与出口边(2)围成等距弯折部(103),等距弯折部(103)向风轮旋转轴L中心折弯。4. A sheet metal centrifugal wind wheel, including a wheel disk (200), a wheel cover (300), and a number of blades (100). The several blades (100) are installed between the wheel disk (200) and the wheel cover (300) , the blade (100) includes an inlet edge (1), an outlet edge (2), a blade root (3) and a blade tip (4), and is characterized in that: it is equidistant from the outlet edge (2) to form a crease line. NR, the crease line NR and the outlet edge (2) form an equidistant bending part (103), and the equidistant bending part (103) is bent toward the center of the rotor rotation axis L. 5.根据权利要求4所述的一种钣金离心风轮,其特征在于:等距偏移是指出口边上的每一个点沿着对应的叶片型线偏移相当距离E。5. A sheet metal centrifugal wind wheel according to claim 4, characterized in that: equidistant offset means that each point on the edge of the outlet is offset by a considerable distance E along the corresponding blade profile line.
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