CN205744592U - A kind of fan blade in multi-wing centrifugal fan - Google Patents
A kind of fan blade in multi-wing centrifugal fan Download PDFInfo
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- CN205744592U CN205744592U CN201620076052.1U CN201620076052U CN205744592U CN 205744592 U CN205744592 U CN 205744592U CN 201620076052 U CN201620076052 U CN 201620076052U CN 205744592 U CN205744592 U CN 205744592U
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Abstract
本实用新型公开了一种多翼离心风机中的风机叶片,包括若干叶片本体,叶片本体的两端面均为弧面,其中,叶片本体的一个弧面上为设有锯齿形结构,叶片本体的另一个弧面上设有仿生非光滑结构,气流经所述仿生非光滑结构后再经所述锯齿形结构。本实用新型能够有效地降低噪声、提高风量、增加风压。
The utility model discloses a fan blade in a multi-blade centrifugal fan, which comprises a plurality of blade bodies. The other arc surface is provided with a bionic non-smooth structure, and the air flows through the bionic non-smooth structure and then passes through the zigzag structure. The utility model can effectively reduce noise, increase air volume and increase air pressure.
Description
技术领域technical field
本实用新型涉及一种风机叶片,具体涉及一种多翼离心风机中的风机叶片。The utility model relates to a fan blade, in particular to a fan blade in a multi-wing centrifugal fan.
背景技术Background technique
多翼离心风机具有流量系数大、压力系数高和结构紧凑等特点,在工业产品中取得广泛应用,目前油烟机行业的风机绝大部分都采用多翼离心风机,此外也被广泛地应用在家用空调器中。与人们生活息息相关的空调器和吸油烟机的噪声和效率成为倍受关注的两大性能指标。目前多翼离心风机多采用等弦长直叶片叶轮结构,如图1所示,即叶片进口缘和出口缘与叶轮轴线平行,沿翼展方向各截面形状、大小相同,这种直线型叶轮的压力系数在0.5以下,在相同条件下的压力采用高转速或者大叶轮直径才能实现,而增大叶轮直径受到了空间的限制,提高转速又增大了噪声。其次,这种叶片进口安装角在进口叶轮边缘所有各点上是相同的,而该处气流速度是不均匀,这样就使得叶轮边缘上所有各点上的气流对叶轮造成大大冲击,减少了叶轮的使用寿命,并伴有大的噪声;而在片的出风口处,由于流道阻塞,容易形成涡流,影响风机出风,使风机的效率低下,并且由于漩涡的存在,增大了风机的涡流噪声,因此,采用等弦长直叶片叶轮结构,使叶轮的效率大大降低,目前吸油烟机的效率都比较低,大约只有25%左右,而吸油烟机和空调器又被广泛应用于人们的日常生活,因此节能显得十分必要。Multi-blade centrifugal fans have the characteristics of large flow coefficient, high pressure coefficient and compact structure, and have been widely used in industrial products. At present, most of the fans in the range hood industry use multi-blade centrifugal fans. In addition, they are also widely used in household in the air conditioner. The noise and efficiency of air conditioners and range hoods, which are closely related to people's lives, have become two performance indicators that have attracted much attention. At present, multi-blade centrifugal fans mostly adopt the impeller structure of equal-chord straight blades, as shown in Figure 1, that is, the inlet and outlet edges of the blades are parallel to the axis of the impeller, and the shape and size of each section along the span direction are the same. If the pressure coefficient is below 0.5, the pressure under the same conditions can only be achieved by using high speed or large impeller diameter, and increasing the impeller diameter is limited by space, and increasing the speed increases the noise. Secondly, the installation angle of the blade inlet is the same at all points on the edge of the impeller, and the airflow velocity at this place is uneven, which makes the airflow at all points on the edge of the impeller have a great impact on the impeller, reducing the impact of the impeller. The service life of the fan is accompanied by a large noise; and at the air outlet of the sheet, due to the blockage of the flow channel, it is easy to form a vortex, which affects the air output of the fan, making the efficiency of the fan low, and due to the existence of the vortex, it increases the fan's performance. Eddy current noise, therefore, the use of equal-chord straight blade impeller structure greatly reduces the efficiency of the impeller. At present, the efficiency of range hoods is relatively low, only about 25%, and range hoods and air conditioners are widely used in people daily life, so energy saving is very necessary.
实用新型内容Utility model content
本实用新型的目的在于克服上述现有技术的缺点,提供了一种多翼离心风机中的风机叶片,该风机叶片能够有效地降低噪声、提高风量、增加风压。The purpose of the utility model is to overcome the above-mentioned shortcomings of the prior art, and provide a fan blade in a multi-blade centrifugal fan, which can effectively reduce noise, increase air volume, and increase wind pressure.
为达到上述目的,本实用新型所述的多翼离心风机中的风机叶片包括若干叶片本体,叶片本体的两端面均为弧面,其中,叶片本体的一个弧面上为设有锯齿形结构,叶片本体的另一个弧面上设有仿生非光滑结构,气流经所述仿生非光滑结构后再经所述锯齿形结构。In order to achieve the above purpose, the fan blades in the multi-blade centrifugal fan described in the utility model include several blade bodies, and both ends of the blade bodies are arc surfaces, wherein one arc surface of the blade body is provided with a zigzag structure, Another arc surface of the blade body is provided with a bionic non-smooth structure, and the air flows through the bionic non-smooth structure and then passes through the zigzag structure.
所述仿生非光滑结构为波浪形结构。The bionic non-smooth structure is a wavy structure.
所述锯齿形结构中相邻两齿之间的夹角为30-50°。The included angle between two adjacent teeth in the zigzag structure is 30-50°.
所述锯齿形结构中各齿的高度为0.4mm-2mm。The height of each tooth in the zigzag structure is 0.4mm-2mm.
所述仿生非光滑结构中各波峰的高度为0.2mm-0.8mm。The height of each peak in the bionic non-smooth structure is 0.2mm-0.8mm.
所述仿生非光滑结构中相邻两波谷之间的间距为3mm-7mm。The distance between two adjacent troughs in the bionic non-smooth structure is 3mm-7mm.
叶片本体的弧面上设有两组锯齿形结构,所述两组锯齿形结构位于对应弧面的两侧。Two sets of sawtooth structures are provided on the arc surface of the blade body, and the two sets of sawtooth structures are located on both sides of the corresponding arc surface.
叶片本体的弧面上设有两组仿生非光滑结构,所述两组仿生非光滑结构位于对应弧面的两侧。Two groups of bionic non-smooth structures are provided on the arc surface of the blade body, and the two groups of bionic non-smooth structures are located on both sides of the corresponding arc surface.
本实用新型具有以下有益效果:The utility model has the following beneficial effects:
本实用新型所述的多翼离心风机中的风机叶片包括叶片本体,所述叶片本体的两端面均为弧面,从而使叶片本体沿轴向的横截面不同,减少进口气流的偏斜程度及冲击损失,降低气流通道前端进口处的摩擦损失和叶道进口的阻塞,同时使进口过流断面上气流速度梯度分布均匀,并使气流速度在转弯过程中适应从风机叶片顶端到底部的快速变化,从而降低叶道弯曲形成的分离损失,减少叶轮顶端出口涡流及二次流,改善进气流动,降低湍流噪声,提高离心风机效率。另外,所述叶片本体的一个弧面上设有锯齿形结构,能够减少叶片出风口处由于流道阻塞生成的涡流,同时能够消弱涡流的强度,改善气流在叶道内的流动;所述叶片本体的另一个弧面上设有仿生非光滑结构,能够消弱声波的反射,减少风机叶片进口区形成的涡流,改善气流的进气流动,消弱气流对风机叶片前缘的冲击,降低离心风机的噪声。The fan blade in the multi-blade centrifugal fan described in the utility model includes a blade body, and both ends of the blade body are arc-shaped, so that the cross-section of the blade body along the axial direction is different, and the degree of deflection and the degree of inclination of the inlet airflow are reduced. Impact loss, reduce the friction loss at the entrance of the front end of the airflow channel and the blockage of the blade passage entrance, and at the same time make the airflow velocity gradient distribution on the inlet flow section uniform, and make the airflow velocity adapt to the rapid change from the top to the bottom of the fan blade during the turning process , so as to reduce the separation loss caused by the bending of the blade path, reduce the outlet vortex and secondary flow at the top of the impeller, improve the intake flow, reduce turbulent noise, and improve the efficiency of the centrifugal fan. In addition, a zigzag structure is provided on an arc surface of the blade body, which can reduce the vortex generated at the air outlet of the blade due to blockage of the flow channel, and at the same time weaken the intensity of the vortex and improve the flow of air in the blade channel; the blade The other curved surface of the body is equipped with a bionic non-smooth structure, which can weaken the reflection of sound waves, reduce the vortex formed in the inlet area of the fan blade, improve the air intake flow, weaken the impact of the air flow on the front edge of the fan blade, and reduce the centrifugal force. Fan noise.
附图说明Description of drawings
图1为现有风机叶片的结构示意图。Fig. 1 is a schematic structural diagram of a conventional fan blade.
图2为本实用新型的结构示意图;Fig. 2 is the structural representation of the utility model;
图3为本实用新型中局部放大图;Fig. 3 is a partially enlarged view in the utility model;
图4为现有多翼离心风机的结构示意图;Fig. 4 is the structural representation of existing multi-blade centrifugal fan;
图5为本发明中的多翼离心风机的结构示意图。Fig. 5 is a structural schematic diagram of the multi-blade centrifugal fan in the present invention.
其中,1为叶片本体、2为仿生非光滑结构、3为锯齿形结构。Among them, 1 is the blade body, 2 is the bionic non-smooth structure, and 3 is the zigzag structure.
具体实施方式detailed description
下面结合附图对本实用新型做进一步详细描述:Below in conjunction with accompanying drawing, the utility model is described in further detail:
参考图2,本实用新型所述的多翼离心风机中的风机叶片包括若干叶片本体1,叶片本体1的两端面均为弧面,其中,叶片本体1的一个弧面上为设有锯齿形结构3,叶片本体1的另一个弧面上设有仿生非光滑结构2,气流经所述仿生非光滑结构2后再经所述锯齿形结构3,锯齿形结构3中相邻两齿之间的夹角为30°-50°,锯齿形结构3中各齿的高度为0.4mm-2mm,仿生非光滑结构2中各波峰的高度为0.2mm-0.8mm,仿生非光滑结构2中相邻两波谷之间的间距为3mm-7mm,叶片本体1的弧面上设有两组锯齿形结构3,所述两组锯齿形结构3位于对应弧面的两侧,叶片本体1的弧面上设有两组仿生非光滑结构2,所述两组仿生非光滑结构2位于对应弧面的两侧,仿生非光滑结构2为波浪形结构。With reference to Fig. 2, the fan blade in the multi-blade centrifugal fan described in the utility model comprises several blade bodies 1, and both ends of the blade body 1 are arc surfaces, wherein, one arc surface of the blade body 1 is provided with a zigzag Structure 3, the other arc surface of the blade body 1 is provided with a bionic non-smooth structure 2, the airflow passes through the bionic non-smooth structure 2 and then passes through the zigzag structure 3, between two adjacent teeth in the zigzag structure 3 The included angle is 30°-50°, the height of each tooth in the zigzag structure 3 is 0.4mm-2mm, the height of each peak in the bionic non-smooth structure 2 is 0.2mm-0.8mm, and the adjacent The distance between the two troughs is 3mm-7mm. Two sets of zigzag structures 3 are arranged on the arc surface of the blade body 1. The two sets of zigzag structures 3 are located on both sides of the corresponding arc surface. The arc surface of the blade body 1 There are two groups of bionic non-smooth structures 2, the two groups of bionic non-smooth structures 2 are located on both sides of the corresponding arc surface, and the bionic non-smooth structures 2 are wavy structures.
经实验,采用本实用新型的多翼离心风机与传统的多翼离心风机相比,风量提高5%以上,风压提高6%以上,噪声降低0.5dB以上,根据离心风机的功率P=Q*B表明,采用本实用新型的多翼离心风机的效率更高,其中,B为风机的全风压,Q为风量。另外,本实用新型的结构简单,制造成本低,可以大大减轻叶轮的重量,从而提高离心风机的驱动电机的工作效率,因此可以选配较低功率的电机就可以满足原来多翼离心风机的需求,节能环保。Through experiments, compared with the traditional multi-blade centrifugal fan, the multi-blade centrifugal fan of the present utility model can increase the air volume by more than 5%, increase the wind pressure by more than 6%, and reduce the noise by more than 0.5dB. According to the power P=Q* of the centrifugal fan B shows that the efficiency of the multi-blade centrifugal fan of the present invention is higher, wherein, B is the full wind pressure of the fan, and Q is the air volume. In addition, the utility model has a simple structure and low manufacturing cost, which can greatly reduce the weight of the impeller, thereby improving the working efficiency of the driving motor of the centrifugal fan, so that a motor with a lower power can be selected to meet the original multi-blade centrifugal fan requirements. ,Energy saving and environmental protection.
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| CN201620076052.1U CN205744592U (en) | 2016-01-26 | 2016-01-26 | A kind of fan blade in multi-wing centrifugal fan |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108980101A (en) * | 2018-08-02 | 2018-12-11 | 江苏大学镇江流体工程装备技术研究院 | A kind of bionic blade based on shark surface drag reduction technology |
| CN111079239A (en) * | 2019-12-19 | 2020-04-28 | 中国航空发动机研究院 | Bionic compressor cascade modeling method |
-
2016
- 2016-01-26 CN CN201620076052.1U patent/CN205744592U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108980101A (en) * | 2018-08-02 | 2018-12-11 | 江苏大学镇江流体工程装备技术研究院 | A kind of bionic blade based on shark surface drag reduction technology |
| CN108980101B (en) * | 2018-08-02 | 2023-07-04 | 江苏大学镇江流体工程装备技术研究院 | Bionic blade based on shark surface drag reduction technology |
| CN111079239A (en) * | 2019-12-19 | 2020-04-28 | 中国航空发动机研究院 | Bionic compressor cascade modeling method |
| CN111079239B (en) * | 2019-12-19 | 2023-07-21 | 中国航空发动机研究院 | Bionic compressor blade grid modeling method |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161130 Termination date: 20180126 |