CN204493271U - A kind of centrifugal blower fan blade wheel - Google Patents
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Abstract
一种离心风机叶轮,包括轮盘和安装在轮盘上的叶片,其特征在于:所述的叶片包括宽叶片和窄叶片,两相邻的宽叶片之间形成叶道,所述的窄叶片设于叶道内,叶道在圆周方向上的长度d1、窄叶片与相邻宽叶片压力面的距离d2,满足条件:1/4<d2/d1<1/2,窄叶片的径向宽度d3、宽叶片的径向宽度d4,满足条件1/3<d3/d4<2/3。本实用新型的优点在于:该离心风机叶轮将位于叶道内的窄叶片的径向宽度设计为宽叶片径向宽度的1/3至2/3,且窄叶片与相邻宽叶片压力面的距离设计为叶道长度的1/4至1/2,从而可以有效减小叶片入口处的阻塞,降低叶道扩张角,使风机的噪声降低且压力和流量损失较小,即可以在尽量不损失风机气动性能的前提下,尽可能地降低风机气动噪声。
A centrifugal fan impeller, including a disc and blades installed on the disc, characterized in that: the blades include wide blades and narrow blades, a blade path is formed between two adjacent wide blades, and the narrow blades Set in the blade passage, the length d1 of the blade passage in the circumferential direction, the distance d2 between the narrow blade and the pressure surface of the adjacent wide blade, satisfy the conditions: 1/4<d2/d1<1/2, the radial width of the narrow blade d3 , The radial width d4 of the wide blade satisfies the condition 1/3<d3/d4<2/3. The utility model has the advantages that: the impeller of the centrifugal fan designs the radial width of the narrow blade located in the blade passage as 1/3 to 2/3 of the radial width of the wide blade, and the distance between the narrow blade and the pressure surface of the adjacent wide blade It is designed to be 1/4 to 1/2 of the length of the blade path, which can effectively reduce the blockage at the blade inlet, reduce the expansion angle of the blade path, reduce the noise of the fan and reduce the loss of pressure and flow, that is, it can be used as little as possible. Under the premise of improving the aerodynamic performance of the fan, reduce the aerodynamic noise of the fan as much as possible.
Description
技术领域technical field
本实用新型涉及一种离心风机,尤其是涉及一种离心风机叶轮。The utility model relates to a centrifugal fan, in particular to an impeller of the centrifugal fan.
背景技术Background technique
叶轮是离心风机的重要部件,离心风机的工作原理是气体通过离心力的作用,经其叶轮中心部位吸入,然后流经叶片之间的叶道并往外流出。研究发现,离心风机叶轮通道中的流动扩压度较大,容易产生气流分离,特别是叶轮后部的吸力面附近分离现象严重,导致叶轮出口周向气流的分布很不均匀。由于叶轮转速较高,因而不均匀的叶轮出口气流会与周围非轴对称分布的静止部件产生强烈的非定常干涉,这是产生离心风机气动噪声,特别是离散噪声的主要原因之一,并对风机的气动性能带来不利影响。The impeller is an important part of the centrifugal fan. The working principle of the centrifugal fan is that the gas is sucked through the center of the impeller through the action of centrifugal force, and then flows through the leaf passage between the blades and flows out. The study found that the flow in the impeller channel of the centrifugal fan has a large degree of pressure diffusion, which is prone to air separation, especially near the suction surface at the rear of the impeller, which leads to uneven distribution of the circumferential air flow at the impeller outlet. Due to the high speed of the impeller, the uneven air flow at the outlet of the impeller will produce strong unsteady interference with the surrounding non-axisymmetrically distributed stationary parts, which is one of the main reasons for the aerodynamic noise of the centrifugal fan, especially the discrete noise, and has a great impact on The aerodynamic performance of the fan is adversely affected.
风机的能量损失分为流动损失、容积损失和机械损失,其中以流动损失为主。由于气体具有粘性,风机叶轮和蜗壳存在不同程度的摩擦和分离等损失,使得风机效率很难达到理想要求,离心风机叶片对叶轮内的实际流动情况起主要作用,合理优化叶片型线和叶片型式,可有效提升风机与其他综合性能。叶片尾迹和蜗舌之间的周期性作用是基频(叶片通过频率)噪声成为离心风机主要气动噪声的原因。The energy loss of the fan is divided into flow loss, volume loss and mechanical loss, among which flow loss is the main one. Due to the viscosity of the gas, there are different degrees of friction and separation losses between the fan impeller and the volute, making it difficult for the fan efficiency to meet the ideal requirements. The centrifugal fan blade plays a major role in the actual flow in the impeller, and the blade profile and blade are reasonably optimized. Type, can effectively improve the fan and other comprehensive performance. The periodic action between the blade wake and the volute tongue is the reason why the fundamental frequency (blade passing frequency) noise becomes the main aerodynamic noise of the centrifugal fan.
目前,国内外对离心风机气动性能和气动噪声的研究大都着眼于改变蜗舌的倾角、蜗壳形状、叶片形状及数量等方面。近年来国内外的一些研究表明,合理布置大小叶片能使离心叶轮出口流动参数沿周向分布比采用单列叶片更加均匀,对降低叶轮与静止部件间的非定常冲击损失及气动噪声有利。另外,气动性能和气动噪声还常常存在着相互制约的关系,一方的提升有时会带来另一方的下降,能够同时改善离心风机气动性能和气动噪声的方法是当前研究所追求的主要目标。为了降低基频处的噪声峰值,一些学者已经提出了将叶轮设计成采用不等距叶片的结构,以此将基频处的噪声峰值分散,从而降低总的噪声级。At present, most of the research on the aerodynamic performance and aerodynamic noise of centrifugal fans at home and abroad focuses on changing the inclination angle of the volute tongue, the shape of the volute, the shape and number of blades, and so on. Some studies at home and abroad in recent years have shown that the reasonable arrangement of large and small blades can make the flow parameters of the centrifugal impeller outlet distributed more uniformly in the circumferential direction than the single row of blades, which is beneficial to reduce the unsteady impact loss and aerodynamic noise between the impeller and the stationary parts. In addition, aerodynamic performance and aerodynamic noise often have a mutual restrictive relationship. The improvement of one sometimes leads to the decline of the other. The method that can improve the aerodynamic performance and aerodynamic noise of centrifugal fans at the same time is the main goal of current research. In order to reduce the noise peak at the fundamental frequency, some scholars have proposed to design the impeller as a structure with unequal-spaced blades, so as to disperse the noise peak at the fundamental frequency, thereby reducing the overall noise level.
实用新型内容Utility model content
本实用新型所要解决的技术问题是针对上述现有技术现状,提供一种能有效减小叶道气流漩涡的离心风机叶轮。The technical problem to be solved by the utility model is to provide a centrifugal fan impeller which can effectively reduce the vortex of the air flow in the blade path in view of the above-mentioned existing technical situation.
本实用新型解决上述技术问题所采用的技术方案为:该离心风机叶轮,包括轮盘和安装在轮盘上的叶片,其特征在于:所述的叶片包括宽叶片和窄叶片,两相邻的宽叶片之间形成叶道,所述的窄叶片设于叶道内,叶道在圆周方向上的长度d1、窄叶片与相邻宽叶片压力面的距离d2,满足条件:1/4<d2/d1<1/2,窄叶片的径向宽度d3、宽叶片的径向宽度d4,满足条件1/3<d3/d4<2/3。The technical scheme adopted by the utility model to solve the above-mentioned technical problems is: the impeller of the centrifugal fan includes a wheel disc and blades installed on the wheel disc, and is characterized in that: the blades include wide blades and narrow blades, and A leaf path is formed between the wide blades, and the narrow blade is arranged in the leaf path. The length d1 of the leaf path in the circumferential direction and the distance d2 between the narrow blade and the pressure surface of the adjacent wide blade satisfy the condition: 1/4<d2/ d1<1/2, the radial width d3 of the narrow blade and the radial width d4 of the wide blade satisfy the condition 1/3<d3/d4<2/3.
优选地,所述的d1与d2以及d3与d4的关系满足条件:d2/d1=1/3且d3/d4=1/2。根据研究得知,对于前向离心风机,加入窄叶片的径向宽度越大,其全压越高,但升高的幅度减小,并且,在一定范围内,窄叶片从吸力面向压力面移动,压力和效率都变大,但当窄叶片离压力面的距离为相应叶道长度1/3的后,靠近压力面的压力反而降低。所以,采用上述结构,更有利于减小甚至消除叶道气流漩涡,从而更有利于减小叶片入口处的阻塞和降低叶道扩张角,进而使风机的噪声降低且压力和流量损失较小。Preferably, the relationship between d1 and d2 and d3 and d4 satisfies the conditions: d2/d1=1/3 and d3/d4=1/2. According to the research, for the forward centrifugal fan, the larger the radial width of the narrow blade is, the higher the total pressure is, but the range of increase is reduced, and, within a certain range, the narrow blade moves from the suction side to the pressure side , both pressure and efficiency increase, but when the distance between the narrow blade and the pressure surface is 1/3 of the corresponding blade path length, the pressure close to the pressure surface decreases instead. Therefore, adopting the above-mentioned structure is more conducive to reducing or even eliminating the airflow vortex in the blade passage, thereby reducing the blockage at the blade inlet and reducing the expansion angle of the blade passage, thereby reducing the noise of the fan and reducing the pressure and flow loss.
进一步优选,所述的窄叶片与相邻的宽叶片向同一侧弯曲。Further preferably, the narrow blade is bent to the same side as the adjacent wide blade.
窄叶片可以有多种不同的分布结构,一种优选方案为,所述的宽叶片与窄叶片间隔分布,即在每个所述的叶道内均设有一片窄叶片。这样,窄叶片的数量与宽叶片的数量相同。The narrow blades can have many different distribution structures. A preferred solution is that the wide blades and the narrow blades are distributed at intervals, that is, a narrow blade is provided in each of the blade passages. In this way, the number of narrow blades is the same as the number of wide blades.
另一种优选方案为,在所述的两相邻窄叶片之间设有至少两片宽叶片。Another preferred solution is that at least two wide blades are provided between the two adjacent narrow blades.
又一种优选方案为,在所述的两相邻窄叶片之间设有四片宽叶片。即窄叶片的数量为宽叶片数量的1/4。Another preferred solution is that four wide blades are arranged between the two adjacent narrow blades. That is, the number of narrow blades is 1/4 of the number of wide blades.
窄叶片可以设置在叶道的不同位置,一种优选方案是,所述的窄叶片设于叶道的出气口处。The narrow blades can be arranged at different positions of the blade passage, and a preferred solution is that the narrow blades are arranged at the air outlet of the blade passage.
另一种优选方案是,所述的窄叶片设于叶道的进气口处。实验发现,叶道的进气口采用窄叶片后,可以明显减小甚至消除整个叶道的气流漩涡。Another preferred solution is that the narrow blades are arranged at the air inlet of the blade passage. Experiments have found that the airflow vortex of the entire blade path can be significantly reduced or even eliminated when narrow blades are used for the air inlet of the blade path.
与现有技术相比,本实用新型的优点在于:该离心风机叶轮将位于叶道内的窄叶片的径向宽度设计为宽叶片径向宽度的1/3至2/3,且窄叶片与相邻宽叶片压力面的距离设计为叶道长度的1/4至1/2,可以有效减小叶道气流漩涡,从而可以有效减小叶片入口处的阻塞并降低叶道扩张角,使风机的噪声降低且压力和流量损失较小,即可以在尽量不损失风机气动性能的前提下,尽可能地降低风机气动噪声。Compared with the prior art, the utility model has the advantages that: the radial width of the narrow blade located in the blade passage is designed to be 1/3 to 2/3 of the radial width of the wide blade in the impeller of the centrifugal fan, and the narrow blade and the corresponding The distance between the pressure surface of the adjacent wide blade is designed to be 1/4 to 1/2 of the length of the blade path, which can effectively reduce the airflow vortex of the blade path, thereby effectively reducing the blockage at the blade inlet and reducing the expansion angle of the blade path, so that the fan's The noise is reduced and the loss of pressure and flow is small, that is, the aerodynamic noise of the fan can be reduced as much as possible on the premise of not losing the aerodynamic performance of the fan as much as possible.
附图说明Description of drawings
图1为本实用新型实施例一的结构示意图;Fig. 1 is the structural representation of the utility model embodiment one;
图2为本实用新型实施例一的剖视图;Fig. 2 is a sectional view of Embodiment 1 of the utility model;
图3为图2中A部分的放大示意图;Fig. 3 is the enlarged schematic view of part A in Fig. 2;
图4为本实用新型实施例二的结构示意图;Fig. 4 is the structural representation of the second embodiment of the utility model;
图5为本实用新型实施例三的结构示意图;Fig. 5 is a structural schematic diagram of a third embodiment of the utility model;
图6为本实用新型实施例四的结构示意图;Fig. 6 is a schematic structural view of Embodiment 4 of the utility model;
图7为本实用新型实施例五的结构示意图;Fig. 7 is a schematic structural view of Embodiment 5 of the utility model;
图8为本实用新型实施例六的结构示意图。Fig. 8 is a schematic structural diagram of Embodiment 6 of the present utility model.
具体实施方式Detailed ways
以下结合附图实施例对本实用新型作进一步详细描述。The utility model is described in further detail below in conjunction with the accompanying drawings.
实施例一:Embodiment one:
如图1至图3所示,本实施例中的叶轮包括轮盘1和安装在轮盘1上的宽叶片2、窄叶片3,宽叶片2间隔均匀地分布在轮盘1的外圆周上,两片宽叶片2之间形成叶道4。窄叶片3设于叶道4内,且两相邻窄叶片3之间设有四片宽叶片2,即窄叶片3的数量为宽叶片2数量的1/4,比如对于常规的离心风机叶轮,若宽叶片2数量为60片,则窄叶片3的数量为15片。并且,窄叶片3与相邻的宽叶片2向同一侧弯曲。As shown in Figures 1 to 3, the impeller in this embodiment includes a wheel disc 1 and wide blades 2 and narrow blades 3 installed on the wheel disc 1, and the wide blades 2 are evenly distributed on the outer circumference of the wheel disc 1 , A blade path 4 is formed between two wide blades 2 . The narrow blades 3 are arranged in the blade passage 4, and four wide blades 2 are arranged between two adjacent narrow blades 3, that is, the number of the narrow blades 3 is 1/4 of the number of the wide blades 2, such as for a conventional centrifugal fan impeller , if the number of wide blades 2 is 60, then the number of narrow blades 3 is 15. Also, the narrow blade 3 is bent to the same side as the adjacent wide blade 2 .
另外,本实施例中,窄叶片3设于叶道4的进气口处,实验表明,叶道进气口设置窄叶片3后,叶道气流几乎不产生漩涡,可以有效减小叶片入口处的阻塞,降低叶道扩张角以减少离损失,同时减小滑移系数而提高做功能力。设叶道4在圆周方向上的长度为d1,宽叶片2的凹面为压力面21,宽叶片2的凸面为吸力面22,窄叶片3与相邻宽叶片2压力面21的距离为d2,则满足条件:d2/d1=1/3。设窄叶片3的径向宽度为d3,宽叶片2的径向宽度为d4,则满足条件:d3/d4=1/2。采用上述结构后,风机的噪声降低且压力和流量损失较小,即可以在尽量不损失风机气动性能的前提下,尽可能地降低风机气动噪声。In addition, in this embodiment, the narrow vane 3 is arranged at the air inlet of the vane passage 4. Experiments have shown that after the narrow vane 3 is arranged at the air inlet of the vane passage, the air flow in the vane passage hardly generates vortices, which can effectively reduce the blockage at the entrance of the vane passage. , reduce the expansion angle of the blade path to reduce the separation loss, and at the same time reduce the slip coefficient to improve the work ability. Assume that the length of the blade path 4 in the circumferential direction is d1, the concave surface of the wide blade 2 is the pressure surface 21, the convex surface of the wide blade 2 is the suction surface 22, and the distance between the narrow blade 3 and the pressure surface 21 of the adjacent wide blade 2 is d2, Then the condition is satisfied: d2/d1=1/3. Assuming that the radial width of the narrow blade 3 is d3 and the radial width of the wide blade 2 is d4, then the condition: d3/d4=1/2 is satisfied. After adopting the above structure, the noise of the fan is reduced and the loss of pressure and flow is small, that is, the aerodynamic noise of the fan can be reduced as much as possible on the premise of not losing the aerodynamic performance of the fan as much as possible.
实施例二:Embodiment two:
如图4所示,本实施例中,窄叶片3设于叶道4的进气口处,两相邻窄叶片3之间设有两片宽叶片2,即窄叶片3的数量为宽叶片2数量的一半。其余结构与实施例一中的结构相同,在此不展开描述。As shown in Figure 4, in the present embodiment, the narrow vane 3 is arranged at the air inlet of the blade passage 4, and two wide vanes 2 are arranged between two adjacent narrow vanes 3, that is, the number of the narrow vanes 3 is the wide vane. 2 half of the quantity. The rest of the structure is the same as that in Embodiment 1, and will not be described here.
实施例三:Embodiment three:
如图5所示,本实施例中,窄叶片3设于叶道4的进气口处,在每个叶道4内均设有一片窄叶片3,即窄叶片3与宽叶片2的数量相同且间隔分布。其余结构与实施例一中的结构相同,在此不展开描述。As shown in Figure 5, in the present embodiment, the narrow vane 3 is arranged at the air inlet of the blade passage 4, and a piece of narrow blade 3 is arranged in each blade passage 4, that is, the number of the narrow blade 3 and the wide blade 2 same and spaced apart. The rest of the structure is the same as that in Embodiment 1, and will not be described here.
实施例四:Embodiment four:
如图6所示,本实施例中,窄叶片3设于叶道4的出气口处,在每个叶道4内均设有一片窄叶片3,即窄叶片3与宽叶片2的数量相同且间隔分布。设叶道4的长度为d1,设窄叶片3与相邻宽叶片2压力面的距离为d2,则满足d2/d1=1/3,设窄叶片3的径向宽度为d3,宽叶片2的径向宽度为d4,则满足且d3/d4=1/2。As shown in Figure 6, in this embodiment, the narrow blades 3 are arranged at the air outlet of the leaf passage 4, and a piece of narrow blade 3 is arranged in each leaf passage 4, that is, the number of the narrow blades 3 and the wide blades 2 are the same And interval distribution. Let the length of the blade path 4 be d1, set the distance between the narrow blade 3 and the pressure surface of the adjacent wide blade 2 to be d2, then satisfy d2/d1=1/3, set the radial width of the narrow blade 3 to be d3, and the wide blade 2 The radial width of is d4, and d3/d4=1/2 is satisfied.
实施例五:Embodiment five:
如图7所示,本实施例中,窄叶片3设于叶道4的出气口处,两相邻窄叶片3之间设有两片宽叶片2,即窄叶片3的数量为宽叶片2数量的一半,其余结构与实施例四中的结构相同,在此不展开描述。As shown in Figure 7, in the present embodiment, the narrow blade 3 is arranged at the air outlet of the blade passage 4, and two wide blades 2 are arranged between two adjacent narrow blades 3, that is, the number of the narrow blades 3 is the width of the wide blade 2. half of the number, and the rest of the structure is the same as that in Embodiment 4, and will not be described here.
实施例六:Embodiment six:
如图8所示,本实施例中,窄叶片3设于叶道4的出气口处,每三片窄叶片3间隔有一个没有设置窄叶片3的叶道4,其余结构与实施例四中的结构相同,在此不展开描述。As shown in Figure 8, in this embodiment, the narrow blades 3 are arranged at the air outlet of the blade passage 4, and every three narrow blades 3 are separated by a blade passage 4 without a narrow blade 3, and the rest of the structure is the same as in Embodiment 4 The structure is the same and will not be described here.
以上所述仅为本实用新型的优选实施方式,应当指出,对于本领域普通技术人员而言,在不脱离本实用新型的原理前提下,可以对本实用新型进行多种改型或改进,比如窄叶片与宽叶片之间还可以采用其他间隔分布结构,这些均被视为本实用新型的保护范围之内。The above descriptions are only preferred implementations of the present utility model. It should be pointed out that for those skilled in the art, without departing from the principle of the present utility model, various modifications or improvements can be made to the present utility model, such as narrow Other spacing distribution structures can also be used between the blade and the wide blade, and these are all considered within the protection scope of the present utility model.
Claims (8)
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109944828A (en) * | 2019-04-01 | 2019-06-28 | 青岛海尔智能技术研发有限公司 | A kind of centrifugal blower and electric appliance |
CN111350691A (en) * | 2020-04-17 | 2020-06-30 | 山东攀峰通风设备有限公司 | High-pressure centrifugal fan impeller |
CN113530883A (en) * | 2021-07-15 | 2021-10-22 | 广东顺威精密塑料股份有限公司 | Combined centrifugal impeller |
-
2015
- 2015-02-05 CN CN201520081238.1U patent/CN204493271U/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109944828A (en) * | 2019-04-01 | 2019-06-28 | 青岛海尔智能技术研发有限公司 | A kind of centrifugal blower and electric appliance |
CN111350691A (en) * | 2020-04-17 | 2020-06-30 | 山东攀峰通风设备有限公司 | High-pressure centrifugal fan impeller |
CN113530883A (en) * | 2021-07-15 | 2021-10-22 | 广东顺威精密塑料股份有限公司 | Combined centrifugal impeller |
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