CN111536077A - High-specific-speed double-outlet volute centrifugal pump - Google Patents

High-specific-speed double-outlet volute centrifugal pump Download PDF

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CN111536077A
CN111536077A CN202010395156.XA CN202010395156A CN111536077A CN 111536077 A CN111536077 A CN 111536077A CN 202010395156 A CN202010395156 A CN 202010395156A CN 111536077 A CN111536077 A CN 111536077A
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impeller
blade
cross
double outlet
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陈会向
陈雅楠
阚阚
周大庆
郑源
邵煜
苏文博
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Hohai University HHU
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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
    • F04D29/426Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • 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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/24Vanes
    • F04D29/242Geometry, shape
    • 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
    • F04D29/426Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps
    • F04D29/4293Details of fluid inlet or outlet

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  • Mechanical Engineering (AREA)
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Abstract

本发明公开了一种高比转速双出口式蜗壳离心泵,所述双出口式蜗壳内侧环形开口处设置有叶轮,叶轮底部连接有吸水管道,双出口式蜗壳的两个出水口均连接有出水管道;所述叶轮的叶片采用类圆柱形扭曲结构,叶片的正面与反面从上至下由不同曲率的曲面平滑连接;所述吸水管道、叶轮、双出口式蜗壳的中心在同一轴线上。本发明通过两个出水口实现双向出水,提高了离心泵出流效率,同时增强了水流在蜗壳圆周方向上的速度分量,改善了蜗壳出口处的水流条件,减小水力损失,使得离心泵具有良好的水力性能和运行效率。

Figure 202010395156

The invention discloses a high specific speed double outlet volute centrifugal pump. An impeller is arranged at the inner annular opening of the double outlet volute, a suction pipe is connected at the bottom of the impeller, and two water outlets of the double outlet volute are A water outlet pipe is connected; the blade of the impeller adopts a quasi-cylindrical twisted structure, and the front and back sides of the blade are smoothly connected by curved surfaces with different curvatures from top to bottom; on the axis. The invention realizes two-way water outlet through two water outlets, improves the outflow efficiency of the centrifugal pump, and at the same time enhances the velocity component of the water flow in the circumferential direction of the volute, improves the water flow conditions at the outlet of the volute, reduces hydraulic loss, and makes centrifugal The pump has good hydraulic performance and operating efficiency.

Figure 202010395156

Description

一种高比转速双出口式蜗壳离心泵A high specific speed double outlet volute centrifugal pump

技术领域technical field

本发明涉及一种高比转速双出口式蜗壳离心泵,属于离心泵技术领域。The invention relates to a high specific rotational speed double outlet volute centrifugal pump, belonging to the technical field of centrifugal pumps.

背景技术Background technique

离心泵的主要过流部件是叶轮和压水室,压水室因其外形呈逐渐扩散状,又被称为蜗壳。蜗壳是离心泵排出流体以及对流体增压的必要场所,因此其水力结构对离心泵的效率有着至关重要的影响。The main flow components of the centrifugal pump are the impeller and the pressurized water chamber. The pressurized water chamber is also known as the volute because of its gradual diffusion shape. The volute is the necessary place for the centrifugal pump to discharge the fluid and pressurize the fluid, so its hydraulic structure has a crucial influence on the efficiency of the centrifugal pump.

目前,人们对离心泵蜗壳的研究主要集中在断面的面积及形状、喉部面积以及隔舌安放角等方面,尚未对蜗壳的出口数做出改变并依此设计优化,提高泵效率。At present, people's research on the centrifugal pump volute mainly focuses on the area and shape of the section, the throat area and the angle of the separation tongue. The number of outlets of the volute has not been changed, and the design and optimization have been made to improve the pump efficiency.

因此,如何克服现有技术的不足已成为当今离心泵技术领域中亟待解决的重点难题之一。Therefore, how to overcome the deficiencies of the prior art has become one of the key problems to be solved urgently in the technical field of centrifugal pumps.

发明内容SUMMARY OF THE INVENTION

目的:为了克服现有技术中存在的不足,本发明提供一种高比转速双出口式蜗壳离心泵。Objective: In order to overcome the deficiencies in the prior art, the present invention provides a high specific speed double outlet volute centrifugal pump.

技术方案:为解决上述技术问题,本发明采用的技术方案为:Technical scheme: in order to solve the above-mentioned technical problems, the technical scheme adopted in the present invention is:

一种高比转速双出口式蜗壳离心泵,包括双出口式蜗壳,所述双出口式蜗壳内侧环形开口处设置有叶轮,叶轮底部连接有吸水管道,双出口式蜗壳的两个出水口均连接有出水管道;所述叶轮的叶片采用类圆柱形扭曲结构,叶片的正面与反面从上至下由不同曲率的曲面平滑连接;所述吸水管道、叶轮、双出口式蜗壳的中心在同一轴线上;所述叶片正面与反面从上至下的曲面的截面翼型曲线设置如下:A high specific speed double outlet volute centrifugal pump, comprising a double outlet volute, an impeller is arranged at the inner annular opening of the double outlet volute, a suction pipe is connected at the bottom of the impeller, and two double outlet volutes are provided. The water outlets are all connected with water outlet pipes; the blades of the impeller adopt a quasi-cylindrical twisted structure, and the front and back sides of the blades are smoothly connected by curved surfaces with different curvatures from top to bottom; The center is on the same axis; the cross-sectional airfoil curves of the front and back surfaces of the blade from top to bottom are set as follows:

距离叶轮顶部50mm处,叶片正面的曲面的截面翼型曲线公式如下:At 50mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows:

y=-0.72425x2+17.24068x+23.91072y=-0.72425x 2 +17.24068x+23.91072

叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows:

y=0.00683x3-0.95369x2+18.94882x+19.35635y=0.00683x 3 -0.95369x 2 +18.94882x+19.35635

距离叶轮顶部150mm处,叶片正面的曲面的截面翼型曲线公式如下:At 150mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface on the front of the blade is as follows:

y=-1.33765×10-7x4+4.63929×10-5x3-0.00788x2+0.55646x+112.20597y = -1.33765×10 -7 x 4 +4.63929×10 -5 x 3 -0.00788x 2 +0.55646x+112.20597

叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows:

y=-1.36421×10-7x4+4.8806×10-5x3-0.00847x2+0.60056x+106.91616y = -1.36421×10 -7 x 4 +4.8806×10 -5 x 3 -0.00847x 2 +0.60056x+106.91616

距离叶轮顶部250mm处,叶片正面的曲面的截面翼型曲线公式如下:At 250mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows:

y=-1.3079×10-7x4+4.53574×10-5x3-0.00779x2+0.5519x+112.99371y = -1.3079×10 -7 x 4 +4.53574×10 -5 x 3 -0.00779x 2 +0.5519x+112.99371

叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows:

y=-1.3285×10-7x4+4.75536×10-5x3-0.00835x2+0.59518x+107.68838y = -1.3285×10 -7 x 4 +4.75536×10 -5 x 3 -0.00835x 2 +0.59518x+107.68838

距离叶轮顶部350mm处,叶片正面的曲面的截面翼型曲线公式如下:At a distance of 350mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows:

y=-2.00056×10-6x4+5.66272×10-5x3-0.003x2+0.51281x+107.29902y=-2.00056×10 -6 x 4 +5.66272×10 -5 x 3 -0.003x 2 +0.51281x+107.29902

叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows:

y=-2.78571×10-6x4-1.36515×10-5x3-0.00192x2+0.54119x+112.37151y = -2.78571×10 -6 x 4 -1.36515×10 -5 x 3 -0.00192x 2 +0.54119x+112.37151

距离叶轮顶部450mm处,叶片正面的曲面的截面翼型曲线公式如下:At a distance of 450mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows:

y=0.14938x3+26.43681x2+1561.70207x+30844.31736y=0.14938x 3 +26.43681x 2 +1561.70207x+30844.31736

叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows:

y=0.00199x3+0.23735x2+10.55235x+244.36147。y= 0.00199x3 +0.23735x2 + 10.55235x+244.36147.

作为优选方案,所述叶片的进水边延伸至叶轮底部进口处。As a preferred solution, the water inlet edge of the blade extends to the inlet of the bottom of the impeller.

作为优选方案,所述双出口式蜗壳圆周方向共有两个出水口,两个出水口呈轴对称设置。As a preferred solution, there are two water outlets in the circumferential direction of the double outlet volute, and the two water outlets are axially symmetrical.

作为优选方案,所述叶轮采用铸造工艺一次成型。As a preferred solution, the impeller is formed at one time by a casting process.

作为优选方案,所述叶片数量为5-8个。As a preferred solution, the number of the blades is 5-8.

作为优选方案,所述叶片数量为6个。As a preferred solution, the number of the blades is 6.

作为优选方案,所述双出口式蜗壳的出水口截面为圆形断面。As a preferred solution, the water outlet section of the double outlet volute is a circular section.

有益效果:本发明提供的一种高比转速双出口式蜗壳离心泵,离心泵应用双出口式蜗壳,通过两个出水口实现双向出水,提高了离心泵出流效率,同时增强了水流在蜗壳圆周方向上的速度分量,改善了蜗壳出口处的水流条件,减小水力损失,使得离心泵具有良好的水力性能和运行效率。Beneficial effects: the present invention provides a high specific speed double outlet volute centrifugal pump, the centrifugal pump uses the double outlet volute, and realizes two-way water outlet through two water outlets, which improves the outflow efficiency of the centrifugal pump and enhances the water flow at the same time. The velocity component in the circumferential direction of the volute improves the water flow conditions at the outlet of the volute, reduces hydraulic loss, and enables the centrifugal pump to have good hydraulic performance and operating efficiency.

附图说明Description of drawings

图1是本发明提出的一种高比转速双出口式蜗壳离心泵的结构示意图。FIG. 1 is a schematic structural diagram of a high specific speed double outlet volute centrifugal pump proposed by the present invention.

图2是本发明提出的单个叶片正三轴视图。Figure 2 is a front triaxial view of a single blade proposed by the present invention.

图3是本发明提出的单个叶片俯视图。Figure 3 is a top view of a single blade proposed by the present invention.

图4是本发明提出的叶片上距叶轮顶部不同轴向距离处的翼型曲线示意图。FIG. 4 is a schematic diagram of the airfoil curves at different axial distances from the top of the impeller on the blade proposed by the present invention.

图5是本发明提出的叶轮正视图。Figure 5 is a front view of the impeller proposed by the present invention.

图6是本发明提出的叶轮中多个叶片组成结构示意图。FIG. 6 is a schematic diagram of the composition structure of a plurality of blades in the impeller proposed by the present invention.

具体实施方式Detailed ways

下面结合附图对本发明作更进一步的说明。The present invention will be further described below in conjunction with the accompanying drawings.

如图1所示,一种高比转速双出口式蜗壳离心泵,按水流方向依次包括吸水管道1、叶轮2、双出口式蜗壳3和出水管道4,所述双出口式蜗壳3内侧环形开口处设置有叶轮2,叶轮2底部连接有吸水管道1,双出口式蜗壳3的两个出水口均连接有出水管道4。As shown in Figure 1, a high specific rotational speed double outlet volute centrifugal pump includes a suction pipe 1, an impeller 2, a double outlet volute 3 and a water outlet pipe 4 in sequence according to the direction of water flow. The double outlet volute 3 The inner annular opening is provided with an impeller 2 , the bottom of the impeller 2 is connected with a water suction pipe 1 , and the two water outlets of the double outlet volute 3 are connected with a water outlet pipe 4 .

如图2-4所示,所述叶轮2的叶片采用类圆柱形扭曲结构,叶片201的正面与反面从上至下由不同曲率的曲面平滑连接,叶片201正面与反面从上至下的曲面的截面翼型曲线设置如下:As shown in Figures 2-4, the blades of the impeller 2 adopt a quasi-cylindrical twisted structure, the front and back surfaces of the blades 201 are smoothly connected from top to bottom by curved surfaces with different curvatures, and the front and back surfaces of the blades 201 are curved from top to bottom. The section airfoil curve is set as follows:

距离叶轮2顶部50mm处,叶片201正面与反面截面翼型曲线上的点坐标的数值参见表1。50mm from the top of the impeller 2, the values of the point coordinates on the airfoil curves of the front and back sections of the blade 201 are shown in Table 1.

表1Table 1

Figure BDA0002486153800000041
Figure BDA0002486153800000041

Figure BDA0002486153800000051
Figure BDA0002486153800000051

拟合的两条曲线分别表示为:The two fitted curves are expressed as:

叶片正面:Front of the leaf:

y=-0.72425x2+17.24068x+23.91072y=-0.72425x 2 +17.24068x+23.91072

叶片反面:The reverse side of the blade:

y=0.00683x3-0.95369x2+18.94882x+19.35635y=0.00683x 3 -0.95369x 2 +18.94882x+19.35635

距离叶轮2顶部150mm处,叶片201正面与反面截面翼型曲线上的点坐标的数值参见表2。150mm from the top of the impeller 2, the values of the point coordinates on the airfoil curves of the front and back sections of the blade 201 are shown in Table 2.

表2Table 2

Figure BDA0002486153800000052
Figure BDA0002486153800000052

Figure BDA0002486153800000061
Figure BDA0002486153800000061

拟合的两条曲线分别表示为:The two fitted curves are expressed as:

叶片正面:Front of the leaf:

y=-1.33765×10-7x4+4.63929×10-5x3-0.00788x2+0.55646x+112.20597y = -1.33765×10 -7 x 4 +4.63929×10 -5 x 3 -0.00788x 2 +0.55646x+112.20597

叶片反面:The reverse side of the blade:

y=-1.36421×10-7x4+4.8806×10-5x3-0.00847x2+0.60056x+106.91616y = -1.36421×10 -7 x 4 +4.8806×10 -5 x 3 -0.00847x 2 +0.60056x+106.91616

距离叶轮2顶部250mm处,叶片201正面与反面截面翼型曲线上的点坐标的数值参见表3。250mm from the top of the impeller 2, the values of the point coordinates on the airfoil curves of the front and back sections of the blade 201 are shown in Table 3.

表3table 3

Figure BDA0002486153800000062
Figure BDA0002486153800000062

Figure BDA0002486153800000071
Figure BDA0002486153800000071

拟合的两条曲线分别可表示为:The two fitted curves can be expressed as:

叶片正面:Front of the leaf:

y=-1.3079×10-7x4+4.53574×10-5x3-0.00779x2+0.5519x+112.99371y = -1.3079×10 -7 x 4 +4.53574×10 -5 x 3 -0.00779x 2 +0.5519x+112.99371

叶片反面:Back of the blade:

y=-1.3285×10-7x4+4.75536×10-5x3-0.00835x2+0.59518x+107.68838y = -1.3285×10 -7 x 4 +4.75536×10 -5 x 3 -0.00835x 2 +0.59518x+107.68838

距离叶轮2顶部350mm处,叶片201正面与反面截面翼型曲线上的点坐标的数值参见表4。350mm from the top of the impeller 2, the values of the point coordinates on the airfoil curves of the front and back sections of the blade 201 are shown in Table 4.

表4Table 4

Figure BDA0002486153800000072
Figure BDA0002486153800000072

Figure BDA0002486153800000081
Figure BDA0002486153800000081

拟合的两条曲线分别表示为:The two fitted curves are expressed as:

叶片正面:Front of the leaf:

y=-2.00056×10-6x4+5.66272×10-5x3-0.003x2+0.51281x+107.29902y=-2.00056×10 -6 x 4 +5.66272×10 -5 x 3 -0.003x 2 +0.51281x+107.29902

叶片反面:Back of the blade:

y=-2.78571×10-6x4-1.36515×10-5x3-0.00192x2+0.54119x+112.37151y = -2.78571×10 -6 x 4 -1.36515×10 -5 x 3 -0.00192x 2 +0.54119x+112.37151

距离叶轮2顶部450mm处,叶片201正面与反面截面翼型曲线上的点坐标的数值参见表5。450mm from the top of the impeller 2, the values of the point coordinates on the airfoil curves of the front and back sections of the blade 201 are shown in Table 5.

表5table 5

Figure BDA0002486153800000082
Figure BDA0002486153800000082

拟合的两条曲线分别表示为:The two fitted curves are expressed as:

叶片正面:Front of the leaf:

y=0.14938x3+26.43681x2+1561.70207x+30844.31736y=0.14938x 3 +26.43681x 2 +1561.70207x+30844.31736

叶片反面:Back of the blade:

y=0.00199x3+0.23735x2+10.55235x+244.36147y= 0.00199x3 +0.23735x2 + 10.55235x+244.36147

如图5-6所示,所述叶轮2的叶片数量为5-8个,叶片的进水边延伸至叶轮2底部进口处,以提高汽蚀性能。As shown in Figure 5-6, the number of blades of the impeller 2 is 5-8, and the water inlet edge of the blades extends to the bottom inlet of the impeller 2 to improve the cavitation performance.

所述吸水管道1、叶轮2、双出口式蜗壳3的中心在同一轴线上。The centers of the water suction pipe 1 , the impeller 2 and the double outlet volute 3 are on the same axis.

所述双出口式蜗壳3圆周方向共有两个出水口,两个出水口呈轴对称设置,所述叶轮采用铸造工艺一次成型。The double-outlet volute 3 has two water outlets in the circumferential direction, and the two water outlets are arranged axially symmetrically, and the impeller is formed by a casting process at one time.

实施例1:Example 1:

对某离心泵进行优化设计,泵的额定流量为367m3/h,扬程为25m,比转速为208。The optimized design of a centrifugal pump, the rated flow of the pump is 367m3/h, the head is 25m, and the specific speed is 208.

本发明优化参数为:叶轮底部进口处直径为1700mm,叶轮顶部出口处直径为4100mm,双出口式蜗壳外直径为4160mm。双出口式蜗壳的出水口截面为直径1700mm的圆形断面,直接连通出水管道。叶轮叶片数量为6,叶片采用类圆柱形等厚扭曲结构。The optimized parameters of the invention are as follows: the diameter of the inlet at the bottom of the impeller is 1700 mm, the diameter of the outlet at the top of the impeller is 4100 mm, and the outer diameter of the double outlet volute is 4160 mm. The water outlet section of the double outlet volute is a circular section with a diameter of 1700mm, which is directly connected to the water outlet pipe. The number of impeller blades is 6, and the blades adopt a quasi-cylindrical and equal-thickness twisted structure.

实施例2:Example 2:

本发明优化参数为:叶轮底部进口处直径为1700mm,叶轮顶部出口处直径为4100mm,双出口式蜗壳外直径为4160mm。双出口式蜗壳的出水口截面为直径1700mm的圆形断面,直接连通出水管道。叶轮叶片数量为8,叶片采用类圆柱形等厚扭曲结构。The optimized parameters of the invention are as follows: the diameter of the inlet at the bottom of the impeller is 1700 mm, the diameter of the outlet at the top of the impeller is 4100 mm, and the outer diameter of the double outlet volute is 4160 mm. The water outlet section of the double outlet volute is a circular section with a diameter of 1700mm, which is directly connected to the water outlet pipe. The number of impeller blades is 8, and the blades adopt a quasi-cylindrical and equal-thickness twisted structure.

实施例3:Example 3:

本发明的具体应用过程为:离心泵泵体和吸水管道1内先充满水,电机带动叶轮2旋转,叶轮中叶片间的水开始旋转,水从叶轮2中心被甩向叶轮外缘并以较高的压强从两个出水口排出。同时由于压差作用,叶轮2不停旋转,液体也不断的从吸水管道1进入并经双出口式蜗壳3从出水管道4流出。The specific application process of the present invention is as follows: the pump body of the centrifugal pump and the water suction pipe 1 are filled with water first, the motor drives the impeller 2 to rotate, the water between the blades in the impeller starts to rotate, and the water is thrown from the center of the impeller 2 to the outer edge of the impeller. High pressure is discharged from two water outlets. At the same time, due to the pressure difference, the impeller 2 keeps rotating, and the liquid also continuously enters from the suction pipe 1 and flows out from the water outlet pipe 4 through the double outlet volute 3.

本发明的具体实施方式中未涉及的说明属于本领域公知技术,可参考公知技术加以实施。The descriptions not involved in the specific embodiments of the present invention belong to the well-known technology in the art, and can be implemented with reference to the well-known technology.

以上所述仅是本发明的优选实施方式,应当指出:对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only the preferred embodiment of the present invention, it should be pointed out that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can also be made, and these improvements and modifications are also It should be regarded as the protection scope of the present invention.

Claims (7)

1.一种高比转速双出口式蜗壳离心泵,其特征在于:包括双出口式蜗壳,所述双出口式蜗壳内侧环形开口处设置有叶轮,叶轮底部连接有吸水管道,双出口式蜗壳的两个出水口均连接有出水管道;所述叶轮的叶片采用类圆柱形扭曲结构,叶片的正面与反面从上至下由不同曲率的曲面平滑连接;所述吸水管道、叶轮、双出口式蜗壳的中心在同一轴线上;所述叶片正面与反面从上至下的曲面的截面翼型曲线设置如下:1. a high specific rotating speed double outlet volute centrifugal pump, is characterized in that: comprise double outlet volute, described double outlet volute inner annular opening is provided with impeller, and the bottom of impeller is connected with suction pipe, and the double outlet is provided with an impeller. The two water outlets of the volute are connected with water outlet pipes; the blades of the impeller adopt a quasi-cylindrical twisted structure, and the front and back sides of the blades are smoothly connected from top to bottom by curved surfaces with different curvatures; the water suction pipes, impeller, The center of the double outlet volute is on the same axis; the cross-sectional airfoil curves of the front and back surfaces of the blades from top to bottom are set as follows: 距离叶轮顶部50mm处,叶片正面的曲面的截面翼型曲线公式如下:At 50mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows: y=-0.72425x2+17.24068x+23.91072y=-0.72425x 2 +17.24068x+23.91072 叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows: y=0.00683x3-0.95369x2+18.94882x+19.35635y=0.00683x 3 -0.95369x 2 +18.94882x+19.35635 距离叶轮顶部150mm处,叶片正面的曲面的截面翼型曲线公式如下:At 150mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface on the front of the blade is as follows: y=-1.33765×10-7x4+4.63929×10-5x3-0.00788x2+0.55646x+112.20597y = -1.33765×10 -7 x 4 +4.63929×10 -5 x 3 -0.00788x 2 +0.55646x+112.20597 叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows: y=-1.36421×10-7x4+4.8806×10-5x3-0.00847x2+0.60056x+106.91616y = -1.36421×10 -7 x 4 +4.8806×10 -5 x 3 -0.00847x 2 +0.60056x+106.91616 距离叶轮顶部250mm处,叶片正面的曲面的截面翼型曲线公式如下:At 250mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows: y=-1.3079×10-7x4+4.53574×10-5x3-0.00779x2+0.5519x+112.99371y = -1.3079×10 -7 x 4 +4.53574×10 -5 x 3 -0.00779x 2 +0.5519x+112.99371 叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows: y=-1.3285×10-7x4+4.75536×10-5x3-0.00835x2+0.59518x+107.68838y = -1.3285×10 -7 x 4 +4.75536×10 -5 x 3 -0.00835x 2 +0.59518x+107.68838 距离叶轮顶部350mm处,叶片正面的曲面的截面翼型曲线公式如下:At a distance of 350mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows: y=-2.00056×10-6x4+5.66272×10-5x3-0.003x2+0.51281x+107.29902y=-2.00056×10 -6 x 4 +5.66272×10 -5 x 3 -0.003x 2 +0.51281x+107.29902 叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows: y=-2.78571×10-6x4-1.36515×10-5x3-0.00192x2+0.54119x+112.37151y = -2.78571×10 -6 x 4 -1.36515×10 -5 x 3 -0.00192x 2 +0.54119x+112.37151 距离叶轮顶部450mm处,叶片正面的曲面的截面翼型曲线公式如下:At a distance of 450mm from the top of the impeller, the cross-sectional airfoil curve formula of the curved surface of the blade front is as follows: y=0.14938x3+26.43681x2+1561.70207x+30844.31736y=0.14938x 3 +26.43681x 2 +1561.70207x+30844.31736 叶片反面的曲面的截面翼型曲线公式如下:The cross-sectional airfoil curve formula of the curved surface on the opposite side of the blade is as follows: y=0.00199x3+0.23735x2+10.55235x+244.36147。y= 0.00199x3 +0.23735x2 + 10.55235x+244.36147. 2.根据权利要求1所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述叶片的进水边延伸至叶轮底部进口处。2 . The high specific rotational speed double outlet volute centrifugal pump according to claim 1 , wherein the water inlet edge of the blade extends to the inlet of the bottom of the impeller. 3 . 3.根据权利要求1所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述双出口式蜗壳圆周方向共有两个出水口,两个出水口呈轴对称设置。3 . The high specific rotational speed double outlet volute centrifugal pump according to claim 1 , wherein: the double outlet volute has two water outlets in the circumferential direction, and the two water outlets are axially symmetrical. 4 . 4.根据权利要求1所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述叶轮采用铸造工艺一次成型。4 . The high specific rotational speed double outlet volute casing centrifugal pump according to claim 1 , wherein the impeller is formed at one time by a casting process. 5 . 5.根据权利要求1所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述叶片数量为5-8个。5 . The high specific speed double outlet volute centrifugal pump according to claim 1 , wherein the number of the blades is 5-8. 6 . 6.根据权利要求5所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述叶片数量为6个。6 . The high specific rotational speed double outlet volute centrifugal pump according to claim 5 , wherein the number of the blades is 6. 7 . 7.根据权利要求1所述的一种高比转速双出口式蜗壳离心泵,其特征在于:所述双出口式蜗壳的出水口截面为圆形断面。7 . The high specific rotational speed double outlet volute centrifugal pump according to claim 1 , wherein the cross section of the water outlet of the double outlet volute is a circular section. 8 .
CN202010395156.XA 2020-05-11 2020-05-11 High-specific-speed double-outlet volute centrifugal pump Pending CN111536077A (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6082000A (en) * 1997-03-14 2000-07-04 Dab Pumps S.P.A. Method for producing an impeller for turbine pumps provided with vanes having an improved profile
CN101881282A (en) * 2009-05-08 2010-11-10 通用汽车环球科技运作公司 Centrifugal fluid pump
CN104776050A (en) * 2015-03-25 2015-07-15 中国计量学院 Impeller and volute chamber guide device in double-suction centrifugal pump
CN107503978A (en) * 2017-09-19 2017-12-22 河海大学 A kind of high-lift higher specific speed mixed-flow pump
CN108626130A (en) * 2018-03-01 2018-10-09 江苏大学 A kind of high-temperature melting salt pump of the double outlet double volute pump bodies of band
CN209959477U (en) * 2019-04-23 2020-01-17 大连耐酸泵技术开发公司 High-temperature-resistant double-outlet type single-stage submerged pump

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6082000A (en) * 1997-03-14 2000-07-04 Dab Pumps S.P.A. Method for producing an impeller for turbine pumps provided with vanes having an improved profile
CN101881282A (en) * 2009-05-08 2010-11-10 通用汽车环球科技运作公司 Centrifugal fluid pump
CN104776050A (en) * 2015-03-25 2015-07-15 中国计量学院 Impeller and volute chamber guide device in double-suction centrifugal pump
CN107503978A (en) * 2017-09-19 2017-12-22 河海大学 A kind of high-lift higher specific speed mixed-flow pump
CN108626130A (en) * 2018-03-01 2018-10-09 江苏大学 A kind of high-temperature melting salt pump of the double outlet double volute pump bodies of band
CN209959477U (en) * 2019-04-23 2020-01-17 大连耐酸泵技术开发公司 High-temperature-resistant double-outlet type single-stage submerged pump

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
离心式与轴流式水泵编写组: "《离心式与轴流式水泵》", 30 September 1980 *

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