[go: up one dir, main page]

CN105909567B - A kind of ejector improving jet-type centrifugal pump cavitation performance - Google Patents

A kind of ejector improving jet-type centrifugal pump cavitation performance Download PDF

Info

Publication number
CN105909567B
CN105909567B CN201610431975.9A CN201610431975A CN105909567B CN 105909567 B CN105909567 B CN 105909567B CN 201610431975 A CN201610431975 A CN 201610431975A CN 105909567 B CN105909567 B CN 105909567B
Authority
CN
China
Prior art keywords
throat
ejector
nozzle
inlet
jet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201610431975.9A
Other languages
Chinese (zh)
Other versions
CN105909567A (en
Inventor
李贵东
王洋
赵立峰
冒杰云
曹璞钰
胡日新
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangsu University
Original Assignee
Jiangsu University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jiangsu University filed Critical Jiangsu University
Priority to CN201610431975.9A priority Critical patent/CN105909567B/en
Publication of CN105909567A publication Critical patent/CN105909567A/en
Application granted granted Critical
Publication of CN105909567B publication Critical patent/CN105909567B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/02Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid
    • F04F5/10Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid displacing liquids, e.g. containing solids, or liquids and elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D9/00Priming; Preventing vapour lock
    • F04D9/04Priming; Preventing vapour lock using priming pumps; using booster pumps to prevent vapour-lock
    • F04D9/06Priming; Preventing vapour lock using priming pumps; using booster pumps to prevent vapour-lock of jet type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

本发明涉及一种改善射流式离心泵空化性能的射流器,包括喷嘴、引流段、混合段、喉管、扩散段和增压孔。当射流式离心泵在大流量工况运行时,在射流器喉管部位设计增压孔,增压孔将泵腔内的高压液体引入喉管低压区域,增加喉管低压区域的压力,抑制射流器喉管内部发生空化诱发振动、噪声,改善射流器喉管内部发生空化而导致射流式离心泵扬程急剧下降现象,将扬程折断点向大流量偏移,增加射流式离心泵的运行范围。

The invention relates to an ejector for improving the cavitation performance of a jet centrifugal pump, which comprises a nozzle, a drainage section, a mixing section, a throat, a diffusion section and a booster hole. When the jet-type centrifugal pump is operating under high-flow conditions, a booster hole is designed at the throat of the ejector. The booster hole introduces the high-pressure liquid in the pump chamber into the low-pressure area of the throat, increases the pressure in the low-pressure area of the throat, and suppresses the jet flow. Vibration and noise induced by cavitation inside the throat of the ejector can improve the phenomenon that the head of the jet centrifugal pump drops sharply due to cavitation inside the throat of the ejector, shift the breaking point of the lift to the large flow rate, and increase the operating range of the jet centrifugal pump .

Description

一种改善射流式离心泵空化性能的射流器An Ejector for Improving the Cavitation Performance of a Jet Centrifugal Pump

技术领域technical field

本发明涉及一种射流式离心泵的主要部件射流器,特别涉及到一种能改善射流式离心泵空化性能的射流器。The invention relates to an ejector which is the main part of a jet-type centrifugal pump, in particular to an ejector which can improve the cavitation performance of the jet-type centrifugal pump.

背景技术Background technique

射流式离心泵是一种采用射流器与离心泵组合方式设计的电泵,其具有结构紧凑、操作方便、二次启动无需灌水、无需安装底阀、可实现自吸等优点,在园林滴灌、农业喷灌等节水系统中应用广泛。同传统离心泵相比,射流式离心泵的运行原理:从泵导叶出流进入泵腔的高压液体通过喷嘴射流在混合段形成局部真空,使泵进水管路内的液体在大气压作用下通过引流段进入射流器的混合段,进而与喷嘴射流出的液体混合,共同经喉管、扩散段流入离心叶轮并从导叶排出,其中,一部分液体排出泵腔,另一部分液体则通过射流器进口继续与进口管内液体混合流入叶轮,如此循环运行。基于射流式离心泵工作原理的特殊性,根据研究发现,在运行过程中,射流式离心泵内部压力最低位置产生在喉管区域,这就决定了该类泵的空化不会发生在叶轮进口处,而是发生在射流器喉管某一位置。随着流量的增加,射流器喉管内部将发生空化而导致射流式离心泵扬程急剧下降,同时诱发振动与噪声,限制了其流量运行范围。The jet-type centrifugal pump is an electric pump designed in combination with a jet and a centrifugal pump. It has the advantages of compact structure, convenient operation, no need for irrigation for the second start, no need to install a bottom valve, and self-priming. It is used in garden drip irrigation, It is widely used in water-saving systems such as agricultural sprinkler irrigation. Compared with traditional centrifugal pumps, jet centrifugal pumps operate on the principle that the high-pressure liquid flowing from the pump guide vanes into the pump cavity forms a partial vacuum in the mixing section through the nozzle jet, so that the liquid in the pump inlet pipe passes through the pump under the action of atmospheric pressure. The drainage section enters the mixing section of the ejector, and then mixes with the liquid ejected from the nozzle, and flows into the centrifugal impeller through the throat and the diffuser section, and is discharged from the guide vane. Part of the liquid is discharged from the pump chamber, and the other part passes through the inlet of the ejector. Continue to mix with the liquid in the inlet pipe and flow into the impeller, so the cycle runs. Based on the particularity of the working principle of the jet centrifugal pump, according to the research, it is found that during the operation, the lowest internal pressure of the jet centrifugal pump is generated in the throat area, which determines that the cavitation of this type of pump will not occur at the impeller inlet Instead, it occurs somewhere in the throat of the ejector. As the flow rate increases, cavitation will occur inside the throat of the ejector, which will lead to a sharp drop in the head of the jet centrifugal pump, and at the same time induce vibration and noise, limiting its flow operating range.

因此,设计一种在大流量运行过程中,通过将泵腔内的高压液体引入射流器喉部区域,用以增加该区域的压力,进而改善射流式离心泵空化性能的射流器至关重要。Therefore, it is very important to design an ejector that improves the cavitation performance of a jet centrifugal pump by introducing the high-pressure liquid in the pump chamber into the throat area of the ejector to increase the pressure in this area during the operation of large flow .

发明内容Contents of the invention

本发明的目的在于提供一种改善射流式离心泵空化性能的射流器,包括喷嘴、引流段、混合段、喉管、扩散段和增压孔。在射流器喉管部位开设一定数量的增压孔,将泵腔内的高压液体引入射流器喉管低压区域,用以增加该区域的压力,抑制射流器喉管内部发生空化诱发振动、噪声,改善射流器喉管内部发生空化而导致射流式离心泵扬程急剧下降现象,将扬程折断点向大流量偏移,增加射流式离心泵的流量运行范围。The object of the present invention is to provide an ejector for improving the cavitation performance of a jet-type centrifugal pump, which includes a nozzle, a drainage section, a mixing section, a throat, a diffusing section and a booster hole. A certain number of booster holes are set in the throat of the ejector to introduce the high-pressure liquid in the pump chamber into the low-pressure area of the throat of the ejector to increase the pressure in this area and suppress the cavitation-induced vibration and noise inside the throat of the ejector , to improve the sharp drop in the head of the jet centrifugal pump caused by cavitation inside the throat of the ejector, shift the breaking point of the lift to the high flow rate, and increase the flow operating range of the jet centrifugal pump.

为实现上述目的,本发明采用如下方案:To achieve the above object, the present invention adopts the following scheme:

首先根据设计要求,确定喷嘴直径First, determine the nozzle diameter according to the design requirements

式中:Q1为喷嘴喷射流量,其中,喷嘴喷射流量Q1等于离心叶轮进口流量Q0减去泵进口流量Q2,离心叶轮进口流量Q0和泵进口流量Q2可根据射流式离心泵设计要求得出;In the formula: Q 1 is the injection flow rate of the nozzle, among which, the injection flow rate Q 1 of the nozzle is equal to the inlet flow rate Q 0 of the centrifugal impeller minus the inlet flow rate Q 2 of the pump . According to the design requirements;

μ为固体颗粒与液体速度滑移修正系数,在清水介质中,其数值为1;μ is the correction coefficient of the velocity slip between solid particles and liquid, and its value is 1 in the clear water medium;

α为射流器喉管进口函数,经验值取1~1.05;α is the inlet function of the ejector throat, and the empirical value is 1~1.05;

Δp0为喷嘴进口与引流段进口处的压力差,引流段进口处压力可近似为泵进口处压力;Δp 0 is the pressure difference between the inlet of the nozzle and the inlet of the drainage section, and the pressure at the inlet of the drainage section can be approximated as the pressure at the inlet of the pump;

γ为液体的容重。γ is the bulk density of the liquid.

进而确定:And then determine:

喉管直径:其中,面积比R表示喉管面积与喷嘴面积的比值,其值与流量比M相关,流量比M表示离心叶轮进口流量Q0与喷嘴喷射流量Q1的比值;Throat diameter: Among them, the area ratio R represents the ratio of the throat area to the nozzle area, and its value is related to the flow ratio M, and the flow ratio M represents the ratio of the centrifugal impeller inlet flow Q0 to the nozzle injection flow Q1 ;

喷嘴圆柱出口长度:L1=(0.3~0.5)D1Nozzle cylindrical outlet length: L 1 = (0.3~0.5) D 1 ;

喉嘴距:L2=(0.5~1)D2,喉嘴距为混合段的长度,即喷嘴出口到喉管进口的距离;Throat-mouth distance: L 2 = (0.5~1)D 2 , the throat-mouth distance is the length of the mixing section, that is, the distance from the outlet of the nozzle to the inlet of the throat;

喉管长度:L3=(1.5~3)D2Throat length: L 3 =(1.5~3)D 2 ;

扩散段长度:L4=(2~5)D2,其中,L4由扩散角β确定,β取5°~8°。The length of the diffusion section: L 4 =(2~5)D 2 , wherein, L 4 is determined by the diffusion angle β, and β is 5°~8°.

上述方案中,增压孔到喉管进口距离L0与喉管长度L3的比值为1/6~1/2。In the above scheme, the ratio of the distance L 0 from the booster hole to the inlet of the throat to the length L 3 of the throat is 1/6˜1/2.

上述方案中,增压孔内液体的出流方向应以能够尽量减小与喉管来流冲击损失为宜,即增压孔与喉管壁面夹角的方向为θ,30°≤θ≤90°。In the above scheme, the outflow direction of the liquid in the booster hole should minimize the impact loss with the incoming flow of the throat, that is, the direction of the angle between the booster hole and the wall of the throat is θ, and 30°≤θ≤90 °.

上述方案中,增压孔直径D0与喉管直径D2的比值为1/20~1/12。In the above solution, the ratio of the diameter D 0 of the pressurizing hole to the diameter D 2 of the throat is 1/20˜1/12.

上述方案中,增压孔数目2≤N≤4,且圆周方向均匀分布。In the above solution, the number of pressurization holes is 2≤N≤4, and the number is evenly distributed in the circumferential direction.

本发明的有益效果是:The beneficial effects of the present invention are:

采用这种结构的射流器,能有效改善在大流量工况运行时,射流器喉管内部发生空化诱发的振动与噪声;改善大流量工况运行时,射流器喉管内部发生空化而导致扬程急剧下降问题,将扬程折断点向大流量偏移,增大射流式离心泵的运行范围。The ejector with this structure can effectively improve the vibration and noise induced by cavitation inside the throat of the ejector when operating under high flow conditions; This leads to the problem of a sharp drop in the head, shifting the breaking point of the head to a large flow rate, and increasing the operating range of the jet centrifugal pump.

附图说明Description of drawings

图1为现有两种不同射流器结构的射流式离心泵示意图,图(a)为射流器呈直管状的射流式离心泵,图(b)为射流器带弯管的射流式离心泵;Fig. 1 is the schematic diagram of the jet type centrifugal pump of existing two kinds of different ejector structures, and figure (a) is the jet type centrifugal pump that ejector is straight pipe shape, and figure (b) is the jet type centrifugal pump with ejector band elbow;

图2为现有两种不同结构的射流器示意图,图(a)为呈直管状的射流器,图(b)为带弯管的射流器;Fig. 2 is the jet device schematic diagram of existing two kinds of different structures, and figure (a) is the jet device that is straight pipe shape, and figure (b) is the jet device with bent pipe;

图3为本发明所述两种不同结构的射流器示意图,图(a)为呈直管状的射流器,图(b)为图(a)中F-F向截面的示意图,图(c)为带弯管的射流器,图(d)为图(c)中F-F向截面的示意图;Fig. 3 is the injector schematic diagram of two kinds of different structures described in the present invention, and figure (a) is the injector that is straight pipe shape, and figure (b) is the schematic diagram of F-F direction cross-section in figure (a), and figure (c) is belt The ejector of elbow, figure (d) is the schematic diagram of F-F to section in figure (c);

图4为本发明所述两种不同结构的射流器内部流动情况示意图。Fig. 4 is a schematic diagram of the internal flow of the ejector with two different structures according to the present invention.

附图标记说明:Explanation of reference signs:

1-进口管路、2-射流器、21-喷嘴、22-引流段、23-混合段、24-喉管、25-扩散段、26-增压孔、3-离心叶轮、4-导叶、5-泵腔、6-出口管路、7-电机。1-inlet pipeline, 2-jet, 21-nozzle, 22-drainage section, 23-mixing section, 24-throat, 25-diffusion section, 26-boosting hole, 3-centrifugal impeller, 4-guide vane , 5-pump cavity, 6-outlet pipeline, 7-motor.

具体实施方式Detailed ways

图3所示为本发明所述一种能改善射流式离心泵空化性能的射流器2的结构示意图,所述射流式离心泵的射流器2,包括喷嘴21、引流段22、混合段23、喉管24、扩散段25和增压孔26。Fig. 3 is a schematic structural view of an ejector 2 that can improve the cavitation performance of a jet-type centrifugal pump according to the present invention. The ejector 2 of the jet-type centrifugal pump includes a nozzle 21, a drainage section 22, and a mixing section 23 , Throat 24, diffuser section 25 and booster hole 26.

如图2所示,当射流式离心泵在大流量工况运行时,射流器喉管内部将发生空化而导致泵扬程急剧下降,同时诱发振动噪声。如图4所示,当在射流器2喉管24部位设计增压孔26后,增压孔26将泵腔5内的高压液体引入喉管24低压区域,增加喉管24低压区域的压力,改善射流式离心泵射流器2的抗空化性能。达到设计预期效果。As shown in Figure 2, when the jet centrifugal pump operates under the condition of large flow, cavitation will occur inside the throat of the jet, which will cause the pump head to drop sharply and induce vibration and noise at the same time. As shown in Figure 4, after the pressure boosting hole 26 is designed at the throat 24 of the ejector 2, the pressure boosting hole 26 will introduce the high-pressure liquid in the pump chamber 5 into the low-pressure area of the throat 24, increasing the pressure in the low-pressure area of the throat 24, To improve the anti-cavitation performance of the injector 2 of the jet centrifugal pump. achieve the desired effect of the design.

如图3所示,增压孔26与喉管24壁面夹角θ为30°≤θ≤90°,较佳地,射流器2的喉管24长度L3较长时,增压孔26与喉管24壁面夹角θ为30°≤θ≤60°。增压孔26到喉管24进口距离L0与喉管24长度L3的比值为1/6~1/2。增压孔26直径D0与喉管24直径D2的比值为1/20~1/12。增压孔26数目为2≤N≤4,且圆周方向均匀分布。As shown in Figure 3, the included angle θ between the pressurization hole 26 and the wall of the throat pipe 24 is 30°≤θ≤90°. Preferably, when the length L3 of the throat pipe 24 of the ejector 2 is longer, the pressure increase hole 26 and The angle θ between the walls of the throat pipe 24 is 30°≤θ≤60°. The ratio of the distance L 0 from the booster hole 26 to the inlet of the throat 24 to the length L 3 of the throat 24 is 1/6˜1/2. The ratio of the diameter D 0 of the pressurizing hole 26 to the diameter D 2 of the throat 24 is 1/20˜1/12. The number of booster holes 26 is 2≤N≤4, and the number is evenly distributed in the circumferential direction.

最后应说明的是:以上实施例仅用以说明本发明的技术方案,而非对其限制;其中用于提高喉管低压区域液流压力的增压孔是本方案中不可缺少的部分,但并不对其进行限制,只要能够对所述射流器通过增压孔将泵腔内的高压液体引入喉管低压区域从而起到改善空化性能的方案都在本发明的保护之列。尽管参照前述各实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解;其依然可以对前述实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。Finally, it should be noted that the above examples are only used to illustrate the technical solutions of the present invention, rather than to limit them; wherein the booster hole for increasing the liquid flow pressure in the low-pressure area of the throat is an indispensable part of the solution, but It is not limited thereto, as long as the ejector can introduce the high-pressure liquid in the pump cavity into the low-pressure area of the throat through the booster hole, so as to improve the cavitation performance, all schemes are included in the protection of the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features; and these The modification or replacement does not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the various embodiments of the present invention.

Claims (3)

1.一种改善射流式离心泵空化性能的射流器,其特征在于,包括喷嘴(21)、引流段(22)、混合段(23)、喉管(24)、扩散段(25)和增压孔(26),所述增压孔(26)设置于射流器(2)的喉管(24)部位,所述增压孔(26)到喉管进口距离L0与喉管长度L3的比值为1/6~1/2,增压孔(26)与喉管(24)壁面夹角的方向为θ,30°≤θ≤90°;1. An ejector for improving the cavitation performance of a jet-type centrifugal pump is characterized in that it comprises a nozzle (21), a drainage section (22), a mixing section (23), a throat (24), a diffuser section (25) and A booster hole (26), the booster hole (26) is arranged at the throat (24) of the ejector (2), and the distance from the booster hole (26) to the inlet of the throat is L0 and the length of the throat is L The ratio of 3 is 1/6~1/2, and the direction of the included angle between the booster hole (26) and the wall surface of the throat pipe (24) is θ, 30°≤θ≤90°; 所述增压孔(26)的直径D0与喉管(24)的直径D2的比值为1/20~1/12;The ratio of the diameter D0 of the pressurizing hole (26) to the diameter D2 of the throat (24) is 1/20-1/12; 所述喷嘴(21)的直径为D1 The diameter of the nozzle (21) is D 1 , 式中:In the formula: Q1为喷嘴喷射流量,其中,喷嘴喷射流量Q1等于离心叶轮进口流量Q0减去泵进口流量Q2,离心叶轮进口流量Q0和泵进口流量Q2可根据射流式离心泵设计要求得出;Q 1 is the injection flow rate of the nozzle, among which, the injection flow rate Q 1 of the nozzle is equal to the inlet flow rate Q 0 of the centrifugal impeller minus the inlet flow rate Q 2 of the pump. out; μ为固体颗粒与液体速度滑移修正系数,在清水介质中,其数值为1;μ is the correction coefficient of the velocity slip between solid particles and liquid, and its value is 1 in the clear water medium; α为射流器喉管进口函数,经验值取1~1.05;α is the inlet function of the ejector throat, and the empirical value is 1~1.05; Δp0为喷嘴进口与引流段进口处的压力差,引流段进口处压力可近似为泵进口处压力;Δp 0 is the pressure difference between the inlet of the nozzle and the inlet of the drainage section, and the pressure at the inlet of the drainage section can be approximated as the pressure at the inlet of the pump; γ为液体的容重;γ is the bulk density of the liquid; 所述喉管(24)的直径为D2 The diameter of the throat (24) is D 2 : 其中,面积比R表示喉管面积与喷嘴面积的比值,其值与流量比M相关,流量比M表示离心叶轮进口流量Q0与喷嘴喷射流量Q1的比值;Among them, the area ratio R represents the ratio of the throat area to the nozzle area, and its value is related to the flow ratio M, and the flow ratio M represents the ratio of the centrifugal impeller inlet flow Q0 to the nozzle injection flow Q1 ; 喷嘴(21)的圆柱出口长度为L1:L1=(0.3~0.5)D1The cylindrical outlet length of the nozzle (21) is L 1 : L 1 =(0.3-0.5)D 1 . 2.根据权利要求1所述的一种改善射流式离心泵空化性能的射流器,其特征在于:所述增压孔(26)的数目为N,2≤N≤4,且圆周方向均匀分布。2. An ejector for improving the cavitation performance of a jet-type centrifugal pump according to claim 1, characterized in that: the number of the booster holes (26) is N, 2≤N≤4, and the circumferential direction is uniform distributed. 3.根据权利要求1所述的一种改善射流式离心泵空化性能的射流器,其特征在于:所述混合段(23)的长度为喉嘴距,喉嘴距L2=(0.5~1)D2,即喷嘴出口到喉管进口的距离;3. An ejector for improving the cavitation performance of a jet-type centrifugal pump according to claim 1, characterized in that: the length of the mixing section (23) is the throat-mouth distance, and the throat-mouth distance L 2 =(0.5~ 1) D 2 , that is, the distance from the outlet of the nozzle to the inlet of the throat; 喉管(24)的长度为L3:L3=(1.5~3)D2The length of the throat (24) is L 3 : L 3 =(1.5~3)D 2 ; 扩散段(25)的长度为L4:L4=(2~5)D2,其中,L4由扩散角β确定,β取5°~8°。The length of the diffusion section (25) is L 4 : L 4 =(2-5)D 2 , where L 4 is determined by the diffusion angle β, and β is 5°-8°.
CN201610431975.9A 2016-06-15 2016-06-15 A kind of ejector improving jet-type centrifugal pump cavitation performance Active CN105909567B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610431975.9A CN105909567B (en) 2016-06-15 2016-06-15 A kind of ejector improving jet-type centrifugal pump cavitation performance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610431975.9A CN105909567B (en) 2016-06-15 2016-06-15 A kind of ejector improving jet-type centrifugal pump cavitation performance

Publications (2)

Publication Number Publication Date
CN105909567A CN105909567A (en) 2016-08-31
CN105909567B true CN105909567B (en) 2018-08-21

Family

ID=56751266

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610431975.9A Active CN105909567B (en) 2016-06-15 2016-06-15 A kind of ejector improving jet-type centrifugal pump cavitation performance

Country Status (1)

Country Link
CN (1) CN105909567B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106224302A (en) * 2016-09-12 2016-12-14 武汉大学 A kind of jet pump with scroll casing type flume
CN106438512A (en) * 2016-11-08 2017-02-22 四川大学 Ring-symmetry air supplementing device and method for reducing cavitation of liquid jet pump
CN106837805B (en) * 2017-03-31 2023-06-16 武汉武泵泵业制造有限公司 Centrifugal pulse jet pump
CN106837822B (en) * 2017-03-31 2023-07-28 武汉武泵泵业制造有限公司 Pulse jet vacuum pump with horizontal water outlet
CN107269544A (en) * 2017-08-16 2017-10-20 利欧集团浙江泵业有限公司 A kind of jet pump
CN109967429A (en) * 2019-03-30 2019-07-05 山东大学 An integrated device for heating, disinfection and cleaning of medical instruments
CN110469542A (en) * 2019-08-16 2019-11-19 中国航发北京航科发动机控制系统科技有限公司 A kind of fuel inlet device improving centrifugal pump suction capacity
CN110439866A (en) * 2019-09-07 2019-11-12 浙江日井泵业股份有限公司 A kind of low noise jet pump
CN110685964B (en) * 2019-11-13 2021-01-05 四川大学 Jet pump capable of automatically and uniformly supplementing air and reducing corrosion
CN111075772B (en) * 2019-12-23 2022-02-11 北京中煤矿山工程有限公司 Reverse circulation jet pump for residual drilling fluid in ground pre-grouting flowback stratum
CN115387760B (en) * 2021-05-25 2024-05-17 中国石油化工股份有限公司 Jet swirling device, self-circulation jet swirling drainage gas production system and method
CN114471362B (en) * 2022-01-29 2023-01-10 武汉大学 A jet type supercavitation generation system and supercavitation generation method
CN115199594A (en) * 2022-07-14 2022-10-18 兰州理工大学 A jet self-priming pump

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1204819A1 (en) * 1984-07-16 1986-01-15 Институт ядерной энергетики АН БССР Pumping unit
US6042089A (en) * 1996-07-01 2000-03-28 Klein; Christophe Foam generating device
CN201045359Y (en) * 2007-05-28 2008-04-09 武汉大学 A Liquid Jet Pump with Reduced Vibration and Noise
CN102146813A (en) * 2011-03-16 2011-08-10 李树生 Waste steam heating, pressurizing and recycling system
CN205744629U (en) * 2016-06-15 2016-11-30 江苏大学 A kind of ejector improving jet-type centrifugal pump cavitation performance

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100564893C (en) * 2006-12-27 2009-12-02 武汉大学 A kind of device that improves liquid flow pump cavitation property

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1204819A1 (en) * 1984-07-16 1986-01-15 Институт ядерной энергетики АН БССР Pumping unit
US6042089A (en) * 1996-07-01 2000-03-28 Klein; Christophe Foam generating device
CN201045359Y (en) * 2007-05-28 2008-04-09 武汉大学 A Liquid Jet Pump with Reduced Vibration and Noise
CN102146813A (en) * 2011-03-16 2011-08-10 李树生 Waste steam heating, pressurizing and recycling system
CN205744629U (en) * 2016-06-15 2016-11-30 江苏大学 A kind of ejector improving jet-type centrifugal pump cavitation performance

Also Published As

Publication number Publication date
CN105909567A (en) 2016-08-31

Similar Documents

Publication Publication Date Title
CN105909567B (en) A kind of ejector improving jet-type centrifugal pump cavitation performance
CN205744629U (en) A kind of ejector improving jet-type centrifugal pump cavitation performance
EP2635816B1 (en) Ejector and method
CN103047199A (en) Air jet pump
SA519402315B1 (en) Ejector Device
CN104533846A (en) High pressure annular jet pump suitable for pumping pressure type supply system
CN105650025A (en) Centrifugal pump impeller
CN113007100A (en) Adjustable jet type self-priming centrifugal pump
CN106224302A (en) A kind of jet pump with scroll casing type flume
CN210919593U (en) Jet pump capable of automatically and uniformly supplementing air and reducing corrosion
KR102271838B1 (en) Turbo Type Pump for Impeller Cavitation Reduction
CN101581312A (en) Mass-flow self-sucking pump
CN204553358U (en) A kind of high pressure annular jet pump being applicable to turbopump-feed system
CN110685964A (en) A Jet Pump for Automatic and Uniform Air Supplementation and Corrosion Reduction
CN207598589U (en) Inhibit the centrifugal pump device of impeller blade cavitation
CN105937507A (en) Guide vane for improving self-priming performance of jet-type centrifugal pump
CN100451343C (en) Big-flow self-priming centrifugal pump
CN205478553U (en) Take supercharging hole's afterburning centrifugal pump
US3185107A (en) Vortex jet pump
CN102927060B (en) A kind of suction port improving cavitation performance of centrifugal pump
CN115199594A (en) A jet self-priming pump
CN114962356A (en) Multi-stage energized jet pump
CN114151388A (en) Air pumping system based on miniature pulse jet vacuum pump
CN206874573U (en) A kind of new three-level jet pump
CN112392769A (en) Reduce hydraulic loss's vertical tubing pump body

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant