CN207830207U - A kind of centrifugal pump impeller - Google Patents

A kind of centrifugal pump impeller Download PDF

Info

Publication number
CN207830207U
CN207830207U CN201721880342.2U CN201721880342U CN207830207U CN 207830207 U CN207830207 U CN 207830207U CN 201721880342 U CN201721880342 U CN 201721880342U CN 207830207 U CN207830207 U CN 207830207U
Authority
CN
China
Prior art keywords
spoiler
blade
centrifugal pump
back shroud
thickness
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
CN201721880342.2U
Other languages
Chinese (zh)
Inventor
冯建军
杨红红
罗兴锜
朱国俊
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.)
Suzhou Xili Technology Services Ltd.
Original Assignee
Xian University of Technology
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 Xian University of Technology filed Critical Xian University of Technology
Priority to CN201721880342.2U priority Critical patent/CN207830207U/en
Application granted granted Critical
Publication of CN207830207U publication Critical patent/CN207830207U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A kind of centrifugal pump impeller disclosed by the utility model, including back shroud, multiple blades are evenly arranged on back shroud, the pressure face end of each blade afterbody is provided with spoiler, and spoiler is arranged along the radial direction of back shroud, the thickness of spoiler is the 1/5~1/3 of vane thickness, and the length of spoiler is equal with the momentum layer of blade position loss thickness, and the height of spoiler is equal with the height of blade.By the way that spoiler is arranged on blade, through-flow effect of the fluid in runner can be improved, make to move after high pressure zone position at runner exit while increasing blade suction surface pressure, to delay the formation of flow separation and stall whirlpool, flow separation and stall problem of the centrifugal pump under low flow rate condition are effectively reduced, the interior external characteristics of pump is further increased.

Description

A kind of centrifugal pump impeller
Technical field
The utility model belongs to centrifugation pump technical field, is related to a kind of centrifugal pump impeller.
Background technology
When centrifugal pump is run under low flow rate condition, since the reduction of flow makes axis plane velocity reduce, the angle of attack increases, fluid There is flow separation in blade suction surface, form separation vortex, separation vortex is developing progressively as stall group, and stall group is plugging stream Road destroys proper flow, seriously affects the operation stability and efficiency of pump.
The research for centrifuging pump stall is mostly rested at present, stall event inside centrifugal pump under low flow rate condition is divided It analyses and to that in the analysis of stall group kinetic characteristic, can not reduce and control the stall event of centrifugal pump, to centrifugal blade itself The optimization design effect unobvious of progress.
Utility model content
The purpose of this utility model is to provide a kind of centrifugal pump impellers, can reduce centrifugal pump under low flow rate condition Flow separation and stall event.
The utility model is the technical scheme adopted is that a kind of centrifugal pump impeller, including back shroud, is uniformly set on back shroud Multiple blades are equipped with, the pressure face end of each blade afterbody is provided with spoiler, and spoiler is arranged along the radial direction of back shroud, The thickness of spoiler is the 1/5~1/3 of vane thickness, and the length of spoiler loses thickness phase with the momentum layer of blade position Deng the height of spoiler is equal with the height of blade.
The utility model is also characterized by
The quantity of blade is 4~6.
The beneficial effects of the utility model are:
The impeller of the utility model can improve through-flow effect of the fluid in runner by the way that spoiler is arranged on blade, Make to move after high pressure zone position at runner exit, to delay the formation of flow separation and stall whirlpool, effectively reduces centrifugal pump small Flow separation under flow rate working conditions and stall event further increase the interior external characteristics of pump.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of centrifugal pump impeller of the utility model;
Fig. 2 is a kind of structural schematic diagram of centrifugal pump impeller intra vane of the utility model.
In figure, 1. back shrouds, 2. blades, 3. spoilers.
Specific implementation mode
The utility model is described in detail with reference to the accompanying drawings and detailed description.
A kind of centrifugal pump impeller of the utility model is evenly arranged with more as shown in Figure 1, including back shroud 1 on back shroud 1 The pressure face end of a blade 2,2 tail portion of each blade is provided with spoiler 3, and spoiler 3 is arranged along the radial direction of back shroud 1, As shown in Fig. 2, the height of spoiler 3 is equal with the height of blade 2, the thickness c of spoiler 3 is the 1/5~1/3 of 2 thickness of blade, The length h of spoiler 3 is equal with the momentum layer of 2 position of blade loss thickness θ, and specific formula for calculation is as follows:U is the velocity component that 3 position of spoiler is parallel to blade surface in formula, and U is blade institute External potential barrier speed corresponding to position, y are the distance perpendicular to blade surface, and boundary layer thickness δ takes blade surface to speed Spend the distance at u=0.99U.
The quantity of blade 2 is 4~6.
Preferably, the quantity of blade 2 is 5.
A kind of course of work of centrifugal pump impeller of the utility model is as follows:
When work, fluid enters along blade 2 in the runner on back shroud 1, and at runtime, spoiler 3 prevents blade to blade 2 The tail of a runner enters next runner on 2, and forms higher-pressure region in next runner exit, and spoiler 3 makes in next runner It is moved after high pressure zone position;Spoiler 3 improves the pressure of 2 suction surface of blade while increasing 2 pressure surface pressure of blade, postpone leaf 2 suction surface boundary layer separation of piece, makes to be not susceptible to flow separation;To reduce the possibility that stall occurs for runner, can effectively solve Certainly centrifuge pump stall problem.
In the above manner, the impeller of the utility model can improve fluid in runner by the way that spoiler is arranged on blade Interior through-flow effect makes to move after high pressure zone position at runner exit while increasing blade suction surface pressure, to delay to flow The formation of dynamic separation and stall whirlpool, effectively reduces flow separation and stall problem of the centrifugal pump under low flow rate condition, further Improve the interior external characteristics of pump.

Claims (2)

1. a kind of centrifugal pump impeller, which is characterized in that including back shroud (1), multiple leaves are evenly arranged on the back shroud (1) The pressure face end of piece (2), each blade (2) tail portion is provided with spoiler (3), and the spoiler (3) is along back shroud (1) radial setting, the thickness of the spoiler (3) are the 1/5~1/3 of blade (2) thickness, the length of the spoiler (3) Equal with the momentum layer of blade (2) position loss thickness, the height of the spoiler (3) is equal with the height of blade (2).
2. a kind of centrifugal pump impeller as described in claim 1, which is characterized in that the quantity of the blade (2) is 4~6.
CN201721880342.2U 2017-12-28 2017-12-28 A kind of centrifugal pump impeller Active CN207830207U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721880342.2U CN207830207U (en) 2017-12-28 2017-12-28 A kind of centrifugal pump impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721880342.2U CN207830207U (en) 2017-12-28 2017-12-28 A kind of centrifugal pump impeller

Publications (1)

Publication Number Publication Date
CN207830207U true CN207830207U (en) 2018-09-07

Family

ID=63390450

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721880342.2U Active CN207830207U (en) 2017-12-28 2017-12-28 A kind of centrifugal pump impeller

Country Status (1)

Country Link
CN (1) CN207830207U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110043507A (en) * 2019-05-23 2019-07-23 萨震压缩机(上海)有限公司 A kind of energy-saving centrifugal impeller
CN113153809A (en) * 2020-12-31 2021-07-23 西安航空学院 High-speed centrifugal wheel with bionic fish tail fin

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110043507A (en) * 2019-05-23 2019-07-23 萨震压缩机(上海)有限公司 A kind of energy-saving centrifugal impeller
CN110043507B (en) * 2019-05-23 2024-06-07 萨震压缩机(上海)有限公司 Energy-saving centrifugal impeller
CN113153809A (en) * 2020-12-31 2021-07-23 西安航空学院 High-speed centrifugal wheel with bionic fish tail fin

Similar Documents

Publication Publication Date Title
CN105650032B (en) The diffuser of centrifugal compressor
CN104776050B (en) A kind of impeller for double suction centrifugal pump and volute chamber guiding device
CN104895832B (en) A kind of Hydraulic Design Method of high viscosity centrifugal pump impeller
CN105736426A (en) Axial flow fan comprising blade pressure surfaces with winglets and blade tops with blowing structures
CN207830207U (en) A kind of centrifugal pump impeller
CN105736425A (en) Axial flow fan comprising blades with wing-type guide plates and guide blades with bionic tail edges
CN106704261A (en) Axial flow fan ternary impeller with vein-shaped structure and nonuniform empennage
CN107061329A (en) A kind of axial flow blower
CN105756996A (en) Axial flow fan with blade suction surfaces having vortex breaking structures and with grooves formed in blade tops
CN103195757A (en) Pneumatic designing method of counter rotating compressor combining pumping of boundary layer
CN106050736B (en) A kind of centrifugal blower noise reduction leaf blade structure
CN109026830B (en) Centrifugal impeller
CN106762824A (en) Axial flow blower 3 d impeller with leaf vein texture and sea-gull type splitterr vanes
CN105822589B (en) A kind of centrifugal pump impeller that work efficiency is high
CN106089808B (en) A kind of blade diffuser and its formative method with trailing edge structures before swallow-tail form
CN204610372U (en) A kind of centrifugal impeller of blade trailing edge band winglet
CN104912843B (en) A kind of mixed-flow pump impeller with working face ellipse exit edge of blade
CN206929130U (en) Axial flow blower 3 d impeller with leaf vein texture and sea-gull type splitterr vanes
CN110529426B (en) Open impeller structure for high-speed pump
CN201250795Y (en) Integral casting impeller
CN103233914B (en) Guide axial flow pump impeller
CN102392831A (en) Swept-curved blade for high-speed fuel oil axial-flow pump
CN205639001U (en) Axial fan that winglet and ye ding have air -blowing structure is worn to blade pressure
CN208106824U (en) Centrifugal pump impeller
CN104279180A (en) Double-suction impeller

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20201119

Address after: No.2358, east side of Chang'an Road, Wujiang Economic and Technological Development Zone, Suzhou, Jiangsu Province, 215200

Patentee after: Suzhou Xili Technology Services Ltd.

Address before: 710048 Shaanxi city of Xi'an Province Jinhua Road No. 5

Patentee before: XI'AN University OF TECHNOLOGY

TR01 Transfer of patent right