CN102865893A - Reverse thrust circular-arc impeller of high-pressure automatic flow controller - Google Patents

Reverse thrust circular-arc impeller of high-pressure automatic flow controller Download PDF

Info

Publication number
CN102865893A
CN102865893A CN2011101897256A CN201110189725A CN102865893A CN 102865893 A CN102865893 A CN 102865893A CN 2011101897256 A CN2011101897256 A CN 2011101897256A CN 201110189725 A CN201110189725 A CN 201110189725A CN 102865893 A CN102865893 A CN 102865893A
Authority
CN
China
Prior art keywords
blade
impeller
arc
fluid
reverse thrust
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.)
Pending
Application number
CN2011101897256A
Other languages
Chinese (zh)
Inventor
王江
林浩
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.)
Shanghai Yinuo Instrument Co Ltd
Original Assignee
Shanghai Yinuo Instrument Co Ltd
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 Shanghai Yinuo Instrument Co Ltd filed Critical Shanghai Yinuo Instrument Co Ltd
Priority to CN2011101897256A priority Critical patent/CN102865893A/en
Publication of CN102865893A publication Critical patent/CN102865893A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to a reverse thrust circular-arc impeller of a high-pressure automatic flow controller. The impeller comprises a plurality of blades and a hub, wherein the plurality of blades are arranged on the hub; both ends of an impeller shaft are connected with a shaft sleeve in a rotatable way; and a reverse thrust window is arranged at the root parts of the blades near the hub. The area of the reverse thrust window is 1/10 of the area of an integral blade. The blade 3 is circular-arc concave; and the concave surface of the blade 3 faces the flow direction of fluid in utilization and installation. The circular-arc radius of the circular-arc concave surface of the blade 3 is from 20mm to 30mm. According to the dynamic balance principle of fluid dynamics, the dynamic pressure of the front surface of the blade is equal to that of the back part of the blade. Meanwhile, the blade is made into a fluid-facing circular-arc concave surface which faces the fluid, so that Karman vortices generated when partial fluid which passes through the reverse thrust window in the process of penetrating through the blade better can act on the back surface of the blade of the impeller so as to generate a reverse thrust F1, which is in direct proportion to fluid dynamics and impact force F of the front surface of the blade of the impeller. Accordingly, the dynamics on the blade of the impeller reaches a dynamic balance state.

Description

The anti-arc impeller that pushes away of high pressure flow auto-controlling apparatus
Technical field
The present invention is the anti-arc impeller that pushes away for high pressure flow auto-controlling apparatus, particularly to the improvement of its structure.
Background technology
At present, high pressure flow auto-controlling apparatus is being widely applied aspect the high pressure underground flooding of oil field owing to itself technology.
The vane type high pressure flow auto-controlling apparatus that adopts at present, impeller is vertical (being also referred to as normal direction) impeller, impeller is planar structure.Its subject matter is: when flow acted on the impeller along pipeline, its impulsive force will make impeller compressing impeller shaft, makes on the impeller shaft inwall that is attached to its axle sleeve tightly, produces thus larger friction of motion and friction force.This friction force will produce three unfavorable factors, and the first starts flow and becomes large; It two makes when being large flow impeller rotation descend; Thereby the relation that makes its revolution and flow is no longer followed original mathematical model rule, increases linear error; It three is that the Trunk Line flow will make when Pulsating Flow is arranged impeller shaft and sleeve lining produce impact friction, increases reproducibility error, affects its life-span and impact friction power.
Summary of the invention
The shortcoming that exists for overcoming above-mentioned prior art the invention provides a kind of new blade wheel structure.
The anti-arc impeller that pushes away of a kind of high pressure flow auto-controlling apparatus, this impeller is comprised of some blades and wheel hub, and some blades are arranged on the wheel hub, and the impeller shaft two ends are rotationally connected axle sleeve; It is characterized in that, have a reaction thrust window at root of blade near wheel hub.
The area of described reaction thrust window is integrated plate blade area 1/10.
Described blade is the circular arc spill, uses when installing, and forward face is met the flow direction to fluid.
In order to reduce and improve friction of motion and the impact friction power between impeller shaft and the sleeve lining, will alleviate as much as possible this kinetic friction force and impact friction power.
The present invention near reaction thrust window of wheel hub processing, arrives the back side of blade at root of blade according to fluid dynamic dynamic balance principle with the blade that makes things convenient for front fluid to pass through impeller, the dynamic pressure at the front of blade and back equates like this; Simultaneously blade is made to meet to meeting of fluid and flowed the circular arc spill, thereby make the segment fluid flow by the reaction thrust window when passing blade, produce the back side that the toll bar whirlpool acts on the blade of impeller better.A thereby reaction thrust F who produces 1, this reaction thrust F 1Be proportional to hydrodynamic force and the impulsive force F of the face of blade of impeller; And then the suffered power of the blade that makes impeller reaches a kind of dynamic equilibrium state, and because this reaction thrust F 1,Thereby impeller shaft is unlikely to and the undue tight friction of sleeve lining, and can produces a slit, be more convenient for fluid media (medium) itself and play effect as lubricant.Structure of the present invention makes impeller operation more steady, and the life-span is larger, and precision is higher, and large-capacity point (upper limit flow) can be larger, and flow range is wider.
Description of drawings
Accompanying drawing 1 is structural representation of the present invention.
Accompanying drawing 2 is Fig. 1 left views.
1 axle sleeve, 2 impeller shafts, 3 blades, 4 anti-window, 5 wheel hubs of pushing away.
Embodiment
The anti-arc impeller that pushes away of a kind of high pressure flow auto-controlling apparatus, this impeller is comprised of some blades 3 and wheel hub 5, and some blades 3 are arranged on the wheel hub 5, and impeller shaft 2 two ends are rotationally connected axle sleeve 1; Have a reaction thrust window 4 at root of blade near wheel hub 5 places.The area of described reaction thrust window 4 is integrated plate blade area 1/10.Described blade 3 is the circular arc spill, uses when installing, and blade 3 concave surfaces are met the flow direction to fluid.The arc radius of described blade arc spill is 20mm~30mm.

Claims (5)

1. anti-arc impeller that pushes away of high pressure flow auto-controlling apparatus, this impeller is comprised of some blades and wheel hub, and some blades are arranged on the wheel hub, and the impeller shaft two ends are rotationally connected axle sleeve; Have a reaction thrust window at root of blade near wheel hub.
2. according to the anti-arc impeller that pushes away of right 1 described high pressure flow auto-controlling apparatus.
3. it is characterized in that, the area of described reaction thrust window is integrated plate blade area 1/10.
4. according to right 1 or the anti-arc impeller that pushes away of 2 described high pressure flow auto-controlling apparatus, it is characterized in that, described blade is the circular arc spill, uses when installing, and forward face is met the flow direction to fluid.
5. according to the anti-arc impeller that pushes away of right 3 described high pressure flow auto-controlling apparatus, it is characterized in that, the arc radius of described blade arc spill is 20mm~30mm.
CN2011101897256A 2011-07-07 2011-07-07 Reverse thrust circular-arc impeller of high-pressure automatic flow controller Pending CN102865893A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011101897256A CN102865893A (en) 2011-07-07 2011-07-07 Reverse thrust circular-arc impeller of high-pressure automatic flow controller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011101897256A CN102865893A (en) 2011-07-07 2011-07-07 Reverse thrust circular-arc impeller of high-pressure automatic flow controller

Publications (1)

Publication Number Publication Date
CN102865893A true CN102865893A (en) 2013-01-09

Family

ID=47444908

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011101897256A Pending CN102865893A (en) 2011-07-07 2011-07-07 Reverse thrust circular-arc impeller of high-pressure automatic flow controller

Country Status (1)

Country Link
CN (1) CN102865893A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62237319A (en) * 1986-04-08 1987-10-17 Ebara Res Co Ltd Impeller flow meter
CN2433437Y (en) * 2000-08-16 2001-06-06 宁波风机有限公司 Impeller of fan
CN1595070A (en) * 2004-07-12 2005-03-16 天津市第五机床厂 Front flow guiding apparatus and turbine gas flow measurement device equipped with the same
CN202420564U (en) * 2011-07-07 2012-09-05 上海一诺仪表有限公司 Reverse thrust circular arc-shaped impeller of high-pressure flow auto-control instrument

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62237319A (en) * 1986-04-08 1987-10-17 Ebara Res Co Ltd Impeller flow meter
CN2433437Y (en) * 2000-08-16 2001-06-06 宁波风机有限公司 Impeller of fan
CN1595070A (en) * 2004-07-12 2005-03-16 天津市第五机床厂 Front flow guiding apparatus and turbine gas flow measurement device equipped with the same
CN202420564U (en) * 2011-07-07 2012-09-05 上海一诺仪表有限公司 Reverse thrust circular arc-shaped impeller of high-pressure flow auto-control instrument

Similar Documents

Publication Publication Date Title
Sutikno et al. Design, simulation and experimental of the very low head turbine with minimum pressure and freevortex criterions
Paudel et al. Experimental investigation on the effect of channel width on flexible rubber blade water wheel performance
CN204458497U (en) A kind of chemical centrifugal pump impeller reducing axial force
CN102251991A (en) Axial force balance device and method for shield pump
CN110321660B (en) Design method of large-scale mixed-flow pump impeller capable of discharging water radially
Gaetani et al. Low field in the vaned diffuser of a centrifugal pump at different vane setting angles
Nishi et al. Study on an axial flow hydraulic turbine with collection device
CN106968909A (en) Rivers Combined water water pumping power pump
JP6592259B2 (en) Water turbine propeller rotor
Gao et al. Numerical flow and performance analysis of a water-jet axial flow pump
CN103925238B (en) Epicycloid centrifugal pump impeller
Bowade et al. A review of different blade design methods for radial flow centrifugal pump
CN202420564U (en) Reverse thrust circular arc-shaped impeller of high-pressure flow auto-control instrument
JP2017008927A (en) Vertical shaft type hydraulic generating set and vertical shaft type hydraulic generating unit
CN102865893A (en) Reverse thrust circular-arc impeller of high-pressure automatic flow controller
Yamashita et al. Measurements of axial and radial thrust forces working on a three-stages centrifugal pump rotor
CN110529426B (en) Open impeller structure for high-speed pump
Nishi et al. Radial thrust of single-blade centrifugal pump
CN103939008B (en) Line projection's blade activation level rotor composite member
CN203532269U (en) Parallel type self-balance multiple-stage centrifugal pump
CN102678615A (en) Pump impeller with novel attached blades
WO2016152639A1 (en) Propeller rotor
CN203560152U (en) Impeller of two-stage centrifugal pump
Singh et al. Cavitation characteristics of a pump-turbine model by CFD analysis
CN203796618U (en) Horizontal self-balancing centrifugal pump with first-stage combination impeller

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130109