CN113704897A - Hydraulic design method of self-air-entraining submersible aerator - Google Patents

Hydraulic design method of self-air-entraining submersible aerator Download PDF

Info

Publication number
CN113704897A
CN113704897A CN202010438411.4A CN202010438411A CN113704897A CN 113704897 A CN113704897 A CN 113704897A CN 202010438411 A CN202010438411 A CN 202010438411A CN 113704897 A CN113704897 A CN 113704897A
Authority
CN
China
Prior art keywords
water
impeller
diameter
air
taking
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.)
Granted
Application number
CN202010438411.4A
Other languages
Chinese (zh)
Other versions
CN113704897B (en
Inventor
白羽
王得安
马超
李宁
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.)
Xylem Europe GmbH
Original Assignee
Xylem Europe GmbH
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 Xylem Europe GmbH filed Critical Xylem Europe GmbH
Priority to CN202010438411.4A priority Critical patent/CN113704897B/en
Publication of CN113704897A publication Critical patent/CN113704897A/en
Application granted granted Critical
Publication of CN113704897B publication Critical patent/CN113704897B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • CCHEMISTRY; METALLURGY
    • C02TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02FTREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F7/00Aeration of stretches of water
    • 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
    • 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
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D31/00Pumping liquids and elastic fluids at the same time
    • CCHEMISTRY; METALLURGY
    • C02TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02FTREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F2201/00Apparatus for treatment of water, waste water or sewage
    • C02F2201/002Construction details of the apparatus
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02WCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
    • Y02W10/00Technologies for wastewater treatment
    • Y02W10/10Biological treatment of water, waste water, or sewage

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical & Material Sciences (AREA)
  • Water Supply & Treatment (AREA)
  • Computational Mathematics (AREA)
  • Hydrology & Water Resources (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Aeration Devices For Treatment Of Activated Polluted Sludge (AREA)

Abstract

The invention discloses a hydraulic design method of a self-air-entraining submersible aerator, which comprises the following steps: step 1, according to the output power P of the motorShaftRated speed n, submerging depth h and air inflow QQi (Qi)Calculating parameters of the impeller; step 2, calculating size parameters of guide vanes; and 3, calculating the size parameter of the aeration disc. The design calculation formula of the geometric dimensions of the impeller, the guide vane and the aeration disc is given, and the gas-water mixing proportion, the gas compression and the jet stability are consideredAnd 4 parameters of power, rotating speed, design submerging depth and air inflow of the submersible motor are selected and matched, and the geometric dimensions of the impeller, the guide vane and the aeration disc are designed and calculated.

Description

Hydraulic design method of self-air-entraining submersible aerator
Technical Field
The invention belongs to the technical field of aerators, and particularly relates to a hydraulic design method of a self-air-entraining submersible aerator.
Background
Aeration is one of the important process flows for treating sewage by an activated sludge method. The self-air-entraining submersible aerator utilizes a submersible motor to drive an impeller to rotate, so that nearby water flow enters the impeller. At the same time, the centrifugal force of the impeller creates a vacuum at the inlet, drawing air in through the bleed duct. The air and the water are fully mixed in the guide vane and are ejected out through the jet pipe on the aeration disc, and effective convection circulation is formed. The air is divided into a large number of fine bubbles, and the fine bubbles are fully mixed with the activated sludge and the sewage, so that the growth of aerobic microorganisms is promoted, organic pollutants in the water body are degraded, and the sewage is purified.
The core of the self-air-entraining submersible aerator for realizing the aeration function is a hydraulic component which consists of an impeller, a guide vane and an aeration disc. The geometrical size of the hydraulic component determines the performance of the aerator, so a hydraulic method is needed to improve the aeration performance of the aerator.
Disclosure of Invention
Therefore, the technical problem to be solved by the invention is that the existing hydraulic design method is complex and tedious, and the performance of the obtained aerator cannot meet the requirement of air input under the submerging depth.
Therefore, the technical scheme is that the hydraulic design method of the self-air-entraining type submersible aerator comprises the following steps:
step 1, according to the output power P of the motorShaftRated speed n, submerging depth h and air inflow QQi (Qi)The parameters of the impeller are calculated,
step 2, calculating size parameters of guide vanes;
and 3, calculating the size parameter of the aeration disc.
Preferably, the step 1 comprises:
the parameters of the impeller include:
dimension D of air entraining pipeQi (Qi)
Figure BDA0002503163750000021
Wind speed VQi (Qi)Taking 7-12m/s, and taking the standard pipeline size similar to the calculated value;
impeller air inlet diameter D0
D0=kD0×DQi (Qi)
kD0Taking 0.6-0.8;
diameter D of blade air inlet1
D1=kD1×D0
kD1Taking 1.05-1.3;
gas flow (after compression) Q at the impeller exitGas 2
Figure BDA0002503163750000025
In the formula P0Is the local atmospheric pressure (Pa), ρWater (W)Is the density of water (kg/m)3) G acceleration of gravity (m/s)2) (ii) a Water flow Q in aeratorWater (W)
Figure BDA0002503163750000022
V is the proportion of water in the gas-water mixture, and is 40% -60% of the water;
density ρ of gas-liquid mixture at impeller exitMixing of
Figure BDA0002503163750000023
Where rhoQi (Qi)Is the air density (kg/m) at local atmospheric pressure3);
Hydraulic efficiency eta of aeratorh
Figure BDA0002503163750000024
Total efficiency eta of aerator
η=kη×ηh
In the formula kηTaking 0.6-0.8;
lift H of aerator
Figure BDA0002503163750000031
Theoretical lift H of aeratort
Figure BDA0002503163750000032
Width b of impeller outlet2
Figure BDA0002503163750000033
In the formula kb2Taking 0.6-0.8;
sltotra slip coefficient sigma
Figure BDA0002503163750000034
In the formula, z is the number of leaves, and 4-7 leaves are selected; beta is a2Setting an angle for the outlet of the blade, wherein the angle is 60-90 degrees;
the assumed value of the outer diameter of the impeller is D2 false
Axial surface flow velocity V at impeller outletm2
Figure BDA0002503163750000035
Peripheral speed U at the impeller outlet2
Figure BDA0002503163750000036
The calculated value of the impeller outer diameter is D2
Figure BDA0002503163750000037
D2And D2 falseComparing, and if the two are the same, taking the value of the outer diameter of the impeller; if the two are greatly different, re-assuming D2 falseRe-calculating according to the steps until D2And D2 falseIdentical or similar;
the intersection point of the cover plate and the blade does not exceed the front 1/3 of the length of the blade, and the diameter of the intersection point is recorded as a blade water inlet D1 Water
Suppose the diameter D of the impeller water inlet0 water
Measurement D0 waterThe total area between the inner impeller cover plates, i.e. the water inlet area of the impeller, is denoted S0 water
Velocity of inflow VWater (W)
Figure BDA0002503163750000041
Inlet flow velocity VWater (W)Is 3m/s, if VWater (W)If the calculated value has a large deviation, re-assuming D0 waterUp to VWater (W)Meets the requirements.
Preferably, the step 2 comprises:
the dimensional parameters of the guide vane include:
diameter D of inlet of guide vane3
D3=kD3×D3
In the formula kD3Taking 1.01-1.02.
Diameter D of guide vane outlet4
D4=kD4×D3
In the formula kD4Taking 1.4-1.6.
Preferably, the step 3 comprises:
the size parameters of the aeration disc comprise:
the inner diameter of the aeration disc is equal to the diameter D of the guide vane outlet4
The aeration disc consists of a plurality of jet pipes, the number of the jet pipes is the same as that of the guide vanes, and the installation angle is tangent to the working surface of the guide vane flow channel; the shape of the jet flow pipe adopts a rectangular pipe, and the rectangular section is larger than the size of a flow passage of the guide vane outlet;
equivalent hydraulic diameter D of jet pipeEquivalent weight
Figure BDA0002503163750000042
In the formula, a is the length of the overflowing section of the rectangular pipe, and b is the width of the overflowing section of the rectangular pipe;
selecting the outer diameter D of the aeration disc5And measuring the length L of the jet pipe, wherein the length of the jet pipe is 3-4 times of the equivalent hydraulic diameter in order to keep the water flow stable and prevent the bubbles from being expanded excessively.
The technical scheme of the invention has the following advantages: the hydraulic design method of the self-air-entraining submersible aerator can simply and conveniently design the hydraulic component of the aerator by considering factors such as air-water mixing ratio, gas compression, jet stability and the like, and meets the requirement of designing the air inflow under the submerging depth through a prototype test.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and drawings.
The technical solution of the present invention is further described in detail by the accompanying drawings and embodiments.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:
FIG. 1 is a flow chart of the present invention.
FIG. 2 is a plan view of a hydraulic component of one embodiment of the present invention.
Fig. 3 is a plan view of an impeller according to an embodiment of the present invention.
FIG. 4 is a plan view of a blade of one embodiment of the present invention
FIG. 5 is a plan view of a guide vane of an embodiment of the present invention.
Fig. 6 is a plan view of an aeration panel according to an embodiment of the present invention.
Fig. 7 is a schematic structural view of an aerator according to the present invention.
Wherein, 1, impeller, 2 guide vanes, 3 aeration discs, 4 impeller air inlet D 05. blade water inlet D 1 Water6. impeller external diameter D27. diameter of blade inlet D 18, diameter D of impeller water inlet 0 water9. blade outlet setting angle beta 210 impeller water inlet area, 11 guide vane inlet diameter D 312 guide vane outlet diameter/aeration disc inner diameter D 413, outer diameter D of aeration disc 514, the length L of the jet pipe, 15, the length a of the flow section of the rectangular pipe, 16, the width b of the flow section of the rectangular pipe, 17, and the jet pipe.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are described herein for the purpose of illustration and explanation and not limitation.
The invention provides a hydraulic design method of a self-air-entraining submersible aerator, which is shown in figures 1-7 and adopts design input
Output power P of motorShaft=3.3kW;
Rated speed n 1380 rpm;
designing the submerging depth h to be 4 m;
design air input QQi (Qi)=55m3/h;
Design step
Design of impeller
Dimension D of air entraining pipeQi (Qi)
Figure BDA0002503163750000061
Wind speed V in the bleed air ductQi (Qi)Taking 7-12m/s, taking the standard pipeline size close to the calculated value, and taking the air guide pipe size DQi (Qi)=0.05m。
Impeller air inlet diameter D0
D0=kD0×DQi (Qi)=0.76×0.05=0.038m
kD0Taking 0.6-0.8.
Dimension D of blade inlet1
D1=kD1×D0=1.105×0.038=0.042m
kD1Taking 1.05-1.3.
Gas flow (after compression) Q at the impeller exitGas 2
Figure BDA0002503163750000071
In the formula P0Is the local atmospheric pressure (Pa), ρWater (W)Is the density of water (kg/m)3) G acceleration of gravity (m/s)2)。
Water flow Q in aeratorWater (W)
Figure BDA0002503163750000072
In the formula, V is the proportion of water in the gas-water mixture, and is generally 40% -60%.
Density ρ of gas-liquid mixture at impeller exitMixing of
Figure BDA0002503163750000073
Where rhoQi (Qi)Is the air density (kg/m) at local atmospheric pressure3)。
Aeration machineHydraulic efficiency etah
Figure BDA0002503163750000074
Total efficiency eta of aerator
η=kη×ηh=0.64×61%=38.7%
In the formula kηTaking 0.6-0.8.
Lift H of aerator
Figure BDA0002503163750000075
Theoretical lift H of aeratort
Figure BDA0002503163750000076
Width b of impeller outlet2
Figure BDA0002503163750000077
In the formula kb2Taking 0.7-0.9.
Sltotra slip coefficient sigma
Figure BDA0002503163750000081
Wherein z is the number of leaves, and is usually 4-7; beta is a2The angle for the blade exit is typically 60 to 90.
The assumed value of the outer diameter of the impeller is D2 false=0.268m
Axial surface flow velocity V at impeller outletm2
Figure BDA0002503163750000082
Peripheral speed U at the impeller outlet2
Figure BDA0002503163750000083
The calculated value of the impeller outer diameter is D2
Figure BDA0002503163750000084
D2And D2 falseComparing, and if the two are the same, taking the value of the outer diameter of the impeller; if the two are greatly different, re-assuming D2 falseRe-calculating according to the steps until D2And D2 falseIdentical or similar.
The intersection point of the cover plate and the blade does not exceed the front 1/3 of the length of the blade, and the diameter of the point is recorded as D1 Water
The length of the blade is 120mm, the front end of the blade length is 40mm from the intersection point of the cover plate and the blade, and D is measured1 Water=0.111m
Suppose the diameter D of the impeller water inlet0 water=0.161m
Measurement D0 waterThe total area between the inner impeller cover plates, i.e. the water inlet area of the impeller, is denoted S0 water=0.004975m2Velocity of inflow VWater (W)
Figure BDA0002503163750000091
Inlet flow velocity VWater (W)Generally about 3m/s, if VWater (W)If the calculated value has a large deviation, re-assuming D0 waterUp to VWater (W)Meets the requirements.
Design of guide vane
Diameter D of inlet of guide vane3
D3=kD3×D2=1.015×0.268=0.272m
In the formula kD3Take 1.01-1.02。
Diameter D of guide vane outlet4
D4=kD4×D3=1.4×0.272=0.38m
In the formula kD4Taking 1.4-1.6.
The design of the guide vane blade refers to a design method of a radial positive guide vane of a centrifugal pump.
Design of aeration disc
The inner diameter of the aeration disc is equal to the diameter D of the guide vane outlet4=0.38m
The aeration disc is composed of a plurality of jet pipes, and the installation angle of the jet pipes is tangent to the working surface of the guide vane flow channel. The shape of the jet pipe adopts a standard rectangular pipe, 50 multiplied by 40 multiplied by 3, and the rectangular section is slightly larger than the size of a flow passage of the guide vane outlet.
Equivalent hydraulic diameter D of jet pipeEquivalent weight
Figure BDA0002503163750000092
In the formula, a is the length of the flow section of the rectangular pipe, and b is the width of the flow section of the rectangular pipe.
Selecting the outer diameter D of the aeration disc5The length L of the jet pipe was 143mm, which was 0.6 m.
Figure BDA0002503163750000101
The length of the jet pipe is 3.73 times of the equivalent hydraulic diameter, and the jet pipe meets the requirement.
Up to this point, the geometry of the hydraulic components (impeller, guide vanes, aeration disc) of the self-bleed submersible aerator has been calculated.
It will be apparent to those skilled in the art that various changes and modifications may be made in the present invention without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include such modifications and variations.

Claims (4)

1. A hydraulic design method of a self-air-entraining submersible aerator is characterized by comprising the following steps:
step 1, outputting power according to a motorShaftRated speed n, submerging depth h and air inflow QQi (Qi)Calculating parameters of the impeller;
step 2, calculating size parameters of guide vanes;
and 3, calculating the size parameter of the aeration disc.
2. The hydraulic design method of a self-air-entraining submersible aerator as claimed in claim 1 wherein step 1 comprises:
the parameters of the impeller include:
dimension D of air entraining pipeQi (Qi)
Figure FDA0002503163740000011
Wind speed VQi (Qi)Taking 7-12m/s, and taking the standard pipeline size similar to the calculated value;
impeller air inlet diameter D0
D0=kD0×DQi (Qi)
kD0Taking 0.6-0.8;
diameter D of blade air inlet1
D1=kD1×D0
kD1Taking 1.05-1.3;
gas flow (after compression) Q at the impeller exitGas 2
Figure FDA0002503163740000012
In the formula P0Is the local atmospheric pressure (Pa), ρWater (W)Is the density of water (kg/m)3) G acceleration of gravity (m/s)2);
Water flow Q in aeratorWater (W)
Figure FDA0002503163740000013
V is the proportion of water in the gas-water mixture, and is 40% -60% of the water;
density ρ of gas-liquid mixture at impeller exitMixing of
Figure FDA0002503163740000021
Where rhoQi (Qi)Is the air density (kg/m) at local atmospheric pressure3);
Hydraulic efficiency eta of aeratorh
Figure FDA0002503163740000022
Total efficiency eta of aerator
η=kη×ηh
In the formula kηTaking 0.6-0.8;
lift H of aerator
Figure FDA0002503163740000023
Theoretical lift H of aeratort
Figure FDA0002503163740000024
Width b of impeller outlet2
Figure FDA0002503163740000025
In the formula kb2Taking 0.6-0.8;
sltotra slip coefficient sigma
Figure FDA0002503163740000026
Wherein z is the number of leaves, and 4-7 leaves are selected; beta is a2Setting an angle for the outlet of the blade, wherein the angle is 60-90 degrees;
the assumed value of the outer diameter of the impeller is D2 false
Axial surface flow velocity V at impeller outletm2
Figure FDA0002503163740000027
Peripheral speed U at the impeller outlet2
Figure FDA0002503163740000031
The calculated value of the impeller outer diameter is D2
Figure FDA0002503163740000032
D2And D2 falseComparing, and if the two are the same, taking the value of the outer diameter of the impeller; if the two are greatly different, re-assuming D2 falseRe-calculating according to the steps until D2And D2 falseIdentical or similar;
the intersection point of the cover plate and the blade does not exceed the front 1/3 of the length of the blade, and the diameter of the intersection point is recorded as a blade water inlet D1 Water
Suppose the diameter D of the impeller water inlet0 water
Measurement D0 waterThe total area between the inner impeller cover plates, i.e. the water inlet area of the impeller, is denoted S0 water
Velocity of inflow VWater (W)
Figure FDA0002503163740000033
Inlet flow velocity VWater (W)Is 3m/s, if VWater (W)If the calculated value has a large deviation, re-assuming D0 waterUp to VWater (W)Meets the requirements.
3. The hydraulic design method of a self-air-entraining submersible aerator as claimed in claim 2 wherein step 2 comprises:
the dimensional parameters of the guide vane include:
diameter D of inlet of guide vane3
D3=kD3×D2
In the formula kD3Taking 1.01-1.02.
Diameter D of guide vane outlet4
D4=kD4×D3
In the formula kD4Taking 1.4-1.6.
4. A method of hydraulic design of a self-entraining air submersible aerator as claimed in claim 3 wherein step 3 includes:
the size parameters of the aeration disc comprise:
the inner diameter of the aeration disc is equal to the diameter D of the guide vane outlet4
The aeration disc consists of a plurality of jet pipes, the number of the jet pipes is the same as that of the guide vanes, and the installation angle is tangent to the working surface of the guide vane flow channel; the shape of the jet flow pipe adopts a rectangular pipe, and the rectangular section is larger than the size of a flow passage of the guide vane outlet;
equivalent hydraulic diameter D of jet pipeEquivalent weight
Figure FDA0002503163740000041
In the formula, a is the length of the overflowing section of the rectangular pipe, and b is the width of the overflowing section of the rectangular pipe;
selecting the outer diameter D of the aeration disc5And measuring the length L of the jet pipe, wherein the length of the jet pipe is 3-4 times of the equivalent hydraulic diameter in order to keep the water flow stable and prevent the bubbles from being expanded excessively.
CN202010438411.4A 2020-05-22 2020-05-22 Hydraulic design method of self-bleed type submersible aerator Active CN113704897B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010438411.4A CN113704897B (en) 2020-05-22 2020-05-22 Hydraulic design method of self-bleed type submersible aerator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010438411.4A CN113704897B (en) 2020-05-22 2020-05-22 Hydraulic design method of self-bleed type submersible aerator

Publications (2)

Publication Number Publication Date
CN113704897A true CN113704897A (en) 2021-11-26
CN113704897B CN113704897B (en) 2023-10-10

Family

ID=78645991

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010438411.4A Active CN113704897B (en) 2020-05-22 2020-05-22 Hydraulic design method of self-bleed type submersible aerator

Country Status (1)

Country Link
CN (1) CN113704897B (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105201916A (en) * 2015-09-17 2015-12-30 浙江工业大学之江学院 Designing method for hydraulic power of space guide-blade centrifugal pump
CN108503052A (en) * 2018-06-25 2018-09-07 安徽建筑大学 A kind of underwater microbubble aerator of differential dual-impeller and its method
KR101944719B1 (en) * 2018-11-22 2019-04-17 주식회사 대영파워펌프 Method for designing external diameter size of impeller

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105201916A (en) * 2015-09-17 2015-12-30 浙江工业大学之江学院 Designing method for hydraulic power of space guide-blade centrifugal pump
CN108503052A (en) * 2018-06-25 2018-09-07 安徽建筑大学 A kind of underwater microbubble aerator of differential dual-impeller and its method
KR101944719B1 (en) * 2018-11-22 2019-04-17 주식회사 대영파워펌프 Method for designing external diameter size of impeller

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
曹卫东 等: "潜水曝汽机水力设计探讨", 中国农村水利水电, no. 01, pages 13 - 14 *
朱荣生;李小龙;施卫东;刘苓苓;王韬;: "潜水自引气曝气机的数值模拟与试验研究", 排灌机械工程学报, no. 01, pages 50 - 55 *
王勇;明加意;董亮;刘厚林;刘嘉伟;汪文生;: "运行参数对倒伞曝气机曝气性能影响试验", 农业工程学报, no. 20, pages 67 - 73 *

Also Published As

Publication number Publication date
CN113704897B (en) 2023-10-10

Similar Documents

Publication Publication Date Title
EP1765486A1 (en) Apparatus and method for diffused aeration
CN108361205A (en) A kind of centrifugal pump impeller and the LNG immersed pumps comprising the centrifugal pump impeller
CN1231664C (en) Hydraulic turbine system
CN201546969U (en) Stainless steel horizontal-type end suction multi-stage centrifugal pump
CN113704897A (en) Hydraulic design method of self-air-entraining submersible aerator
CN103743257A (en) Efficient hydrodynamic cooling tower
US8056887B2 (en) Apparatus for surface mixing of gasses and liquids
Schraa et al. A comprehensive aeration system model for WRRF design and control
RU2422733C1 (en) Heat cavitation generator
CN106050700A (en) Noiseless fan structure
CN115475546A (en) Wing section microbubble generator
CN210859291U (en) Centrifugal fan
CN103244440B (en) Hydrodynamic(al) wind power thruster and cooling tower wind power system
CN203809056U (en) Centrifugal turbine
CN201071327Y (en) Submersible aerator
CN106640692A (en) Centrifugal compressor with induction wheel
Guo et al. Flow passage shape design of a high pressure multistage centrifugal pump for performance improvement and miniaturization
CN202597263U (en) Large-flow single-shaft constant-temperature air-compressor spiral casing structure
CN104389798A (en) Axial flow energy-saving fan
CN205876763U (en) Muting draught fan structure
JPH04505199A (en) Centrifugal blower with airfoil vanes in a circular spiral envelope
CN213416418U (en) Integrated mixed flow type aeration plug flow device
CN111966956B (en) Method for calculating lift and flow of multi-stage submersible pump for well
CN204267335U (en) Axial type energy-saving blower fan
CN220151568U (en) Small-sized double-blade isolation type centrifugal fan

Legal Events

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