CN114329828B - Multistage centrifugal pump axial force calculation method considering mouth ring leakage - Google Patents

Multistage centrifugal pump axial force calculation method considering mouth ring leakage Download PDF

Info

Publication number
CN114329828B
CN114329828B CN202111600797.5A CN202111600797A CN114329828B CN 114329828 B CN114329828 B CN 114329828B CN 202111600797 A CN202111600797 A CN 202111600797A CN 114329828 B CN114329828 B CN 114329828B
Authority
CN
China
Prior art keywords
axial force
multistage centrifugal
centrifugal pump
formula
calculated
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
CN202111600797.5A
Other languages
Chinese (zh)
Other versions
CN114329828A (en
Inventor
王家斌
段江龙
张本营
刘军
林海
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.)
Shandong Shuanglun Co Ltd
Original Assignee
Shandong Shuanglun 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 Shandong Shuanglun Co Ltd filed Critical Shandong Shuanglun Co Ltd
Priority to CN202111600797.5A priority Critical patent/CN114329828B/en
Publication of CN114329828A publication Critical patent/CN114329828A/en
Application granted granted Critical
Publication of CN114329828B publication Critical patent/CN114329828B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention relates to a multistage centrifugal pump axial force calculation method considering mouth ring leakage, which solves the technical problem that the axial force cannot be accurately calculated by the existing multistage centrifugal pump axial force calculation method and is based on the stage number N, flow Q, single-stage lift H, rotating speed N and impeller inlet diameter D of a segmental multistage centrifugal pump 1 Diameter D of the oral ring m Hub diameter D h Equal parameters, and taking the leakage factor of the mouth ring into consideration, calculating the axial force F born by the pump A . The invention is widely applied to the field of axial force calculation of multistage centrifugal pumps.

Description

Multistage centrifugal pump axial force calculation method considering mouth ring leakage
Technical Field
The invention relates to the field of axial force calculation of multistage centrifugal pumps, in particular to a multistage centrifugal pump axial force calculation method considering mouth ring leakage.
Background
Multistage centrifugal pumps generally adopt a segmented structure, and because the front cover plate and the rear cover plate of the impeller are stressed asymmetrically, the change of fluid momentum generates reaction forces on the impeller, and the axial components of the forces are called axial forces. Axial force F A Generally comprises three parts: (1) Cover force F acting on the impeller cover A1 The direction of the air inlet is directed to the impeller inlet; (2) Kinetic reaction force F caused by fluid movement A2 The direction points to the impeller back cover plate; (3) Imbalance force F acting on pump shaft due to imbalance of suction pressure and external pressure A3 The direction is related to the suction pressure, which is greater than atmospheric pressure and directed toward the back cover plate of the impeller and less than atmospheric pressure and toward the front cover plate.
The high-pressure multistage seawater desalination pump is a type of multistage centrifugal pump, and is generally of a cantilever type structure, and axial force can cause deformation increase of a pump shaft in the operation process, so that the operation stability of a pump device is affected. Calculating the axial force is the basis for designing the pump shaft and selecting the type of the bearing. Because the multistage pump has a complex structure and large axial force, the axial force is difficult to accurately measure by the existing method.
Currently, the conventional method for calculating the axial force ignores the change of the pressure distribution of the front pump cavity caused by the flow of the sealing clearance of the mouth ring, and considers that the pressure distribution functions of the front pump cavity and the rear pump cavity are consistent, which is not accurate in practical application. Meanwhile, only the change in momentum is considered when calculating the dynamic reaction force, but the calculated dynamic reaction force is lower than the actual value because the dynamic reaction force caused by the unsteady flow in the impeller is not included, so that the conventional axial force calculation method cannot accurately calculate the axial force.
Disclosure of Invention
The invention provides a multistage centrifugal pump axial force calculation method which is more accurate in calculation and takes mouth ring leakage into consideration, and aims to solve the technical problem that the axial force calculation method of the conventional multistage centrifugal pump cannot accurately calculate the axial force.
The invention provides a multistage centrifugal pump axial force calculation method considering mouth ring leakage, which comprises the following steps:
first step, calculate the cover force F A1
The axial force applied by the single-stage impeller is F A1,i Is an axial force F acting on the front cover plate A1f,i And an axial force F acting on the back plate A1r,i The difference between the front pump cavity pressure distribution p f The rear pump chamber pressure profile p is considered as a linear function r Considered as a constant, calculated by the following formula:
F A1,i =F A1r,i -F A1f,i (1)
Figure BDA0003431701480000021
Figure BDA0003431701480000022
Figure BDA0003431701480000023
in the formulas (2) and (3), R is the distance from any point on the impeller cover plate in the radial direction to the axis, and the unit is m; r is R 2 =D 2 /2,R m =D m /2,R h =D h /2,D 2 Represents the impeller diameter, D m Diameter of the oral ring, D h Is the diameter of the hub; in formula (4), ρ represents the density of the fluid medium; k is a correction coefficient;
specific rotation speed n s Calculated by the following formula (5):
Figure BDA0003431701480000024
in the formula (5), Q represents the flow rate, and the unit of Q is m 3 S; n represents the rotating speed, and H represents the single-stage lift;
total cover force F A1 Calculated according to the following formula (6):
Figure BDA0003431701480000031
in the formula (6), F A1,1 Represents the axial force applied by the first-stage impeller, and m is more than or equal to 1 1 ≤1.2,0.96≤m 2 ≤1;
Second, the dynamic reaction force F is calculated by the following formula (7) A2
Figure BDA0003431701480000032
In the formula (7), Q represents the flow rate, and the unit of Q is m 3 S; n represents the number of stages of the segmental multistage centrifugal pump; d (D) 1 Representing leavesWheel inlet diameter; ρ represents the density of the fluid medium; c is a correction coefficient;
third, the unbalanced force F acting on the pump shaft is calculated by the following formula (8) A3
Figure BDA0003431701480000033
In the formula (8), D h Represents the hub diameter; p is p 1 The suction pressure is designed to be a given value; p is p a Is at atmospheric pressure;
fourth, the total axial force F is calculated by the following formula (9) A
F A =F A1 -F A2 +F A3 (9)
Preferably, k is more than or equal to 0.8 and less than or equal to 0.9, and the specific rotation speed n s When the rotation speed is less than 150, k takes a small value of 0.8, and the specific rotation speed n s And k takes a large value of 0.9 when the k is larger than 150.
Preferably, c is 2.8, which is a large value of 2.8 when the actual flow is not equal to the design flow.
The axial force calculation method has the advantages of being capable of accurately calculating the axial force, simple and convenient in calculation process, high in practicality and convenient to apply.
Further features and aspects of the present invention will become apparent from the following description of specific embodiments with reference to the accompanying drawings.
Drawings
FIG. 1 is a schematic structural view of a segmented multistage centrifugal pump;
FIG. 2 is a schematic illustration of impeller stress for a segmented multistage centrifugal pump;
FIG. 3 is a schematic illustration of the radial dimension of an impeller of a segmented multistage centrifugal pump;
fig. 4 is a schematic illustration of impeller sizing and pressure direction.
Detailed Description
In the prior art, a common method for calculating the axial force ignores the change of the pressure distribution of the front pump cavity caused by the flow of the sealing clearance of the mouth ring, and considers that the pressure distribution functions of the front pump cavity and the rear pump cavity are consistent, which is not accurate in practical application. Meanwhile, when calculating the dynamic reaction force, only the change in momentum is considered, but the dynamic reaction force due to the unsteady flow inside the impeller is not included, and the calculated dynamic reaction force is lower than the actual value.
According to the stage number N, flow Q, single stage lift H, rotating speed N and impeller inlet diameter D of a segmental multistage centrifugal pump 1 Diameter D of the oral ring m Hub diameter D h Equal parameters, calculating the axial force F applied by the pump A . The method comprises the following specific steps:
first step, calculate the cover force F A1
The axial force applied by the single-stage impeller is F A1,i Is an axial force F acting on the front cover plate A1f,i And an axial force F acting on the back plate A1r,i And (3) a difference. The pump orifice ring seal leakage loss is considered, so that the pressure distribution p of the front pump cavity can be realized f As a linear function; the rear pump cavity pressure distribution p is realized due to the fact that the rear pump cavity is extremely small in leakage r And is considered as a constant. Thus, the following calculation formula is derived:
F A1,i =F A1r,i -F A1f,i (1)
Figure BDA0003431701480000041
Figure BDA0003431701480000042
Figure BDA0003431701480000043
in the formulas (2) and (3), R is the distance from any point on the impeller cover plate in the radial direction to the axis, and the unit is m; r is R 2 =D 2 /2,R m =D m /2,R h =D h /2,D 2 Represents the impeller diameter, D m Diameter of the oral ring, D h Is the hub diameter. In the formula (4), ρ represents the density of the fluid mediumA degree; considering the leakage of the sealing of the mouth ring, the force acting on the front cover plate is corrected by adopting the coefficient k, wherein k is more than or equal to 0.8 and less than or equal to 0.9, and the specific rotation speed n s When the rotation speed is less than 150, k takes a small value of 0.8, and the specific rotation speed n s And k takes a large value of 0.9 when the k is larger than 150.
Specific rotation speed n s Calculated by the following formula (5):
Figure BDA0003431701480000051
in the formula (5), Q represents the flow rate, and the unit of Q is m 3 S; n represents the rotation speed, and H represents the single-stage lift.
Considering that the pre-rotation exists at the inlet of the secondary impeller, the single-stage performance is reduced, and the total cover plate force F A1 Calculated according to the following formula:
Figure BDA0003431701480000052
in the formula (6), F A1,1 Represents the axial force applied by the first-stage impeller, and m is more than or equal to 1 1 ≤1.2,0.96≤m 2 ≤1。
Second, the dynamic reaction force F is calculated by the following formula (7) A2
Figure BDA0003431701480000053
In the formula (7), Q represents the flow rate, and the unit of Q is m 3 S; n represents the number of stages of the segmental multistage centrifugal pump; d (D) 1 Representing the impeller inlet diameter; ρ represents the density of the fluid medium; 2.3<c<2.8, considering the unsteady flow in the impeller, adopting a coefficient c for correction, and taking a large value of 2.8 when the actual flow is not equal to the design flow, namely, when the actual flow deviates from the design working condition.
Third, the unbalanced force F acting on the pump shaft is calculated by the following formula (8) A3
Figure BDA0003431701480000054
In the formula (8), D h Represents the hub diameter; p is p 1 The suction pressure is designed to be a given value; p is p a Is at atmospheric pressure.
Fourth, the total axial force F is calculated by the following formula (9) A
F A =F A1 -F A2 +F A3 (9)
The pump stage number n=6 is taken as an example, and a single stage lift h=50m and a flow q=100deg.m are designed 3 /h, rotational speed n=2950r/min, D 1 =132mm,D 2 =220mm,D m =145mm,D h =80 mm, the suction pressure is atmospheric pressure. The medium is clear water, the density rho=1000 kg/m3, and the gravity acceleration g is 9.81m/s 2
(1) Calculating the cover plate force F A1
Specific rotation speed n s Taking k=0.8,
Figure BDA0003431701480000061
taking m 1 =1.05,m 2 =0.96,
F A1 =1.05×7743+0.96×5×7743=45297N
(2) Calculating dynamic reaction force F A2
Taking the value of c=2.5,
Figure BDA0003431701480000062
(3) Calculating unbalance force F acting on pump shaft A3
Figure BDA0003431701480000063
(4) Calculating the total axial force F A
F A =F A1 -F A2 +F A3 =45297-30447=14850N
The above example is more accurate by comparison with test and numerical simulation results.
The above description is only for the preferred embodiments of the present invention and is not intended to limit the present invention, but various modifications and variations can be made to the present invention by those skilled in the art.

Claims (3)

1. The multistage centrifugal pump axial force calculation method considering the leakage of the orifice ring is characterized by comprising the following steps of:
first step, calculate the cover force F A1
The axial force applied by the single-stage impeller is F A1,i Is an axial force F acting on the front cover plate A1f,i And an axial force F acting on the back plate A1r,i The difference between the front pump cavity pressure distribution p f The rear pump chamber pressure profile p is considered as a linear function r Considered as a constant, calculated by the following formula:
F A1,i =F A1r,i -F A1f,i (1)
Figure QLYQS_1
Figure QLYQS_2
Figure QLYQS_3
in the formulas (2) and (3), R is the distance from any point on the impeller cover plate in the radial direction to the axis, and the unit is m; r is R 2 =D 2 /2,R m =D m /2,R h =D h /2,D 2 Represents the impeller diameter, D m Diameter of the oral ring, D h Is the diameter of the hub; in formula (4), ρ represents the density of the fluid medium; k (k)Is a correction coefficient; g represents gravitational acceleration;
specific rotation speed n s Calculated by the following formula (5):
Figure QLYQS_4
in the formula (5), Q represents the flow rate, and the unit of Q is m 3 S; n represents the rotating speed, and H represents the single-stage lift;
total cover force F A1 Calculated according to the following formula (6):
Figure QLYQS_5
in the formula (6), F A1,1 Represents the axial force applied by the first-stage impeller, and m is more than or equal to 1 1 ≤1.2,0.96≤m 2 ≤1;
Second, the dynamic reaction force F is calculated by the following formula (7) A2
Figure QLYQS_6
In the formula (7), Q represents the flow rate, and the unit of Q is m 3 S; n represents the number of stages of the segmental multistage centrifugal pump; d (D) 1 Representing the impeller inlet diameter; ρ represents the density of the fluid medium; c is a correction coefficient;
third, the unbalanced force F acting on the pump shaft is calculated by the following formula (8) A3
Figure QLYQS_7
In the formula (8), D h Represents the hub diameter; p is p 1 The suction pressure is designed to be a given value; p is p a Is at atmospheric pressure;
fourth, the total axial force F is calculated by the following formula (9) A
F A =F A1 -F A2 +F A3 (9)。
2. The method for calculating axial force of multistage centrifugal pump taking into account leakage of orifice ring according to claim 1, wherein k is 0.8.ltoreq.k.ltoreq.0.9, specific rotation speed n s When the rotation speed is less than 150, k takes a small value of 0.8, and the specific rotation speed n s And k takes a large value of 0.9 when the k is larger than 150.
3. The method for calculating the axial force of the multistage centrifugal pump considering the leakage of the orifice ring according to claim 2, wherein c is 2.8 which is a large value when the actual flow is not equal to the design flow, and c is 2.3< c < 2.8.
CN202111600797.5A 2021-12-24 2021-12-24 Multistage centrifugal pump axial force calculation method considering mouth ring leakage Active CN114329828B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111600797.5A CN114329828B (en) 2021-12-24 2021-12-24 Multistage centrifugal pump axial force calculation method considering mouth ring leakage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111600797.5A CN114329828B (en) 2021-12-24 2021-12-24 Multistage centrifugal pump axial force calculation method considering mouth ring leakage

Publications (2)

Publication Number Publication Date
CN114329828A CN114329828A (en) 2022-04-12
CN114329828B true CN114329828B (en) 2023-06-13

Family

ID=81012928

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111600797.5A Active CN114329828B (en) 2021-12-24 2021-12-24 Multistage centrifugal pump axial force calculation method considering mouth ring leakage

Country Status (1)

Country Link
CN (1) CN114329828B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117034502B (en) * 2023-09-04 2024-01-12 浙江大学 Axial force calculation method for mechanical seal in multistage centrifugal pump

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102322443A (en) * 2011-09-08 2012-01-18 浙江工业大学 Single-stage centrifugal pump with balanced axial force
CN104196752A (en) * 2013-12-31 2014-12-10 江苏大学 Multi-working-condition hydraulic design method of centrifugal pump with eccentrically placed impeller
CN107461361A (en) * 2017-09-20 2017-12-12 江苏大学 A kind of design method of multistage pump first-stage double suction impeller
CN108223459A (en) * 2017-06-23 2018-06-29 闫龙 The stuck method for maintaining of multistage Rule pumping hole ring is solved using the not mode of disintegrating

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10859084B2 (en) * 2016-04-26 2020-12-08 Onesubsea Ip Uk Limited Subsea process lubricated water injection pump

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102322443A (en) * 2011-09-08 2012-01-18 浙江工业大学 Single-stage centrifugal pump with balanced axial force
CN104196752A (en) * 2013-12-31 2014-12-10 江苏大学 Multi-working-condition hydraulic design method of centrifugal pump with eccentrically placed impeller
CN108223459A (en) * 2017-06-23 2018-06-29 闫龙 The stuck method for maintaining of multistage Rule pumping hole ring is solved using the not mode of disintegrating
CN107461361A (en) * 2017-09-20 2017-12-12 江苏大学 A kind of design method of multistage pump first-stage double suction impeller

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
"叶轮背叶片对离心泵轴向力影响的试验及分析";刘在伦 等;《排灌机械工程学报》;第37卷(第12期);1013-1018 *

Also Published As

Publication number Publication date
CN114329828A (en) 2022-04-12

Similar Documents

Publication Publication Date Title
EP1717449B1 (en) A centrifugal pump and an impeller thereof
Hamrick et al. Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
CN114329828B (en) Multistage centrifugal pump axial force calculation method considering mouth ring leakage
CN111368372B (en) Method for calculating axial force of semi-open impeller of centrifugal compressor
CN109253113A (en) Volute Profile of Multi-blade Centrifugal Fan design method used for range hood and its multi-wing centrifugal fan spiral case
CN109083864A (en) A kind of radial-flow type rotating machinery impeller
CN111720356A (en) Axial thrust balancing method of semi-open type centrifugal compressor
Benra et al. Calculation of hydrodynamic forces and flow induced vibrations of centrifugal sewage water pumps
CN107524627B (en) Static pressure radial impeller and its design method
Day et al. Effect of Reynolds number on performance of a small centrifugal pump
Dai et al. A hydraulic performance comparison of centrifugal pump operating in pump and turbine modes
Kearton The influence of the number of impeller blades on the pressure generated in a centrifugal compressor and on its general performance
CN210637242U (en) Multistage pump flow-induced vibration suppression device
CN115438441A (en) Centrifugal compressor impeller quasi-three-dimensional design method based on inverse design algorithm
CN117034502B (en) Axial force calculation method for mechanical seal in multistage centrifugal pump
CN111680372A (en) One-dimensional calculation method considering working capacity of centrifugal fan impeller in natural prerotation
CN109711047B (en) Design method for aerodynamic performance of S2 flow surface of helium compressor
JP4079740B2 (en) Axial fluid machine
Deniz et al. Modification of Pump Turbine Characteristics With Fluid Injection in Pump Operating Mode
Son et al. Spiral casing of a volute centrifugal pump: Effects of varying the cross-sectional area
Tsukamoto et al. Effect of Impeller Outlet Flow Affected by Casing Treatment on Rotating Stall in Vane-Less Diffuser in Centrifugal Turbomachinery
CN219605634U (en) Centrifugal pump impeller with curved back vane structure
Zeng et al. Numerical investigation of pressure pulsation in vaneless region of a high speed centrifugal pump
Tsukamoto et al. Effect of curvilinear element blade for open-type centrifugal impeller on stator performance
Hiradate et al. Experimental investigation on unstable flow in multi-stage centrifugal blower with inlet guide vane

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