CN110083924A - Film lubrication performance simulation method under hydrostatic thrust bearing unbalance loading operating condition - Google Patents

Film lubrication performance simulation method under hydrostatic thrust bearing unbalance loading operating condition Download PDF

Info

Publication number
CN110083924A
CN110083924A CN201910332243.8A CN201910332243A CN110083924A CN 110083924 A CN110083924 A CN 110083924A CN 201910332243 A CN201910332243 A CN 201910332243A CN 110083924 A CN110083924 A CN 110083924A
Authority
CN
China
Prior art keywords
block
oil
option
setting
film
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
CN201910332243.8A
Other languages
Chinese (zh)
Other versions
CN110083924B (en
Inventor
于晓东
王宇
伍广鹏
周文凯
毕宏伟
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.)
Harbin University of Science and Technology
Original Assignee
Harbin University of Science and 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 Harbin University of Science and Technology filed Critical Harbin University of Science and Technology
Priority to CN201910332243.8A priority Critical patent/CN110083924B/en
Publication of CN110083924A publication Critical patent/CN110083924A/en
Application granted granted Critical
Publication of CN110083924B publication Critical patent/CN110083924B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2119/00Details relating to the type or aim of the analysis or the optimisation
    • G06F2119/06Power analysis or power optimisation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Evolutionary Computation (AREA)
  • Computer Hardware Design (AREA)
  • General Engineering & Computer Science (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Computational Mathematics (AREA)
  • Sliding-Contact Bearings (AREA)

Abstract

Oil film performance simulation method under hydrostatic thrust bearing unbalance loading operating condition, the invention mainly relates to the analogy methods of film lubrication performance under double square chamber hydrostatic thrust bearing unbalance loading operating condition.The invention solves hydrostatic thrust bearings under unbalance loading operating condition without actually active method come the problem of simulating film lubrication performance.This method is to pass through: 1, establishing 6 symmetrical double square lubricating pad models by UG;2, model is imported in ANSYS ICEM CFD software, creates Fuel film model part, create topological structure partition structure grid;3, check whether the Points And lines of model are all associated with the point of block with line;4, grid division number of nodes, the encryption of oil inlet number of nodes;5, boundary film condition is set in ANSYS CFX software;6, convergence uses the standard of ANSYS CFX software default, judges whether fluctuation is stable.The present invention is applied to greasy property simulation field under hydrostatic thrust bearing unbalance loading operating condition.

Description

Film lubrication performance simulation method under hydrostatic thrust bearing unbalance loading operating condition
Technical field
It is inclined in particular for double square chamber the present invention relates to a kind of analogy method of hydrostatic thrust bearing film lubrication performance The analogy method of film lubrication performance when load.
Background technique
Hydrostatic thrust bearing is one of the kernel component of heavy type numerical control process equipment, its performance is better, and equipment adds Working medium amount and operational efficiency are higher.In the ideal situation, the mass center of workpiece should carry center at the center of rotary table Load, hydrostatic thrust bearing working condition is in optimum performance state at this time.But in the actual processing process, the mass center of workpiece can The case where unbalance loading can not occur at the center of rotary table, keep hydrostatic thrust bearing oil film locally thinning, or even occur dry Friction, so as to cause hydrostatic thrust bearing failure, this problem restricts China's heavy type numerical control process equipment in high precision, efficiently The direction of rate is developed.And both at home and abroad be directed to unbalance loading when hydrostatic thrust bearing film lubrication behavior pattern analogy method research compared with It is few, therefore it is very necessary for studying new hydrostatic thrust bearing analogy method of greasy property in unbalance loading operating condition, is also quiet The design that advanced optimizes of pressure thrust bearing provides foundation.
Summary of the invention
The purpose of the present invention is to solve hydrostatic thrust bearing is in practical work process, workpiece mass center and revolution Work table rotation center, which is not overlapped, there is unbalance loading, and oil film thickness becomes uneven distribution, so as to cause hydrostatic thrust bearing lubricity It can be greatly reduced or even be occurred dry friction, lack a kind of effective method come the problem of simulation to this phenomenon.In order to The greasy property for probing into hydrostatic thrust bearing oil film in unbalance loading proposes a kind of hydrostatic bearing film lubrication performance in unbalance loading Analogy method.
The analogy method of greasy property when hydrostatic thrust bearing unbalance loading is achieved through the following technical solutions.
(1), 6 symmetrical double square lubricating pad threedimensional models are established by UG 3 d modeling software;
(2), model is imported in ANSYS ICEM CFD software, face required for splitting creates Fuel film model part, and creation is opened up Flutter structure partition structure grid;
(3), check whether the Points And lines of model are all associated with the point of block with line, if block all lines are all green Color then all in association, otherwise without all associations, therefore need to be associated by above-mentioned steps again;
(4), grid division number of nodes;The encryption of oil inlet number of nodes, adjacent segments points are no more than twice, guarantee grid matter with this Amount;
(5), boundary film condition, the setting of setting and domain including viscous kelvin relation are set in ANSYS CFX software;
(6), convergence uses the standard of ANSYS CFX software default, i.e. residual values are lower than 10-4, judge whether fluctuation is stable, has Without apparent downward trend.
The present invention can simulate actual condition of the hydrostatic thrust bearing when unbalance loading occurs for workpiece by computer, obtain The film lubrication parameter of hydrostatic thrust bearing under different unbalance loading degree.This method can save the plenty of time, obtain and tie with experiment The film lubrication parameter that fruit is consistent.By studying lubricating oil film parameter, different unbalance loading degree are disclosed to film lubrication characteristic Affecting laws.This provides effective reference frame for the further optimizing research of hydrostatic thrust bearing, also to use static pressure The heavy equipment of thrust bearing realizes high efficiency, has established solid foundation in high precision.
Detailed description of the invention
Fig. 1 is film lubrication performance simulation method flow diagram under hydrostatic thrust bearing unbalance loading operating condition.
Fig. 2 is the Fuel film model under the unbalance loading operating condition that step A is mentioned.
Fig. 3 is list after the definition Part that step B1 is mentioned.
Fig. 4 is the oil film network topology illustraton of model that step B2 is mentioned.
Fig. 5 is the oil film grid dividing figure that step C is mentioned.
Fig. 6 is the oil film mesh quality schematic diagram that step D is mentioned.
Fig. 7 is the oil film each position setting that step E is mentioned.
Fig. 8 is the iteration residual plot that step F is mentioned.
Specific embodiment
It can be achieved through the following technical solutions,
Step A: the lubricating pad under unbalance loading operating condition is modeled using UG software, is created that different shape size according to different operating conditions Model.
Step B1: the Fuel film model under established different operating conditions is exported as into .x.t file using UG software, will be exported .x.t file imported into ANSYS ICEM CFD software, setting unit mm;Since CFD software can not will be established in UG Face is divided into two faces automatically, so what is done first after model importing is that the face in UG is split as required face;Secondly Be create Fuel film model part, the step for mainly for import CFX back boundary condition setting, part be set with IN1, IN2, OUT1, OUT2, OUT3, OUT4, INTERFACE1, INTERFACE 2, these definition faces ROTATE, WALL.
Step B2: top-down division methods are used when creation topological structure partition structure grid.First click on option Blocking selects Check Block option, selects the subtopology structure in split block, first draws to X-direction block Point, then Y, Z-direction block are divided, delete unnecessary topological structure.When creation point mapping, by each top of threedimensional model Point is successively mapped in the vertex of block, and the Auto association that line mapping can directly select in Blocking is closed automatically Join option, completes the mapping of oil film and oil pocket Points And lines.
Step B3: the shape of oil inlet is cylinder, then grid should use O-shaped grid, individually be divided to its block, Two points are dosed at the symmetrical position of circle first, the block of X, Y-direction is divided, then select Check Block option By following rectangular block it is stretched come, and then obtain the block of rectangular shape, when mapping, quadrangle be mapped to Circle.The Select face option in Split Block is finally clicked, the top and bottom of cylinder are selected, clicks and determines, so far complete All block are divided and dotted line mapping.
Step C: checking whether the Points And lines of model are all associated with the Points And lines of block, will be under Geometry Point and edge hides, and checks whether the line of block is all green.If it is, all in association;If somewhere is not Be it is green, show herein without that therefore need to be associated again by above-mentioned steps in association.
Step D: Mesh Quality module is clicked, oil film grid and angle mesh quality are checked.Export grid Shi Caiyong Output/Select Solver selects ANSYS CFX solver, and default output file format is .CFX5.
Step E1: selection ANSYS CFX software carries out simulation analysis to oil film.Fluid domain is set as FLUID, is selected Material is 32# lubricating oil, and fluid calculation model is selected as total energy, temperature setting 293K, other settings are kept Default setting.
Step E2: the setting of oil inlet Inlet.The flow of inlet porting IN1 and IN2 are 0.035, and temperature is given as room temperature 293K i.e. 20 DEG C.
Step E3: four oil outlets, respectively OUT1, OUT2, OUT3, OUT4, phase is arranged in the setting of oil outlet Outlet It is 0Pa to atmospheric pressure.
Step E4: clicking Interface, and Interface Type selects Fluid, interface Interface side1 choosing Item selection INTERFACE1, interface Iterfance side2 select option INTERFACE2, and Rtation Axis rotary shaft is Z axis, selects GGI grid connecting method in Mesh connecion option, and periodical axial-radial tolerance is 0.0001.
Step E5: the setting of wall surface Wall, oil film upper surface are rotating face, are set as Rotate Wall, under oil film The face and oil pocket inner wall that surface is in contact with lubricating pad are both configured to Wall.
The setting of step E6:ROTATE: Option option selects Rotating Wall, rotates to rotate axis selection Z axis global Z, revolving speed is 100r/min to setting rotary table about the z axis, completes the setting of Oil Boundary condition.
Step F: the convergence of use is the standard of ANSYS CFX software default, i.e., residual values are already below 10-4, and And fluctuation situation is stablized, without apparent downward trend.

Claims (1)

1. the analogy method of film lubrication performance under hydrostatic thrust bearing unbalance loading operating condition, it is characterised in that hydrostatic thrust bearing unbalance loading Operating condition Imitating method is realized according to the following steps:
Step A: the lubricating pad under unbalance loading operating condition is modeled using UG software, is created that different shape size according to different operating conditions Model;
Step B1: exporting as .x.t file for the Fuel film model under established different operating conditions using UG software, will be derived .x.t file is imported into ANSYS ICEM CFD software, setting unit mm;The face that can not will be established in UG due to CFD software Automatically two faces are divided into, so what is done first after model importing is that the face in UG is split as required face;Followed by Create the part of Fuel film model, the step for be setting in order to import CFX back boundary condition, part be set with IN1, IN2, OUT1, OUT2, OUT3, OUT4, INTERFACE1, INTERFACE 2, these definition faces ROTATE, WALL;
Step B2: top-down division methods are used when creation topological structure partition structure grid, first click on option Blocking selects Check Block option, selects the subtopology structure in split block, first draws to X-direction block Point, then Y, Z-direction block are divided, unnecessary topological structure is deleted, when creation point maps, by each top of threedimensional model Point is successively mapped in the vertex of block, and the Auto association that line mapping can directly select in Blocking is closed automatically Join option, completes the mapping of oil film and oil pocket Points And lines;
Step B3: the shape of oil inlet is cylinder, then grid should use O-shaped grid, individually be divided to its block, first Two points are dosed at the symmetrical position of circle, the block of X, Y-direction is divided, then select Check Block option will under The rectangular block in face it is stretched come, and then obtain the block of rectangular shape, when mapping, quadrangle be mapped to circle, most The Select face option in Split Block is clicked afterwards, selects the top and bottom of cylinder, is clicked and is determined, so far completes all Block is divided and dotted line mapping;
Step C: checking whether the Points And lines of model are all associated with the Points And lines of block, by under Geometry point and Edge hides, and checks whether the line of block is all green, if it is, all in association;If somewhere is not green , show in no association herein, therefore need to be associated again by above-mentioned steps;
Step D: clicking Mesh Quality module, check oil film grid and angle mesh quality, adopts when exporting grid ANSYS CFX solver is selected with Output/Select Solver, default output file format is .CFX5;
Step E1: selection ANSYS CFX software carries out simulation analysis to oil film, sets fluid domain as FLUID, selects material For 32# lubricating oil, fluid calculation model is selected as total energy, temperature setting 293K, other settings keep default Setting;
Step E2: the setting of oil inlet Inlet, the flow of inlet porting IN1 and IN2 are 0.035, and temperature is given as room temperature 293K I.e. 20 DEG C;
Step E3: four oil outlets, respectively OUT1, OUT2, OUT3, OUT4 are arranged in the setting of oil outlet Outlet, relatively large Air pressure is 0Pa;
Step E4: clicking Interface, and Interface Type selects Fluid, the choosing of interface Interface side1 option INTERFACE1 is selected, interface Iterfance side2 selects option INTERFACE2, and Rtation Axis rotary shaft is Z axis, GGI grid connecting method is selected in Mesh connecion option, periodical axial-radial tolerance is 0.0001;
Step E5: the setting of wall surface Wall, oil film upper surface are rotating face, are set as Rotate Wall, oil film lower surface The face and oil pocket inner wall being in contact with lubricating pad are both configured to Wall;
The setting of step E6:ROTATE: Option option selects Rotating Wall, rotates to rotate axis selection Z axis Global Z, revolving speed is 100r/min to setting rotary table about the z axis, completes the setting of Oil Boundary condition;
Step F: the convergence of use is the standard of ANSYS CFX software default, i.e., residual values are already below 10-4, and wave Emotionally condition is stablized, without apparent downward trend.
CN201910332243.8A 2019-04-23 2019-04-23 Oil film lubrication performance simulation method under static pressure thrust bearing unbalance loading working condition Active CN110083924B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910332243.8A CN110083924B (en) 2019-04-23 2019-04-23 Oil film lubrication performance simulation method under static pressure thrust bearing unbalance loading working condition

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910332243.8A CN110083924B (en) 2019-04-23 2019-04-23 Oil film lubrication performance simulation method under static pressure thrust bearing unbalance loading working condition

Publications (2)

Publication Number Publication Date
CN110083924A true CN110083924A (en) 2019-08-02
CN110083924B CN110083924B (en) 2022-05-27

Family

ID=67416395

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910332243.8A Active CN110083924B (en) 2019-04-23 2019-04-23 Oil film lubrication performance simulation method under static pressure thrust bearing unbalance loading working condition

Country Status (1)

Country Link
CN (1) CN110083924B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111666644A (en) * 2020-06-18 2020-09-15 哈尔滨工业大学 Performance analysis method for parameterized CFD aerostatic bearing
CN113158369A (en) * 2021-04-19 2021-07-23 哈尔滨理工大学 Oil film flow simulation monitoring method for oil seal edge of hydrostatic thrust bearing oil pad
CN113742978A (en) * 2021-11-08 2021-12-03 哈尔滨理工大学 Friction failure prediction method for oil pad inclinable hydrostatic thrust bearing under extreme working condition

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102141084A (en) * 2011-03-30 2011-08-03 哈尔滨理工大学 Numerical simulation method for temperature and thickness relation of static thrust bearing gap oil film based on film thickness variation
US20150023785A1 (en) * 2013-07-19 2015-01-22 Michael J. Stanko Coupling for directly driven compressor
US9169728B2 (en) * 2011-12-08 2015-10-27 General Electric Company Dynamic load reduction system
CN105135197A (en) * 2015-09-02 2015-12-09 哈尔滨理工大学 Lubricating property forecasting method of double-rectangular-cavity hydrostatic thrust bearing
CN106594076A (en) * 2016-12-07 2017-04-26 北京工业大学 Dynamic and static pressure mixed fan-shaped oil pad
CN109117522A (en) * 2018-07-24 2019-01-01 北京工业大学 A kind of calculation method of the static-pressure slide carriage fluid structurecoupling working performance based on MATLAB-ANSYS software

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102141084A (en) * 2011-03-30 2011-08-03 哈尔滨理工大学 Numerical simulation method for temperature and thickness relation of static thrust bearing gap oil film based on film thickness variation
US9169728B2 (en) * 2011-12-08 2015-10-27 General Electric Company Dynamic load reduction system
US20150023785A1 (en) * 2013-07-19 2015-01-22 Michael J. Stanko Coupling for directly driven compressor
CN105135197A (en) * 2015-09-02 2015-12-09 哈尔滨理工大学 Lubricating property forecasting method of double-rectangular-cavity hydrostatic thrust bearing
CN106594076A (en) * 2016-12-07 2017-04-26 北京工业大学 Dynamic and static pressure mixed fan-shaped oil pad
CN109117522A (en) * 2018-07-24 2019-01-01 北京工业大学 A kind of calculation method of the static-pressure slide carriage fluid structurecoupling working performance based on MATLAB-ANSYS software

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
YU XIAODONG 等: ""Research on the pressure field of hydrostatic center rest"", 《PROCEEDINGS OF 2011 INTERNATIONAL CONFERENCE ON ELECTRONIC & MECHANICAL ENGINEERING AND INFORMATION TECHNOLOGY》, 19 September 2011 (2011-09-19), pages 458 - 461 *
于晓东 等: ""极端工况双矩形腔静压推力轴承动态特性"", 《力学学报》, vol. 50, no. 4, 13 May 2018 (2018-05-13), pages 1085 - 1091 *
于晓东 等: ""极端工况静压推力轴承承载性能动压补偿"", 《推进技术》, vol. 39, no. 5, 2 April 2018 (2018-04-02), pages 899 - 907 *
于晓东等: "环形腔多油垫静压推力轴承热变形", 《吉林大学学报(工学版)》, vol. 45, no. 2, 15 March 2015 (2015-03-15), pages 125 - 130 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111666644A (en) * 2020-06-18 2020-09-15 哈尔滨工业大学 Performance analysis method for parameterized CFD aerostatic bearing
CN113158369A (en) * 2021-04-19 2021-07-23 哈尔滨理工大学 Oil film flow simulation monitoring method for oil seal edge of hydrostatic thrust bearing oil pad
CN113158369B (en) * 2021-04-19 2023-11-28 哈尔滨理工大学 Oil film flow simulation monitoring method for oil sealing edge of oil pad of hydrostatic thrust bearing
CN113742978A (en) * 2021-11-08 2021-12-03 哈尔滨理工大学 Friction failure prediction method for oil pad inclinable hydrostatic thrust bearing under extreme working condition

Also Published As

Publication number Publication date
CN110083924B (en) 2022-05-27

Similar Documents

Publication Publication Date Title
CN110083924A (en) Film lubrication performance simulation method under hydrostatic thrust bearing unbalance loading operating condition
CN102141084B (en) Numerical simulation method for temperature and thickness relation of static thrust bearing gap oil film based on film thickness variation
CN103020393B (en) Aircraft assembly data visualization method based on Web
CN109855238A (en) A kind of modeling of central air-conditioning and efficiency optimization method and device
CN107341288B (en) Optimization method for controlling vibration of combined cycle unit by adjusting elevation of bearing
CN112487734B (en) CFD numerical simulation method for air system structure
CN109471377A (en) Based on two twin axis X-Y leather and fur products Cutting machine control methods of number
CN105046432A (en) Building dimensional guide construction method
WO2023138013A1 (en) Method and system for computing power gridding in multi-cloud scene
CN105893695A (en) Through-flow clearance error compensation method for small-size turbine in cylinder combination state
CN104615801B (en) The heavy critical lubricating status tachometer value of hydrostatic bearing determines method
US6526550B1 (en) Analyzing characteristics of geometries
CN107526914B (en) Variable-watershed flow field calculation method of tilting-pad sliding bearing based on structured dynamic grid
CN113111453B (en) Numerical simulation simplifying method for drag reduction performance of micro-texture of rotating blade
CN112949112B (en) Rotor-sliding bearing system lubrication basin dynamic grid parallel computing method
CN109063223B (en) BIM model light weight method and device and BIM model processing method and system
CN114155341A (en) Cross-platform consistency method for three-dimensional model of large-scale digital workshop based on Unity platform
CN116702374A (en) Turbine pump sealing structure design method, device and equipment
CN102902769A (en) Database benchmark test system of cloud computing platform and method thereof
CN104598666A (en) Large-scale hydrostatic support critical load parameter acquiring method
CN112711889B (en) Dynamic heat-fluid-solid simulation method based on LS-DYNA software
CN114840946B (en) Dynamic pressure type mechanical seal reliability calculation method based on liquid film vaporization phase transition
CN115601548A (en) Cutting method for CFD analysis rotating domain of rotating machine
CN114528657A (en) Energy loss dimensionality reduction coupling method and system, computer equipment and readable storage medium
CN104731051A (en) Method for achieving sensor point position objectification

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