CN105843999A - Finite element simulative analysis method for spline connection anti-rolling torsion bars - Google Patents

Finite element simulative analysis method for spline connection anti-rolling torsion bars Download PDF

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CN105843999A
CN105843999A CN201610157334.9A CN201610157334A CN105843999A CN 105843999 A CN105843999 A CN 105843999A CN 201610157334 A CN201610157334 A CN 201610157334A CN 105843999 A CN105843999 A CN 105843999A
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spline
model
submodel
geometric model
finite element
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CN105843999B (en
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曾晶晶
卜继玲
王京雁
王永冠
张亚新
罗燕
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Zhuzhou Times New Material Technology Co Ltd
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    • 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]

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Abstract

The invention discloses a method for carrying out strength analysis and fatigue life verification on spline connection anti-rolling torsion bars. The method comprises the following steps: 1) establishing a geometric model; 2) carrying out meshing, setting binding constraints between spline tooth pairs in finite element analysis software and submitting analytical calculation to obtain a preliminary calculation result; 3) carrying out cutting to obtain a sub-model with spline tooth pairs and tool withdrawal groove characteristics; 4) meshing the sub-model, carrying out node-merging on meshes between the spline tooth pairs of the sub-model, setting interference contact between the spline tooth pairs, importing the preliminary calculation result, applying surface force on the cutting surface of the sub-model to carry out driving, and submitting analytical calculation to obtain a final calculation result of the sub-model; 5) carrying out fatigue life verification on the final calculation result of the sub-model. According to the method disclosed in the invention, the analysis speed and analysis precision of finite element analysis can be ensured, the fatigue life verification cost can be reduced and much research and development cost can be saved.

Description

A kind of Finite Element Simulation Analysis method coupling anti-side rolling torsion rod for spline
Technical field
The present invention relates to spline and couple anti-side rolling torsion rod intensity analysis and Verification Technology fatigue life, be specifically related to a kind of for spline Couple the Finite Element Simulation Analysis method of anti-side rolling torsion rod.
Background technology
EMU, passenger vehicle etc. all have employed air spring and open and improve Vertical Vibration of Vehicle performance, makes the angle of car body rolling Rigidity becomes flexible relative, but this also makes the angle of heel angular displacement of car body in operation increase, and brings serious potential safety hazard.For this Bogie Frames of High Speed Passenger Car is all provided with anti-side rolling torsion rod while using air spring both at home and abroad.Anti-side rolling torsion rod by torsion bar shaft, Reverse arm forms, and wherein torsion bar shaft is main stressed member.When car body sidewinders, two reverse arms of horizontal positioned are for torsion bar There is the effect of a mutually opposing power and moment respectively, make twiot arm bear moment of torsion and produce elasticity of torsion deformation, with car body Produce the in opposite direction, to retrain the rolling of car body of angle of roll angular displacement.Torsion bar shaft mainly has with the connecting mode of reverse arm Interference fit joint couples with spline.Interference fit joint typically uses the method one-shot forming of the temperature difference, simple and reliable process, but the most quick detachable, Affect operation maintenance maintenance efficiency;Spline couples and typically is made up of internal spline and external splines, be commonly applied to transmit bigger torque with Centering precision requires high quiet connection and dynamic connection, uses spline to couple and then can dismantle replacement, and can preferably transmit moment.
At present in the anti-side rolling torsion rod design phase, finite element analysis technology all can be utilized to carry out intensity analysis and fatigue life checks. But when at present anti-side rolling torsion rod being carried out finite element analysis, generally there are following shortcoming: (I) is due in torsion bar shaft and reverse arm There is spline tooth and escape labyrinth feature, general employing C3D4 grid cell divides, in order to obtain accurately Result, grid is finely divided, makes the number of grid of structure increase, cause that number of grid is big, computational efficiency is low, analysis and solution Time is long.(II) many to contact surface due to spline tooth, convergence is very poor, spline tooth between adopt the method for binding constraints, impact Analysis precision, it is impossible to accurately calculate the stress value at spline tooth and escape, accuracy in computation is low.(III) existing spline connection Check fatigue life connecing anti-side rolling torsion rod is usually carried out on testing stand, and the fatigue load of anti-side rolling torsion rod is designed as 10,000,000 Secondary, the loading frequency of testing stand is generally 2Hz, and therefore, the time that the fatigue life of a set of spline anti-side rolling torsion rod checks is 1388 Individual hour, need substantial amounts of time and expense.In sum, how to improve spline and couple the analysis efficiency of anti-side rolling torsion rod, ask The accuracy solved, reduces the expense checked fatigue life, it has also become the technical problem that those skilled in the art are urgently to be resolved hurrily.
Summary of the invention
The technical problem to be solved in the present invention: for the problems referred to above of prior art, it is provided that one ensure that finite element analysis divides Analysis speed and analysis precision, reduce and check expense fatigue life, and that saves substantial amounts of R&D costs couples anti-side rolling torsion for spline The Finite Element Simulation Analysis method of bar.
In order to solve above-mentioned technical problem, the technical solution used in the present invention is:
A kind of spline couples anti-side rolling torsion rod intensity analysis and check method fatigue life, and step includes:
1) set up spline and couple the geometric model of anti-side rolling torsion rod;
2) described geometric model employing C3D4 grid cell is carried out stress and strain model;Geometric model after carrying out stress and strain model exists In finite element analysis software by spline tooth between binding constraints is set and submits analytical calculation to, obtain described spline couple anti-side rolling The primary Calculation result of torsion bar intensity;
3) described geometric model is cut, obtain remaining with spline tooth to and the submodel of relief groove structure feature;
4) described submodel employing C3D8R grid cell is carried out stress and strain model;Submodel after carrying out stress and strain model is being had Grid between spline tooth pair is realized conode by finite element analysis software, Interference contact is set by between spline tooth pair, import described tentatively Result of calculation, applies face power on the facet of described submodel and is driven and submits analytical calculation to, obtain described submodel Final calculation result;
5) final calculation result for described submodel carries out check fatigue life.
Preferably, described step 2) detailed step include:
2.1) C3D4 grid cell is used to carry out stress and strain model for described geometric model;
2.2) geometric model after carrying out stress and strain model imports finite element analysis software;
2.3) in described finite element analysis software, C3D4 grid cell is used to carry out stress and strain model described geometric model, and The size of mesh opening encryption at spline tooth and escape position, the grid at remaining position in described geometric model are carried out free size amplification;
2.4) to described geometric model imposed load and boundary condition in finite element analysis software, turning round for described geometric model Apply vertical load on pivoted arm, retrain mounting seat, Interference contact is set by between spline tooth pair, quickly submits calculating to, obtain described Spline couples the primary Calculation result of anti-side rolling torsion rod intensity.
Preferably, described step 3) in described geometric model cut specifically refer to carry out at the position concentrated away from stress Cutting, obtain remaining with spline tooth to and the submodel of relief groove structure feature.
Preferably, described step 5) specifically use fe-safe software to carry out check fatigue life.
Preferably, described step 5) detailed step include: the final calculation result of described submodel is imported fe-safe software And the stress value of final step in each analysis step of the final calculation result extracting described submodel;Fe-safe software is arranged Fatigue load, load history, number of times fatigue life, surface roughness, material parameter, tired algorithm also submit calculating to, obtain Result of calculation file;Described result of calculation file is imported in finite element analysis software, checks life-span cloud atlas and stress intensity factor Cloud atlas FOS, described stress intensity factor cloud atlas FOS characterize the intensity factor S of imposed load, when the value of intensity factor S is more than Or during equal to 1, it is determined that the fatigue load arranged in fe-safe software under the conditions of current projected life is safe.
Spline of the present invention couples anti-side rolling torsion rod intensity analysis and check method fatigue life has an advantage that
1, the present invention is directed to torsion bar geometric model uses C3D4 grid cell to carry out stress and strain model in finite element analysis software, will Spline tooth between binding constraints is set and submits analytical calculation to, obtain spline couple anti-side rolling torsion rod intensity primary Calculation result, Number of grid can be controlled, improve analysis efficiency.
2, the present invention uses the method for submodel to carry out secondary calculating, the cutting of torsion bar geometric model is obtained submodel, retains spline Tooth to and relief groove structure feature, use C3D8R stress and strain model, and realize grid conode, spline tooth between use interference The mode of contact, improves accuracy of analysis, it is ensured that the analysis efficiency of its finite element analysis.
3, the present invention uses the method for finite element that anti-side rolling torsion rod carries out check fatigue life, reduces control experiment fatigue life and takes With, save substantial amounts of R&D costs.
Accompanying drawing explanation
Fig. 1 is the basic flow sheet of embodiment of the present invention method.
Fig. 2 is embodiment of the present invention step 1) the geometric model schematic diagram set up.
Fig. 3 is embodiment of the present invention step 2) grid model of geometric model that obtains after gridding.
Fig. 4 is embodiment of the present invention step 3) cut the submodel schematic diagram obtained.
Fig. 5 is embodiment of the present invention step 4) the submodel grid model that obtains after gridding
Fig. 6 is that the embodiment of the present invention arranges interface schematic diagram in applying face, submodel border power.
Fig. 7 is the interface schematic diagram that the embodiment of the present invention extracts stress value in fe-safe.
Fig. 8 is the embodiment of the present invention interface schematic diagram at load defined in fe-safe and loading sequence.
Fig. 9 is that the embodiment of the present invention is at fe-safe software design patterns analysis of fatigue bound of parameter face schematic diagram.
Figure 10 is the S-N curve of the material quoted in the embodiment of the present invention.
Figure 11 is the stress intensity factor cloud atlas FOS that embodiment of the present invention analysis obtains.
Figure 12 is the life-span cloud atlas that embodiment of the present invention analysis obtains.
Figure 13 is the fracture that embodiment of the present invention kind spline couples anti-side rolling torsion rod.
Detailed description of the invention
Hereafter will couple as a example by anti-side rolling torsion rod by certain spline, spline of the present invention will be coupled anti-side rolling torsion rod intensity analysis and tired longevity The detailed description of the invention of life check method is described in further detail.
As it is shown in figure 1, the step that the present embodiment spline couples anti-side rolling torsion rod intensity analysis and check method fatigue life includes:
1) set up spline and couple the geometric model of anti-side rolling torsion rod.
In the present embodiment, step 1) specifically use PTC Creo software to set up the geometric model of spline connection anti-side rolling torsion rod.
As in figure 2 it is shown, the geometric model setting up spline connection anti-side rolling torsion rod in the present embodiment includes torsion bar shaft 1, mounting seat 2 With reverse arm 3, two sections of torsion bar shaft 1 are respectively and fixedly provided with a mounting seat 2, and are arranged with a reverse arm 3 in mounting seat 2, peace Dress seat 2 and reverse arm 3 between be provided with spline tooth to and use spline to couple.
2) geometric model use C3D4 grid cell carry out stress and strain model;The geometric model after stress and strain model will be carried out limited In meta-analysis software by spline tooth between binding constraints is set and submits analytical calculation to, obtain spline couple anti-side rolling torsion rod intensity Primary Calculation result;
In the present embodiment, step 2) detailed step include:
2.1) C3D4 grid cell is used to carry out stress and strain model for geometric model;
2.2) geometric model after carrying out stress and strain model imports finite element analysis software;In the present embodiment, finite element analysis software Concrete employing Abaqus software;
2.3) in finite element analysis software, C3D4 grid cell is used to carry out stress and strain model geometric model, and by geometry mould In type, the size of mesh opening encryption at spline tooth and escape position, the grid at remaining position carry out free size amplification, and obtain is limited Meta-model is as shown in Figure 3;By by the size of mesh opening encryption at spline tooth in geometric model and escape position, the net at remaining position Lattice carry out free size amplification, it is possible to effectively control number of grid, improve analysis efficiency;
2.4) to geometric model imposed load and boundary condition in finite element analysis software, execute on reverse arm for geometric model Add vertical load, retrain mounting seat, Interference contact is set by between spline tooth pair, quickly submits calculating to, obtain spline and couple anti-side The primary Calculation result (Global_odb destination file) of rolling torsion bar intensity.
3) geometric model is cut, obtain remaining with spline tooth to 4 and the submodel of escape 5 architectural feature.
Based on St.Venant law, the present embodiment step 3) in geometric model cut specifically refer to concentrating away from stress Position is cut, and obtains remaining with spline tooth to 4 and the submodel of escape 5 architectural feature, as shown in Figure 4, and escape 5 gradually detach the skewed slot of formation for mounting seat 2 is added cutter in man-hour from mounting seat 2.
4) submodel use C3D8R grid cell carry out stress and strain model;To carrying out the submodel after stress and strain model in finite element Analyze in software (i.e. Abaqus software) and grid between spline tooth pair is realized conode (as shown in Figure 5), by between spline tooth pair Interference contact is set, imports primary Calculation result (Global_odb destination file), the facet of submodel applies face power and enters (Surface tractions as shown in Figure 6) and submit analytical calculation to, obtains the final calculation result of submodel to row cutting (Sub_model.odb destination file).The present embodiment uses the method for submodel to carry out secondary calculating, cuts structure, Retain spline tooth to 4 and the architectural feature of escape 5, use C3D8R grid cell to divide, and realize grid conode, flower Key tooth between use the mode of Interference contact, it is possible to be effectively improved the accuracy of analysis.
5) final calculation result (Sub_model.odb destination file) for submodel carries out check fatigue life.This enforcement In example, step 5) specifically use fe-safe software to carry out check fatigue life, the present embodiment uses fe-safe software to carry out fatigue Life-span checking substitutes and is carrying out fatigue experiment on testing stand, saves substantial amounts of time and expense.
In the present embodiment, step 5) detailed step include:
5.1) final calculation result of submodel is imported fe-safe software and extracts each analysis of final calculation result of submodel The stress value of final step in step, as it is shown in fig. 7, as a example by analysis step step1, the final step of analysis step step1 is Increment6, then extract the stress value of Increment6 for analysis step step1;
5.2) arrange in fe-safe software fatigue load, load history, number of times fatigue life, surface roughness, material parameter, Tired algorithm also submits calculating to, obtains result of calculation file, and Fig. 8 (a) and (b) are that the embodiment of the present invention is fixed in fe-safe Justice load and the interface schematic diagram of loading sequence, see Fig. 8 (a), and during wherein load selects Dataset 1, stress value is: forward Stress (Direct Range) is 738to-673MPa, and shear stress (Shear Range) is 94to-89MPa, sees figure 8 (b), load loading sequence (Stress Dataset 1) is sinusoidal load (1 ,-1), and fatigue life, (Repeats) was set as 10000000 times;Fig. 9 be the embodiment of the present invention at fe-safe software design patterns analysis of fatigue bound of parameter face schematic diagram, wherein surface is thick Rough (Surface Finish) is (1.6~4 μm), and high spring steel 52CrMoV4 selected by the material (Material) of torsion bar, tired Labor algorithm (Algorithm) uses BrownMiller criterion (Morrow mean stress correction).In the present embodiment, spline joins Connecing anti-side rolling torsion rod material selection 52CrMoV4 steel, as shown in Figure 10, wherein abscissa is the S-N curve quoted in analysis Cycle-index, vertical coordinate is stress value;
5.3) result of calculation file is imported in finite element analysis software, checks life-span cloud atlas and stress intensity factor cloud atlas FOS, Stress intensity factor cloud atlas FOS characterizes the intensity factor S of imposed load, when the value of intensity factor S is more than or equal to 1, sentences It is safe for being scheduled on the fatigue load arranged in fe-safe software under the conditions of current projected life.Shown in Figure 11 enforcement The stress intensity factor cloud atlas FOS that example analysis obtains, wherein at torsion bar spline, minimum stress-intensity factor is 0.909, sees figure The life-span cloud atlas that 12 illustrated embodiment analyses obtain, the fatigue life that at torsion bar spline, minimum stress-intensity factor is corresponding is 3,440,000 Secondary fatigue loading, less than initial designs life-span 10,000,000 times, more coincide with actual tests and (completes 4,100,000 times in actual tests After fatigue loading, torsion bar shaft 15 ruptures, as shown in figure 13) at escape.
Couple the intensity analysis of anti-side rolling torsion rod it should be noted that the present embodiment only lists a kind of spline and check fatigue life Examples of implementation, but the present embodiment method be obviously also applied for any other structure spline couple anti-side rolling torsion rod intensity divide Analysis and fatigue life check, therefore do not repeat them here.
The above is only the preferred embodiment of the present invention, and protection scope of the present invention is not limited merely to above-described embodiment, all The technical scheme belonged under thinking of the present invention belongs to protection scope of the present invention.It should be pointed out that, for the art is common For technical staff, some improvements and modifications without departing from the principles of the present invention, these improvements and modifications also should be regarded as this The protection domain of invention.

Claims (5)

1. a spline couples anti-side rolling torsion rod intensity analysis and check method fatigue life, it is characterised in that step includes:
1) set up spline and couple the geometric model of anti-side rolling torsion rod;
2) described geometric model employing C3D4 grid cell is carried out stress and strain model;Geometric model after carrying out stress and strain model exists In finite element analysis software by spline tooth between binding constraints is set and submits analytical calculation to, obtain described spline couple anti-side rolling The primary Calculation result of torsion bar intensity;
3) described geometric model is cut, obtain remaining with spline tooth to and the submodel of relief groove structure feature;
4) described submodel employing C3D8R grid cell is carried out stress and strain model;Submodel after carrying out stress and strain model is being had Grid between spline tooth pair is realized conode by finite element analysis software, Interference contact is set by between spline tooth pair, import described tentatively Result of calculation, applies face power on the facet of described submodel and is driven and submits analytical calculation to, obtain described submodel Final calculation result;
5) final calculation result for described submodel carries out check fatigue life.
Spline the most according to claim 1 couples anti-side rolling torsion rod intensity analysis and check method fatigue life, and its feature exists In, described step 2) detailed step include:
2.1) C3D4 grid cell is used to carry out stress and strain model for described geometric model;
2.2) geometric model after carrying out stress and strain model imports finite element analysis software;
2.3) in described finite element analysis software, C3D4 grid cell is used to carry out stress and strain model described geometric model, and The size of mesh opening encryption at spline tooth and escape position, the grid at remaining position in described geometric model are carried out free size amplification;
2.4) to described geometric model imposed load and boundary condition in finite element analysis software, turning round for described geometric model Apply vertical load on pivoted arm, retrain mounting seat, Interference contact is set by between spline tooth pair, quickly submits calculating to, obtain described Spline couples the primary Calculation result of anti-side rolling torsion rod intensity.
Spline the most according to claim 2 couples anti-side rolling torsion rod intensity analysis and check method fatigue life, and its feature exists In, described step 3) in described geometric model cut the position specifically referred to concentrating away from stress cut, To remain with spline tooth to and the submodel of relief groove structure feature.
4. couple anti-side rolling torsion rod intensity analysis and check method fatigue life according to the spline described in claim 1 or 2 or 3, It is characterized in that, described step 5) specifically use fe-safe software to carry out check fatigue life.
Spline the most according to claim 4 couples anti-side rolling torsion rod intensity analysis and check method fatigue life, and its feature exists In, described step 5) detailed step include: the final calculation result of described submodel is imported fe-safe software and extracts institute The stress value of final step in each analysis step of the final calculation result stating submodel;Fe-safe software is arranged fatigue load, Load history, number of times fatigue life, surface roughness, material parameter, tired algorithm also submit calculating to, obtain result of calculation literary composition Part;Described result of calculation file is imported in finite element analysis software, checks life-span cloud atlas and stress intensity factor cloud atlas FOS, Described stress intensity factor cloud atlas FOS characterizes the intensity factor S of imposed load, when the value of intensity factor S is more than or equal to 1, Judge that the fatigue load arranged in fe-safe software under the conditions of current projected life is safe.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109885901A (en) * 2019-01-29 2019-06-14 格特拉克(江西)传动系统有限公司 A kind of speed changer welded gear intensity and fatigue life calculation method
CN112744249A (en) * 2021-01-21 2021-05-04 中车青岛四方机车车辆股份有限公司 Anti-side-rolling torsion bar and forming process thereof
CN113742954A (en) * 2020-05-29 2021-12-03 株洲中车时代电气股份有限公司 Interference contact structure, and finite element modeling and calibrating method and system of motor stator
CN114638057A (en) * 2021-12-20 2022-06-17 重庆大学 Spline wear and fatigue life simulation method based on ABAQUS secondary development
CN115859747A (en) * 2023-02-13 2023-03-28 中海油田服务股份有限公司 Calculation method, device and equipment for interference coupling transmission load and storage medium

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11272735A (en) * 1998-03-25 1999-10-08 Matsushita Electric Works Ltd Method for generating finite element method analysis mode for electronic device strength evaluation, method for evaluating strength of electronic device, and evaluation device
CN105069200A (en) * 2015-07-22 2015-11-18 株洲时代新材料科技股份有限公司 Fatigue life analysis method of metal component of underground rail absorber

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11272735A (en) * 1998-03-25 1999-10-08 Matsushita Electric Works Ltd Method for generating finite element method analysis mode for electronic device strength evaluation, method for evaluating strength of electronic device, and evaluation device
CN105069200A (en) * 2015-07-22 2015-11-18 株洲时代新材料科技股份有限公司 Fatigue life analysis method of metal component of underground rail absorber

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘建勋 等: ""花键联接抗侧滚扭杆的应力分析与试验"", 《机械设计与研究》 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109885901A (en) * 2019-01-29 2019-06-14 格特拉克(江西)传动系统有限公司 A kind of speed changer welded gear intensity and fatigue life calculation method
CN113742954A (en) * 2020-05-29 2021-12-03 株洲中车时代电气股份有限公司 Interference contact structure, and finite element modeling and calibrating method and system of motor stator
CN112744249A (en) * 2021-01-21 2021-05-04 中车青岛四方机车车辆股份有限公司 Anti-side-rolling torsion bar and forming process thereof
CN112744249B (en) * 2021-01-21 2022-06-10 中车青岛四方机车车辆股份有限公司 Anti-side-rolling torsion bar and forming process thereof
CN114638057A (en) * 2021-12-20 2022-06-17 重庆大学 Spline wear and fatigue life simulation method based on ABAQUS secondary development
CN114638057B (en) * 2021-12-20 2024-02-06 重庆大学 Spline abrasion and fatigue life simulation method based on ABAQUS secondary development
CN115859747A (en) * 2023-02-13 2023-03-28 中海油田服务股份有限公司 Calculation method, device and equipment for interference coupling transmission load and storage medium

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