CN110046416A - A kind of finite element method of the tools for bolts ' pretension state change under action of lateral load - Google Patents

A kind of finite element method of the tools for bolts ' pretension state change under action of lateral load Download PDF

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CN110046416A
CN110046416A CN201910277741.7A CN201910277741A CN110046416A CN 110046416 A CN110046416 A CN 110046416A CN 201910277741 A CN201910277741 A CN 201910277741A CN 110046416 A CN110046416 A CN 110046416A
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bolt
finite element
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CN110046416B (en
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高大威
龚嘉成
梁浩天
郑腾飞
刘乾
张黎
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University of Shanghai for Science and Technology
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    • 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
    • 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
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Abstract

The present invention relates to a kind of finite element methods of tools for bolts ' pretension state change under action of lateral load.The following steps are included: S1: establishing thread connection finite element mesh model in Hypermesh software;S2: setting material parameter;S3: model file is saved and is imported in Abaqus software;S4: creation screw thread engagement contact to and nuts contact with clamped part pair;S5: three analysis steps are defined;S6: three reference points are established;S7: six-freedom degree is defined respectively to bolt, nut and each reference point;S8: field output is defined;S9: setting boundary condition;S10: the state change that nuts is contacted with clamped part is extracted.The main reason for present invention is by loosening thread connection in actual condition-action of lateral load carries out simulation analysis, it obtains being threadably coupled within the corner variation that action of lateral load contacts the variation of Pre strained state in the process, tangential force is moved back with lateral displacement variation and nuts generation pine, computational efficiency is improved, saves and calculates the time.

Description

A kind of finite element method of the tools for bolts ' pretension state change under action of lateral load
Technical field
The present invention relates to finite element simulation technical fields, and in particular to one kind tools for bolts ' pretension state under action of lateral load The finite element method of variation.
Background technique
Thread connection is one of most common and most widely used type of attachment, precision height, warp convenient with assembly and disassembly The advantages that Ji property is good.Therefore the reliability of thread connection is particularly important, especially under vibration, because the factors such as loosening cause Thread connection failure leads to structure abnormal sound, even results in thread joined structure so as to cause the decline of pressing force suffered by clamped part Fatigue fracture etc. causes major accident.As shown in Figure 1, nuts shows with clamped part contact surface state change when being bolt-connection It is intended to, close-coupled that both black state is, both the grid-like state of grey, which is, is slidably connected, it can be seen that with using the time Passage, pretightning force between the two is smaller and smaller, and last pretightning force disappears, and the two connection pine drags.
Finite element analysis (Finite Element Analysis), abbreviation FEA is developed rapidly in modern computer On the basis of and a kind of numerical approximation method for growing up, it is to solve object with the unit of many interactions of composition model Come replace directly to complex model solve, to realize the simplification of challenge, but be not Exact Solutions by the solution that it is acquired, and It is a kind of approximate solution.In practical applications, many models, operating condition are excessively complicated, or even can not estimate, but finite element analysis side Method is widely applicable, in recent years again constantly update and compensatory algorithm, have become solve engineering problem and analysis important means.
Many researchs are had been carried out to thread connection currently with finite element method, but for a long time due to screw thread The complexity of coupling structure lacks always unified understanding for the loosening mechanism of thread connection, but existing research shows transverse direction Oscillating load is the main reason for caused thread connection loosens.
Summary of the invention
Against the above deficiency, the present invention provides a kind of finite elements of tools for bolts ' pretension state change under action of lateral load Analysis method, this method disclose transverse load pair from contact relation and tangential force two angles of variation between thread connection component The influence that thread connection loosens solves the problems, such as that existing thread connection loosens.
The technical solution of the present invention is as follows:
A kind of finite element method of the tools for bolts ' pretension state change under action of lateral load, comprising the following steps:
S1: establishing thread connection finite element mesh model in Hypermesh software, and the model includes one clamped Part, a bolt and an attaching nut;
S2: setting material parameter, including density of material, Young's modulus, Poisson's ratio, and material properties are assigned for each part;
S3: model file is saved and is imported in Abaqus software;
S4: creation screw thread engagement contact to and nuts contact with clamped part pair;
S5: three analysis steps, respectively step1, step2 and step3 are defined;
S6: establishing three reference points, respectively RP-Plate, RP-Bolt, RP-Nut, the reference point RP-Plate with Clamped part bottom surface node makees movement coupling constraint, and the reference point RP-Bolt is transported with nuts cylindrical outer surface node Dynamic coupling constraint, the reference point RP-Nut and nut cylindrical outer surface node make movement coupling constraint;
S7: defining six-freedom degree to bolt, nut and each reference point respectively, is respectively as follows: displacement along the x axis, along Y Axis direction displacement, along Z-direction displacement, turn about the X axis angle, around Y-axis rotational angle, turn about the Z axis angle;
S8: field output is defined, the tangential friction force that course output nuts contact pair with clamped part, course, which exports, to be referred to Point RP-Bolt's turns about the X axis angle;
S9: setting boundary condition: the constraint to symmetry class of the bolt setting since initial step only discharges X-direction Displacement freedom remains unchanged when being displaced along the x axis from step1 to step2, and when step3 selects failure mode;To reference point The constraint of displacement type of the RP-Plate setting since initial step, and six-freedom degree is discharged, six-freedom degree value is in step1 When be disposed as remaining unchanged when 0, step2, will modification of displacement be along the y axis lateral displacement load amplitude when step3, and select Sinusoidal load mode is selected, other freedom degrees maintain 0 value constant;Displacement type since step1 is arranged to reference point RP-Nut Constraint, and discharge six-freedom degree, six-freedom degree value is disposed as 0 in step1, and when step2, step3 keeps not Become;
S10: extracting the state change that nuts is contacted with clamped part, using lateral displacement load as abscissa, ordinate The tangential friction force for exporting nuts and clamped part contact surface, using the time as abscissa, ordinate exports reference point RP-Bolt Turn about the X axis angle.
The thread connection mesh of finite element model established in the step S1 is the hexahedron network mould for considering lead angle Type.
The tangential behavior contacted in the step S4 is all made of penalty function friction model algorithm.
In the normal direction behavior contacted in the step S4, screw thread engagement contact uses the soft Contact Algorithm of exponential form, spiral shell Bolt cap contacts the hard Contact Algorithm using penalty function with clamped part.
The present invention is from the contact relation and tangential force two angles of variation between thread connection component, by actual condition The main reason for thread connection loosens-action of lateral load carries out simulation analysis, to observe it to threaded pre-tightening state change It influences.The present invention accounts for the fine modeling of lead angle to screw thread as a result, and introduces the thought of interaction, by setting Setting boundary condition reduces contact creation logarithm, can be obtained and contacts Pre strained state during being threadably coupled within action of lateral load Variation, tangential force changes with lateral displacement and nuts occurs the corner that moves back of pine and changes, improve computational efficiency, save and calculate Time.Meanwhile the present invention can be in simulating other similar bolt looseness problems as reference.
Detailed description of the invention
Fig. 1 is that the nuts of the embodiment of the present invention and clamped part contact condition change schematic diagram;
Fig. 2 is the model structure and reference point schematic diagram of the embodiment of the present invention;
Fig. 3 is nuts constraint and the reference point coupling constraint schematic diagram of the embodiment of the present invention;
Fig. 4 is the tangential force of the embodiment of the present invention with lateral displacement load change relation schematic diagram;
Fig. 5 is the nuts pine retreat angle variation schematic diagram of the embodiment of the present invention.
Specific embodiment
It is described further below with reference to technical effect of the attached drawing to design of the invention, specific structure and generation, with It is fully understood from the purpose of the present invention, feature and effect.
Referring to figs. 2 and 3, the finite element analysis side of the tools for bolts ' pretension state change of the invention under action of lateral load Method, comprising the following steps:
S1: establishing thread connection finite element mesh model in Hypermesh software, and model includes a clamped part 10, a M16 plain bolt 20 and an attaching nut 30, clamped part 10 are spun on the screw rod of bolt 20, and side resists spiral shell Bolt cap, the other side are clamped with nut 30, and grid model is the hexahedron network model for considering lead angle;
S2: setting material parameter, including density of material, Young's modulus, Poisson's ratio, and material properties are assigned for each part;
S3: model file is saved as into .inp file, and is imported in Abaqus software;
S4: creation screw thread engagement contact to and nuts contact with clamped part pair, the tangential behavior of contact, which is all made of, penalizes Function friction model algorithm, in the normal direction behavior of contact, screw thread engagement contact uses the soft Contact Algorithm of exponential form, nuts The hard Contact Algorithm using penalty function is contacted with clamped part;
S5: three analysis steps, respectively step1, step2 and step3 are defined;
S6: three reference points, respectively RP-Plate11, RP-Bolt21, RP-Nut31, reference point RP- are established Plate11 and clamped 10 bottom surface node of part make movement coupling constraint, reference point RP-Bolt21 and 20 cap cylinder appearance of bolt Face node makees movement coupling constraint, and reference point RP-Nut31 and 30 cylindrical outer surface node of nut make movement coupling constraint;
S7: defining six-freedom degree U1, U2, U3, UR1, UR2, UR3 to bolt 20, nut 30 and each reference point respectively, Displacement along the x axis is respectively represented, is displaced along the y axis, is displaced along Z-direction, turns about the X axis angle, around Y-axis angle of rotation It spends, turn about the Z axis angle;
S8: field output is defined, the tangential friction force that course output nuts contact pair with clamped part, course, which exports, to be referred to Point RP-Bolt21's turns about the X axis angle UR1;
S9: setting boundary condition:
The constraint for the symmetry class that initial step starts is set to bolt 20, only discharges X-direction displacement freedom, i.e. edge X-direction is displaced U1 ≠ 0, and U1 is remained unchanged when from step1 to step2, is U1 selection failure mould when brought forward value, step3 Formula;
Constraint to displacement type of the reference point RP-Plate11 setting since initial step, and six-freedom degree is discharged, Six-freedom degree value is disposed as 0, i.e. U1=U2=U3=UR1=UR2=UR3=0 in step1, and when step2 keeps not Become, is revised as lateral displacement load amplitude for U2 will be displaced along the y axis when brought forward value, step3, and select sinusoidal load mould Formula, other freedom degrees maintain 0 value constant;
The constraint of displacement type since step1 is set to reference point RP-Nut31, and discharges six-freedom degree, six Free angle value is disposed as 0, i.e. U1=U2=U3=UR1=UR2=UR3=0 in step1, and when step2, step3 keeps It is constant, for after brought forward value;
S10: the state change that nuts is contacted with clamped part is extracted: as shown in figure 4, with lateral displacement load for horizontal seat Mark, ordinate export the tangential friction force of nuts and clamped part contact surface, reflect lateral displacement load to bolt pretightening Influence.As shown in figure 5, using the time as abscissa, ordinate exports the axial corner of reference point RP-Bolt, reflection with when Between elapse, nuts pine retreat angle variation.
The present invention can concisely obtain being threadably coupled within action of lateral load mistake based on screw thread refined model The tangential force of the variation of contact condition in journey, nuts and clamped part contact surface changes with lateral displacement, and and nuts The variation that pine retreat angle occurs, improves computational efficiency, saves and calculates the time.
Disclosed above is only the embodiment of the present invention, and still, the present invention is not limited to this, the technology of any this field What personnel can think variation should all fall into protection scope of the present invention.

Claims (4)

1. a kind of finite element method of the tools for bolts ' pretension state change under action of lateral load, which is characterized in that including with Lower step:
S1: establishing thread connection finite element mesh model in Hypermesh software, and the model includes a clamped part (10), a bolt (20) and an attaching nut (30);
S2: setting material parameter, including density of material, Young's modulus, Poisson's ratio, and material properties are assigned for each part;
S3: model file is saved and is imported in Abaqus software;
S4: creation screw thread engagement contact to and nuts contact with clamped part pair;
S5: three analysis steps, respectively step1, step2 and step3 are defined;
S6: three reference points, respectively RP-Plate (11), RP-Bolt (21), RP-Nut (31), the reference point RP- are established Plate (11) and clamped part (10) bottom surface node make movement coupling constraint, the reference point RP-Bolt (21) and bolt (20) cap cylindrical outer surface node makees movement coupling constraint, the reference point RP-Nut (31) and nut (30) cylindrical outer surface section Point makees movement coupling constraint;
S7: six-freedom degree is defined to bolt (20), nut (30) and each reference point respectively, is respectively as follows: position along the x axis Move, along the y axis displacement, along Z-direction displacement, turn about the X axis angle, around Y-axis rotational angle, turn about the Z axis angle;
S8: field output, the tangential friction force that course output nuts contacts pair with clamped part, course output reference point are defined RP-Bolt's (21) turns about the X axis angle;
S9: setting boundary condition: the constraint to symmetry class of bolt (20) setting since initial step only discharges X-direction Displacement freedom remains unchanged when being displaced along the x axis from step1 to step2, and when step3 selects failure mode;
Constraint to displacement type of reference point RP-Plate (11) setting since initial step, and six-freedom degree is discharged, six A free angle value remains unchanged when being disposed as 0, step2 in step1, will modification of displacement be along the y axis laterally when step3 It is displaced load amplitude, and selects sinusoidal load mode, other freedom degrees maintain 0 value constant;Reference point RP-Nut (31) are arranged The constraint of displacement type since step1, and six-freedom degree is discharged, six-freedom degree value is disposed as 0 in step1, It is remained unchanged when step2, step3;
S10: extracting the state change that nuts is contacted with clamped part, using lateral displacement load as abscissa, ordinate output The tangential friction force of nuts and clamped part contact surface, using the time as abscissa, ordinate exports reference point RP-Bolt (21) Turn about the X axis angle.
2. finite element method according to claim 1, which is characterized in that the thread connection established in the step S1 Mesh of finite element model is the hexahedron network model for considering lead angle.
3. finite element method according to claim 1, which is characterized in that the tangential behavior contacted in the step S4 It is all made of penalty function friction model algorithm.
4. finite element method according to claim 1, which is characterized in that the normal direction behavior contacted in the step S4 On, screw thread engagement contact uses the soft Contact Algorithm of exponential form, and nuts contacts connecing firmly using penalty function with clamped part Touch algorithm.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111046512A (en) * 2020-01-02 2020-04-21 重庆齿轮箱有限责任公司 Planetary gearbox bolt analysis method
CN111209707A (en) * 2020-02-21 2020-05-29 山东交通学院 Friction type bolt connecting node bearing compression-shear combination effect, method and system
CN112052510A (en) * 2019-12-12 2020-12-08 格特拉克(江西)传动系统有限公司 Method for checking slip risk of bolted connection of differential mechanism based on dynamic load
CN112632659A (en) * 2020-12-08 2021-04-09 株洲时代新材料科技股份有限公司 Analysis method for GINA waterstop for immersed tunnel
CN112699465A (en) * 2020-12-29 2021-04-23 中国航空工业集团公司西安飞机设计研究所 ABAQUS-based multi-bolt connection knot building model method
CN113886984A (en) * 2021-09-28 2022-01-04 中国第一汽车股份有限公司 Bolt solid grid modeling and loading method
CN117390914A (en) * 2023-09-25 2024-01-12 航天精工股份有限公司 Connection system looseness finite element simulation method considering thread creep

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108460237A (en) * 2018-04-08 2018-08-28 大连理工大学 A kind of bolt fastening structure loosening finite element simulation method considering the practical tangential force state of screw thread

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108460237A (en) * 2018-04-08 2018-08-28 大连理工大学 A kind of bolt fastening structure loosening finite element simulation method considering the practical tangential force state of screw thread

Non-Patent Citations (8)

* Cited by examiner, † Cited by third party
Title
倪佩韦等: "基于三维有限元模型的螺纹副承载力分布研究", 《起重运输机械》 *
孔繁晓等: "预紧力对风电叶片根部螺栓疲劳寿命的影响分析", 《风机技术》 *
孙晓萌等: "螺栓预紧力下的应力分析", 《电子科技》 *
张忠伟等: "曲轴平衡重螺栓仿真分析与试验研究", 《铁道机车车辆》 *
李虎等: "基于ABAQUS的螺栓连接分析方法研究", 《机械研究与应用》 *
杨广雪等: "基于有限元的一种新型螺母的防松机理研究", 《工程力学》 *
王传华等: "基于精确建模的横向振动工况下螺栓松动机理研究", 《宇航总体技术》 *
胡远忠: "螺栓摩擦系数对连接防松影响的有限元分析", 《机械工程师》 *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112052510A (en) * 2019-12-12 2020-12-08 格特拉克(江西)传动系统有限公司 Method for checking slip risk of bolted connection of differential mechanism based on dynamic load
CN112052510B (en) * 2019-12-12 2024-04-05 麦格纳动力总成(江西)有限公司 Dynamic load-based differential mechanism bolting slip risk checking method
CN111046512A (en) * 2020-01-02 2020-04-21 重庆齿轮箱有限责任公司 Planetary gearbox bolt analysis method
CN111046512B (en) * 2020-01-02 2023-05-12 重庆齿轮箱有限责任公司 Analysis method for planetary gear box bolt
CN111209707A (en) * 2020-02-21 2020-05-29 山东交通学院 Friction type bolt connecting node bearing compression-shear combination effect, method and system
CN111209707B (en) * 2020-02-21 2023-06-23 山东交通学院 Friction type bolt connection node under combined action of compression shear, method and system
CN112632659A (en) * 2020-12-08 2021-04-09 株洲时代新材料科技股份有限公司 Analysis method for GINA waterstop for immersed tunnel
CN112699465A (en) * 2020-12-29 2021-04-23 中国航空工业集团公司西安飞机设计研究所 ABAQUS-based multi-bolt connection knot building model method
CN113886984A (en) * 2021-09-28 2022-01-04 中国第一汽车股份有限公司 Bolt solid grid modeling and loading method
CN113886984B (en) * 2021-09-28 2022-09-09 中国第一汽车股份有限公司 Bolt solid grid modeling and loading method
CN117390914A (en) * 2023-09-25 2024-01-12 航天精工股份有限公司 Connection system looseness finite element simulation method considering thread creep

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