CN102004819B - Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state - Google Patents

Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state Download PDF

Info

Publication number
CN102004819B
CN102004819B CN201010535573A CN201010535573A CN102004819B CN 102004819 B CN102004819 B CN 102004819B CN 201010535573 A CN201010535573 A CN 201010535573A CN 201010535573 A CN201010535573 A CN 201010535573A CN 102004819 B CN102004819 B CN 102004819B
Authority
CN
China
Prior art keywords
stress
mother metal
under
sigma
sim
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
CN201010535573A
Other languages
Chinese (zh)
Other versions
CN102004819A (en
Inventor
詹梅
杨合
刘静
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.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical University
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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Priority to CN201010535573A priority Critical patent/CN102004819B/en
Publication of CN102004819A publication Critical patent/CN102004819A/en
Application granted granted Critical
Publication of CN102004819B publication Critical patent/CN102004819B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

The invention relates to a method for determining constitutive parameters of a butt welded pipe welding seam in the biaxial stress state, which comprises the following steps of: determining the constitutive parameters of the parent metal in the uniaxial stress state, thereby determining the range of the parent metal strength factor K<sim> in the perforated sample tensile finite element analogy, and the range of the hardening index n<sim>; and by determining the variation ranges of the strength factor and the hardening index, obtaining the relationship between different constitutive parameter combinations (K<sim>, n<sim>) and the combinations (F<sim>, Delta l<sim>) of tensile force and gauge length elongation, and establishing a recessive mapping relationship between the combination (F, Delta l) of tensile force and gauge length elongation and the constitutive parameter combination (K, n), thereby obtaining the constitutive parameters of the welding seam in the biaxial stress state. The method induces the planar biaxial tension stress state, which is more approximate to the true stress state of pipe deformation, in the uniaxial tension process of a perforated sample, can be used for accurately and efficiently determining the constitutive parameters of the welding seam ductility of a butt welded pipe, and is beneficial to enhancing the forming quality and the forming limit of the welded pipe.

Description

The method of straight welded pipe welding-seam constitutive parameter under a kind of definite two-dimensional state of stress
Technical field
The present invention relates to ERW Plastic Forming field, specifically is the method for straight welded pipe welding-seam constitutive parameter under a kind of definite two-dimensional state of stress, and this technology also can be extended to confirming of welding plate welding seams constitutive parameter.
Background technology
Because ERW bool has characteristics such as low cost, short period, Strengthening and Toughening, in auto industry, has obtained widespread use.The main difference of welded tube and solid drawn tube is the significant difference of weld seam and mother metal performance; There are significant difference in the strength factor K and the hardenability value n that then mainly are reflected in for the Plastic Forming Effect on Performance in the constitutive parameter of weld seam and mother metal; Be much bigger than mother metal of the strength factor K of weld seam, its hardenability value n is much little than mother metal then.Because ERW mainly presents two-dimensional state of stress in BENDING PROCESS, confirm that therefore the constitutive parameter K of welded tube weld material under the two-dimensional state of stress and n are the bases of research welded tube bending ductility deformational behavior, raising welded tube bending forming quality and forming limit.
Through to literature searches such as existing domestic and international patented technology, standards, do not see the related patent U.S. Patent No. bibliographical information of confirming weld seam constitutive parameter K and n method under the two-dimensional state of stress at present as yet.
Consult relevant both at home and abroad periodical literature, finding that existing method about the weld seam constitutive parameter K that confirms to weld plate and welded tube and n all is based on carries out under the uniaxial stressed state.These methods comprise three kinds of unilateral stretching experimental method, composite material stretching experiment method and microhardness experimental methods.Wherein, the unilateral stretching experimental method is standard or the non-standard tensile sample that directly direct intercepting only comprises weld material on welded tube, carries out the unilateral stretching experiment then.Strength factor K value and the hardenability value n value that the stress-strain diagram match that obtains obtains reflecting the weld material characteristic tested in unilateral stretching.This method mainly is applicable to wide weld seam welded tube, and for the bead weld welded tube, directly intercepting only contains the tensile sample difficulty of weld seam, because the width of sample is very big to the measurement result influence, thereby causes determined Weld Performance parameter fluctuation property big, inaccurate.To the deficiency that is difficult to prepare pure weld seam tensile sample in the weld material stretching experiment; Composite material stretching experiment method is that intercepting comprises that weld seam and material around make the composite material tensile sample near weld seam; Carry out the unilateral stretching experiment; Go out the flow stress of weld seam again based on mixing rule " extraction " from test figure, and then match obtains the constitutive parameter K and the n value of weld material.But, perhaps be regarded as mother metal because this method will or be regarded as weld material between the heat-affected zone material between weld seam and mother metal.Specimen width is different, just means that also heat-affected zone proportion in sample is different, thereby the precision of the weld material constitutive parameter that obtained is had very big influence.And the microhardness experimental method through weld seam and experiment of mother metal microhardness and mother metal unilateral stretching experiment, obtains the flow stress of weld seam then based on hardness-stress direct ratio formula, and then match obtains the constitutive parameter K and the n of weld material.Because the microhardness experimental method is simple, thereby has obtained widespread use.
For the solid drawn tube bending forming, Yan Jing etc. have proposed the method for solid drawn tube constitutive parameter K and n under a kind of definite two-dimensional state of stress.This method has at first designed the porose tensile sample that two-dimensional state of stress under unilateral stretching, can occur; Adopt porose sample unilateral stretching experiment then, obtained the constitutive parameter K and the n of solid drawn tube under the two-dimensional state of stress in conjunction with finite element analogy and artificial neural network.This method is applicable to seamless tubular goods, can be the constitutive parameter K and the n that confirm ERW mother metal under the two-dimensional state of stress reference is provided.
Summary of the invention
For overcoming the difficult problem that prior art can't obtain welded tube weld seam constitutive parameter under the two-dimensional state of stress, the present invention proposes the method for straight welded pipe welding-seam constitutive parameter under a kind of definite two-dimensional state of stress.
The method of straight welded pipe welding-seam constitutive parameter comprises the steps: under definite two-dimensional state of stress that the present invention proposes
Step 1; Carry out mother metal unilateral stretching experiment, confirm constitutive parameter
Figure BSA00000337395600021
and of mother metal under uniaxial stressed state
The specimen types of using according to tubing among the GB/T 228-2002 appendix D, from the mother metal position of the weld seam symmetry vertical standard arc tensile sample of intercepting total wall thickness vertically, wherein scale-up factor gets 5.65.
Adopt cupping machine that this sample is carried out the unilateral stretching experiment; Obtain the flow stress-strain data of mother metal in the drawing process, adopt formula (1), formula (2) to obtain constitutive parameter
Figure BSA00000337395600023
and
Figure BSA00000337395600024
of mother metal under uniaxial stressed state then
n uni b = N &CenterDot; &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) &CenterDot; ( lg &sigma; &OverBar; uni , j b ) - &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) &CenterDot; &Sigma; j = 1 N ( lg &sigma; &OverBar; uni , j b ) N &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) 2 - [ &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) ] 2 - - - ( 1 )
K uni b = exp [ &Sigma; j = 1 N ( lg &sigma; &OverBar; uni , j b ) - n uni b &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) N ] - - - ( 2 )
In formula (1), (2);
Figure BSA00000337395600027
is the flow stress under the mother metal uniaxial stressed state; ε is the logarithmic strain under the mother metal uniaxial stressed state; N is the flow stress-strain data group number under the mother metal uniaxial stressed state that obtains in the stretching experiment;
Figure BSA00000337395600028
is the strength factor under the mother metal uniaxial stressed state, and
Figure BSA00000337395600029
is the hardenability value under the mother metal uniaxial stressed state.
Step 2 is confirmed the quadrature arranging scheme of the porose sample stretching of mother metal sunykatuib analysis
Strength factor according to mother metal under the uniaxial stressed state that obtains in the step 1
Figure BSA000003373956000210
And hardenability value
Figure BSA000003373956000211
Confirm the strength of parent COEFFICIENT K in the porose sample stretching finite element analogy SimScope do
Figure BSA00000337395600031
Hardenability value n SimScope do
Figure BSA00000337395600032
And the variation range of strength factor and hardenability value two factors is subdivided into 3~4 levels, corresponding factor level table is seen table 1, table 2.Corresponding to the factor level number is that 3 and 4 orthogonal table is confirmed as L respectively 9(3 4) and L 16(4 5).Certain that then strength factor and hardenability value two factors is put into selected orthogonal table two lists, thereby obtains the orthogonal experiment arranging scheme of porose sample stretching sunykatuib analysis.
Table 1: the factor level table when strength factor and hardenability value are got 3 levels
Figure BSA00000337395600033
Table 2: the factor level table when strength factor and hardenability value are got 4 levels
Figure BSA00000337395600034
Step 3 obtains different constitutive parameter combination (K Sim, n Sim) make up (F with tensile force and elongation between gages amount Sim, Δ l Sim) corresponding relation
Set up the porose sample unilateral stretching of mother metal finite element model.The porose specimen configuration size wherein and the physical dimension of the vertical standard arc tensile sample of total wall thickness are identical, and beat the through hole of Φ 5mm along thickness direction at the sample center, and draw speed is 3mm/min.Adopt the porose sample stretch finite element model of being set up of mother metal,, simulate different constitutive parameter combination (K according to the quadrature arranging scheme that step 2 is confirmed Sim, n Sim) under porose sample unilateral stretching process.Obtain maximum stretching force and corresponding sample marking distance elongation in the simulation process.5s extracts 5 tensile forces and corresponding sample marking distance elongation data equably in the time before this maximum stretching force occurs then, and back 4s extracts 4 tensile forces and correspondence equably in the time sample marking distance elongation data occur at this maximum stretching force.Thereby obtain every group of constitutive parameter combination (K Sim, n Sim) with 10 groups of tensile forces and sample marking distance elongation (F Sim, Δ l Sim) corresponding relation.
Step 4 is set up the combination of the combination of tensile force and elongation between gages amount (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n)
Structure comprises the error back propagation artificial neural network of three layers of input layers, latent layer, output layer.Wherein, the node number of input layer, latent layer, output layer is respectively 20,8 and 2; And the training function of network using is the Levenberg-Marquardt function; The transport function of input layer-latent interlayer is Tangent sigmoid, and the transport function between latent layer-output layer is the linear function.With tensile force that obtains in the step 3 and elongation between gages amount combination (F Sim, Δ l Sim) as the input vector of artificial neural network, constitutive parameter makes up (K Sim, n Sim) as output vector, this artificial neural network is trained, set up the combination of the combination of tensile force and elongation between gages amount (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n).
Step 5 is carried out the porose sample unilateral stretching experiment of mother metal, obtains the tensile force F in the experiment ExpWith elongation between gages amount Δ l Exp
With the mother metal zone of weld seam symmetry, measure-alike punching sample in intercepting and the step 2 adopts cupping machine that sample is carried out the unilateral stretching experiment of 3mm/min, the sample marking distance elongation of maximum stretching force in obtaining testing and correspondence.5s extracts 5 tensile forces and corresponding sample marking distance elongation data equably in the time before this maximum stretching force occurs then, and back 4s extracts 4 tensile forces and correspondence equably in the time sample marking distance elongation data occur at this maximum stretching force.Thereby obtain 10 groups of tensile forces and sample marking distance elongation (F Exp, Δ l Exp) data are right.
Step 6, constitutive parameter
Figure BSA00000337395600041
and of mother metal under the acquisition two-dimensional state of stress
10 groups of tensile forces that step 5 is obtained and elongation between gages amount (F Exp, Δ l Exp) data make up with elongation between gages amount combination (F, Δ l) and constitutive parameter in step 4, set up tensile force as input vector input that (K in the artificial neural network of the recessive mapping relations between n), obtains the constitutive parameter of mother metal under two-dimensional state of stress
Figure BSA00000337395600043
With
Figure BSA00000337395600044
Step 7 is set up the relation between the mother metal flow stress under the single, double stress state
Given strain value variation range ε=[0,0.5], and adopt formula (3) that it is separated into 100 sections.Obtained according to step a base material in the uniaxial stress state constitutive parameters and
Figure BSA00000337395600046
using the formula
Figure BSA00000337395600047
get the base material in uniaxial stress state flow stress According to the base material obtained in Step 6 biaxial stress state in the constitutive parameters
Figure BSA00000337395600049
and
Figure BSA000003373956000410
using formula
Figure BSA000003373956000411
get the base material in the biaxial stress state flow stress
Figure BSA000003373956000412
using regression analysis to establish the base material under biaxial stress state flow stress
Figure BSA000003373956000413
and the base material under uniaxial stress state flow stress
Figure BSA000003373956000414
functional relationship between the two (4)
ε j=0.5/100×(j-1)(j=1,…,101) (3)
&sigma; bi b = f ( &sigma; uni b ) - - - ( 4 )
In formula (3), j is with one of them discrete point after being separated into 100 sections between strain regions, ε jIt is the corresponding strain value of j discrete point.In formula (4);
Figure BSA00000337395600052
is the flow stress of mother metal under uniaxial stressed state;
Figure BSA00000337395600053
is the flow stress of mother metal under two-dimensional state of stress, and f is the funtcional relationship of the two.
Step 8 is carried out the microhardness experiment, confirms weld hardness HV wAnd mother metal hardness HV b
After with sand paper welded tube surface finish to be measured being polished; Along circumferentially pasting a slice coordinate paper, clip pipe fitting on the pipe surface, be put on the testing table with anchor clamps; Begin to measure hardness from the weld seam center; Then pipe is rotated 1mm (the 1mm mesh lines through alignment coordinate paper is realized), clamp pipe once more, measure once more.So repeat, obtain the hardness HV of weld seam wAnd the hardness HV of mother metal b
Step 9 is confirmed the flow stress
Figure BSA00000337395600054
of weld seam under uniaxial stressed state
Flow stress with mother metal under the uniaxial stressed state in [0,0.5] between the given strain regions of step 7 acquisition
Figure BSA00000337395600055
The weld seam and the mother metal hardness HV that obtain with step 8 w, HV bSubstitution formula (5), the flow stress of weld seam under the acquisition uniaxial stressed state
Figure BSA00000337395600056
&sigma; uni , j w = HV w HV b &sigma; uni , j b , ( j = 1 , &CenterDot; &CenterDot; &CenterDot; , 101 ) - - - ( 5 )
In the formula (5), HV w, HV bBe respectively weld seam and mother metal hardness, j is with one of them discrete point after being separated into 100 sections between strain regions,
Figure BSA00000337395600058
Be respectively weld seam and the mother metal flow stress under uniaxial stressed state.
Step 10 is confirmed the flow stress
Figure BSA00000337395600059
of weld seam under two-dimensional state of stress
Between the given strain regions that step 9 is obtained [0; 0.5] in
Figure BSA000003373956000510
substitution formula (4) in the scope, obtain the flow stress between this strain regions of weld seam under the two-dimensional state of stress
Step 11 is confirmed constitutive parameter
Figure BSA000003373956000512
and
Figure BSA000003373956000513
of weld seam under two-dimensional state of stress
Flow stress according to weld seam under the two-dimensional state of stress in [0,0.5] scope between the strain regions of step 10 acquisition
Figure BSA000003373956000514
With strain stress jData, employing formula (6), formula (7) obtain the constitutive parameter of weld seam under two-dimensional state of stress With
Figure BSA000003373956000516
n bi w = 101 &CenterDot; &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) &CenterDot; ( lg &sigma; &OverBar; bi , j w ) - &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) &CenterDot; &Sigma; j = 1 101 ( lg &sigma; bi , j w ) 101 &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) 2 - [ &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) ] 2 - - - ( 6 )
K bi w = exp [ &Sigma; j = 1 101 ( lg &sigma; bi , j w ) - n bi w &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) 101 ] - - - ( 7 )
In formula (6), (7),
Figure BSA000003373956000519
is the flow stress of weld material under two-dimensional state of stress;
Figure BSA000003373956000520
is the strength factor of weld material under two-dimensional state of stress;
Figure BSA00000337395600061
is the hardenability value of weld material under two-dimensional state of stress; ε is strain.
The invention has the beneficial effects as follows: the method for straight welded pipe welding-seam constitutive parameter under a kind of definite two-dimensional state of stress that the present invention proposes; Only need carry out simple standard and singly draw experiment, porose sample stretching experiment and micro-hardness testing experiment; In conjunction with finite element numerical simulation and neural network prediction method, can obtain the constitutive parameter of welded tube weld seam.The experimental implementation that this method relates to is simple; Induced the two-way tensile stress state in plane of the true stress state that more approaches the tubing distortion in the sample unilateral stretching process of in addition punching, and the method that the artificial neural network that is adopted, finite element analogy and experiment combine has been proved to be the method that a kind of high precision obtains the solid drawn tube plasticity constitutive parameter under two-dimensional state of stress and the large deformation condition.Therefore the present invention can be used for confirming accurately and efficiently straight welded pipe welding-seam plasticity constitutive parameter; Plastic yield behavior for research welded tube BENDING PROCESS; Shaping law and parameter optimization and the assessment of welded tube forming property provide important method and basis; Help improving welded tube forming quality and forming limit, promote further developing of the advanced theory and technology of welded tube bending and Plastic Forming.
Four, description of drawings
Fig. 1 is for confirming the process flow diagram of straight welded pipe welding-seam constitutive parameter under the two-dimensional state of stress;
Fig. 2 is porose sample stretch finite element model.
Five, embodiment
Embodiment one:
Present embodiment is to confirm that specification is the weld seam constitutive parameter of ERW under the QSTE340 two-dimensional state of stress of 78 * 2.7mm, and it confirms that specifically step is following:
The specimen types of using according to tubing among the GB/T 228-2002 appendix D, from the mother metal position of the weld seam symmetry vertical standard arc tensile sample of intercepting total wall thickness vertically, wherein scale-up factor gets 5.65.Adopt cupping machine that this sample is carried out the unilateral stretching experiment; Obtain the flow stress-strain data of mother metal in the drawing process, adopt formula (1), formula (2) to obtain the constitutive parameter
Figure BSA00000337395600063
of mother metal under uniaxial stressed state then
n uni b = N &CenterDot; &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) &CenterDot; ( lg &sigma; &OverBar; uni , j b ) - &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) &CenterDot; &Sigma; j = 1 N ( lg &sigma; &OverBar; uni , j b ) N &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) 2 - [ &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) ] 2 - - - ( 1 )
K uni b = exp [ &Sigma; j = 1 N ( lg &sigma; &OverBar; uni , j b ) - n uni b &Sigma; j = 1 N ( lg &epsiv; &OverBar; j ) N ] - - - ( 2 )
In formula (1), (2);
Figure BSA00000337395600066
is the flow stress under the mother metal uniaxial stressed state; ε is the logarithmic strain under the mother metal uniaxial stressed state; N is the flow stress under the mother metal uniaxial stressed state-strain data group number;
Figure BSA00000337395600071
is the strength factor under the mother metal uniaxial stressed state, and
Figure BSA00000337395600072
is the hardenability value under the mother metal uniaxial stressed state.
Step 2 is confirmed the quadrature arranging scheme of the porose sample stretching of mother metal sunykatuib analysis
Strength factor according to mother metal under the uniaxial stressed state that obtains in the step 1
Figure BSA00000337395600073
And hardenability value
Figure BSA00000337395600074
Confirm the strength of parent COEFFICIENT K in the porose sample stretching finite element analogy SimScope be (449,1249), hardenability value n SimScope be (0.177,0.267), and the variation range of strength factor and hardenability value two factors is subdivided into 3 levels, corresponding factor level table is seen table 3.And adopt orthogonal table L in view of the above 9(3 4).Certain that then strength factor and hardenability value two factors is put into selected orthogonal table two lists, thereby confirms to obtain the quadrature arranging scheme of porose sample stretching sunykatuib analysis, and is as shown in table 4.
Table 3: the factor level table when the sharp hardenability value of strength factor is got 3 levels in the instance 1
Figure BSA00000337395600075
Table 4: the quadrature arranging scheme of instance 1
Figure BSA00000337395600076
Step 3 obtains different constitutive parameter combination (K Sim, n Sim) make up (F with tensile force and elongation between gages amount Sim, Δ l Sim) corresponding relation
Set up the porose sample unilateral stretching of mother metal finite element model.Wherein the physical dimension of the vertical standard arc tensile sample of the physical dimension of porose sample and total wall thickness is identical, and beats the through hole of Φ 5mm along thickness direction at the sample center, and draw speed is 3mm/min.Porose sample unilateral stretching finite element model parameter comprises: sample adopts the S4R mesh discretization, and the size of mesh opening of bare terminal end is that size of mesh opening is that 0.8mm, remainder size of mesh opening are 1.5mm around 2mm, the hole.Adopt this finite element model,, simulate different constitutive parameter combination (K according to the quadrature arranging scheme that step 2 is confirmed Sim, n Sim) under porose sample unilateral stretching process.Obtain maximum stretching force and corresponding sample marking distance elongation in the simulation process.5s extracts 5 tensile forces and corresponding sample marking distance elongation data equably in the time before this maximum stretching force occurs then, and back 4s extracts 4 tensile forces and correspondence equably in the time sample marking distance elongation data occur at this maximum stretching force.Thereby obtain every group of constitutive parameter combination (K Sim, n Sim) with 10 groups of tensile forces and sample marking distance elongation (F Sim, Δ l Sim) corresponding relation.The tensile force F that simulation obtains SimSample marking distance elongation Δ l with correspondence SimData are as shown in table 5.
Table 5: the quadrature collocation analog result of instance 1
Figure BSA00000337395600081
Step 4 is set up the combination of the combination of tensile force and elongation between gages amount (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n)
Structure comprises the error back propagation artificial neural network of three layers of input layers, latent layer, output layer.Wherein, the node number of input layer, latent layer, output layer is respectively 20,8 and 2; And the training function of network using is the Levenberg-Marquardt function; The transport function of input layer-latent interlayer is Tangent sigmoid, and the transport function between latent layer-output layer is the linear function.With tensile force that obtains in the step 4 and elongation between gages amount combination (F Sim, Δ l Sim) as the input vector of artificial neural network, constitutive parameter makes up (K Sim, n Sim) as output vector, this artificial neural network is trained, set up the combination of the combination of tensile force and elongation between gages amount (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n).
Step 5 is carried out the porose sample unilateral stretching experiment of mother metal, obtains the tensile force F in the experiment ExpWith elongation between gages amount Δ l Exp
With the mother metal zone of weld seam symmetry, measure-alike punching sample in intercepting and the step 2 adopts cupping machine that sample is carried out the unilateral stretching experiment of 3mm/min, the sample marking distance elongation of maximum stretching force in obtaining testing and correspondence.5s extracts 5 tensile forces and corresponding sample marking distance elongation data equably in the time before this maximum stretching force occurs then, and back 4s extracts 4 tensile forces and correspondence equably in the time sample marking distance elongation data occur at this maximum stretching force.Thereby obtain 10 groups of tensile forces and sample marking distance elongation (F Exp, Δ l Exp) data are right, see table 6.
Table 6: the experimental result of instance 1
Step 6, constitutive parameter
Figure BSA00000337395600092
and
Figure BSA00000337395600093
of mother metal under the acquisition two-dimensional state of stress
With 10 groups of tensile forces that obtain in step 5 experiment and elongation between gages amount (F Exp, Δ l Exp) data are to as input vector, input has been set up tensile force and has been made up with elongation between gages amount combination (F, Δ l) and constitutive parameter that (K in the artificial neural network of the recessive mapping relations between n), obtains the constitutive parameter of mother metal under two-dimensional state of stress in step 4
Figure BSA00000337395600094
Be 615MPa,
Figure BSA00000337395600095
Be 0.1.
Step 7 is set up the relation between the mother metal flow stress under the single, double stress state
Given strain value variation range ε=[0,0.5], and adopt formula (3) that it is separated into 100 sections.Obtained according to step a base material in the uniaxial stress state constitutive parameters
Figure BSA00000337395600096
and
Figure BSA00000337395600097
using the formula
Figure BSA00000337395600098
get the base material in uniaxial stress state flow stress
Figure BSA00000337395600099
According to the base material obtained in Step 6 biaxial stress state in the constitutive parameters
Figure BSA000003373956000910
and
Figure BSA000003373956000911
using formula
Figure BSA000003373956000912
get the base material in the biaxial stress state flow stress
Figure BSA000003373956000913
using regression analysis to establish the base material under biaxial stress state flow stress and the base material under uniaxial stress state flow stress
Figure BSA00000337395600102
functional relationship between the two (4)
ε j=0.5/100×(j-1)(j=1,…,101) (3)
&sigma; bi b = f ( &sigma; uni b ) - - - ( 4 )
In formula (3), j is with one of them discrete point after being separated into 100 sections between strain regions, ε jIt is the corresponding strain value of j discrete point.In formula (4); is the flow stress of mother metal under uniaxial stressed state;
Figure BSA00000337395600105
is the flow stress of mother metal under two-dimensional state of stress, and f is the funtcional relationship of the two.In the present embodiment, obtain &sigma; Bi b = 1.19 &sigma; Uni b - 78.75 .
Step 8 is carried out the microhardness experiment, confirms weld hardness HV wAnd mother metal hardness HV b
After with sand paper welded tube surface finish to be measured being polished; Along circumferentially pasting a slice coordinate paper, clip pipe fitting on the pipe surface, be put on the testing table with anchor clamps; Begin to measure hardness from the weld seam center; Then pipe is rotated 1mm (the 1mm mesh lines through alignment coordinate paper is realized), clamp pipe once more, measure once more.So repeat, realize the test of butt welded seam and mother metal microhardness.Average again at last, obtain weld hardness HV wBe 206HV, mother metal hardness HV bBe 159HV.
Step 9 is confirmed the flow stress of weld seam under uniaxial stressed state
Flow stress with mother metal under the uniaxial stressed state in [0,0.5] between the given strain regions of step 7 acquisition The weld seam and the mother metal hardness HV that obtain with step 8 w, HV bSubstitution formula (5), the flow stress of weld seam under the acquisition uniaxial stressed state
Figure BSA00000337395600109
&sigma; uni , j w = HV w HV b &sigma; uni , j b , ( j = 1 , &CenterDot; &CenterDot; &CenterDot; , 101 ) - - - ( 5 )
In the formula (5), HV w, HV bBe respectively weld seam and mother metal hardness, j is with one of them discrete point after being separated into 100 sections between strain regions,
Figure BSA000003373956001011
Be respectively weld seam and the mother metal flow stress under uniaxial stressed state.
Step 10 is confirmed the flow stress
Figure BSA000003373956001012
of weld seam under two-dimensional state of stress
Between the given strain regions that step 9 is obtained [0; 0.5] in
Figure BSA000003373956001013
substitution formula (6) in the scope, obtain the flow stress
Figure BSA000003373956001014
between this strain regions of weld seam under the two-dimensional state of stress
Step 11 is confirmed constitutive parameter
Figure BSA000003373956001015
and
Figure BSA000003373956001016
of weld seam under two-dimensional state of stress
Flow stress according to weld seam under the two-dimensional state of stress in [0,0.5] scope between the strain regions of step 10 acquisition
Figure BSA000003373956001017
With strain stress jData, employing formula (6), formula (7) obtain the strength factor of the weld seam of weld seam under two-dimensional state of stress
Figure BSA000003373956001018
Be 820MPa, hardenability value Be 0.0964.
n bi w = 101 &CenterDot; &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) &CenterDot; ( lg &sigma; &OverBar; bi , j w ) - &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) &CenterDot; &Sigma; j = 1 101 ( lg &sigma; bi , j w ) 101 &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) 2 - [ &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) ] 2 - - - ( 6 )
K bi w = exp [ &Sigma; j = 1 101 ( lg &sigma; bi , j w ) - n bi w &Sigma; j = 1 101 ( lg &epsiv; &OverBar; j ) 101 ] - - - ( 7 )
In formula (6), (7),
Figure BSA00000337395600113
is the flow stress of weld material under two-dimensional state of stress; is the strength factor of weld material under two-dimensional state of stress;
Figure BSA00000337395600115
is the hardenability value of weld material under two-dimensional state of stress; ε is strain.

Claims (2)

1. the method for straight welded pipe welding-seam constitutive parameter under the definite two-dimensional state of stress is characterized in that the detailed process of straight welded pipe welding-seam constitutive parameter is following under described definite two-dimensional state of stress:
Step 1; Carry out mother metal unilateral stretching experiment, confirm constitutive parameter
Figure FSB00000843223300011
and of mother metal under uniaxial stressed state
From with the mother metal position of the weld seam symmetry vertical standard arc tensile sample of intercepting total wall thickness vertically, wherein scale-up factor gets 5.65; This sample is carried out the unilateral stretching experiment; Obtain the flow stress-logarithmic strain data of mother metal in the drawing process, employing formula (1), formula (2) obtain constitutive parameter and of mother metal under uniaxial stressed state
n uni b = N &CenterDot; &Sigma; j = 1 N ( lg &epsiv; j ) &CenterDot; ( lg &sigma; uni , j b ) - &Sigma; j = 1 N ( lg &epsiv; j ) &CenterDot; &Sigma; j = 1 N ( lg &sigma; uni , j b ) N &Sigma; j = 1 N ( lg &epsiv; j ) 2 - [ &Sigma; j = 1 N ( lg &epsiv; j ) ] 2 - - - ( 1 )
K uni b = exp [ &Sigma; j = 1 N ( lg &sigma; uni , j b ) - n uni b &Sigma; j = 1 N ( lg &epsiv; j ) N - - - ( 2 )
In formula (1), (2);
Figure FSB00000843223300017
is the flow stress under the mother metal uniaxial stressed state; ε is the logarithmic strain under the mother metal uniaxial stressed state; N is the flow stress-logarithmic strain data set number under the mother metal uniaxial stressed state that obtains in the stretching experiment; is the strength factor in the constitutive parameter under the mother metal uniaxial stressed state, and
Figure FSB00000843223300019
is the hardenability value in the constitutive parameter under the mother metal uniaxial stressed state;
Step 2 is confirmed the quadrature arranging scheme of the porose sample stretching of mother metal sunykatuib analysis; According to the strength factor in the constitutive parameter of mother metal under the uniaxial stressed state that obtains in the step 1
Figure FSB000008432233000110
And hardenability value
Figure FSB000008432233000111
Confirm the strength factor K in the mother metal constitutive parameter in the porose sample stretching finite element analogy SimScope do
Figure FSB000008432233000112
Hardenability value n in the mother metal constitutive parameter SimScope do
Figure FSB000008432233000113
And the variation range of strength factor in the mother metal constitutive parameter and hardenability value two factors is divided into 3~4 levels, corresponding factor level table is seen table 1 and table 2:
Table 1: the factor level table when strength factor and hardenability value are got 3 levels
Figure FSB000008432233000114
Table 2: the factor level table when strength factor and hardenability value are got 4 levels
Figure FSB00000843223300021
Corresponding to the factor level number is that 3 and 4 orthogonal table is confirmed as L respectively 9(3 4) and L 16(4 5); Certain that then strength factor and hardenability value two factors is put into selected orthogonal table two lists, thereby obtains the orthogonal experiment arranging scheme of porose sample stretching sunykatuib analysis;
Step 3 is confirmed different constitutive parameter combination (K Sim, n Sim) and simulate tensile force and the sample marking distance elongation combination (F that obtains Sim, Δ l Sim) corresponding relation; Set up the porose sample unilateral stretching of mother metal finite element model; The porose specimen configuration size wherein and the physical dimension of the vertical standard arc tensile sample of total wall thickness are identical, and beat the through hole of Φ 5mm along thickness direction at the sample center, and draw speed is 3mm/min;
According to the quadrature arranging scheme that step 2 is confirmed, simulate different constitutive parameter combination (K Sim, n Sim) under porose sample unilateral stretching process, obtain maximum stretching force and corresponding sample marking distance elongation in the simulation process; 5s extracts 5 tensile forces and corresponding sample marking distance elongation data equably in the time before this maximum stretching force occurs; And 4s extracts 4 tensile forces and corresponding sample marking distance elongation data equably in the time after this maximum stretching force occurs, thereby obtains every group of constitutive parameter combination (K Sim, n Sim) the 10 groups of tensile forces and the sample marking distance elongation (F that obtain with simulation Sim, Δ l Sim) corresponding relation;
Step 4 is set up the combination of the combination of tensile force and sample marking distance elongation (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n); Structure comprises the error back propagation artificial neural network of three layers of input layers, latent layer, output layer; Wherein, the node number of input layer, latent layer, output layer is respectively 20,8 and 2; And the training function of network using is the Levenberg-Marquardt function; The transport function of input layer-latent interlayer is Tangent sigmoid, and the transport function between latent layer-output layer is the linear function; Tensile force and sample marking distance elongation that simulation in the step 3 is obtained make up (F Sim, Δ l Sim) as the input vector of artificial neural network, constitutive parameter makes up (K Sim, n Sim) as output vector, this artificial neural network is trained, set up the combination of the combination of tensile force and sample marking distance elongation (F, Δ l) and constitutive parameter (K, the recessive mapping relations between n);
Step 5 is carried out the porose sample unilateral stretching experiment of mother metal, obtains the tensile force F in the experiment ExpWith sample marking distance elongation Δ l ExpWith the mother metal zone of weld seam symmetry, measure-alike punching sample in intercepting and the step 2 carries out the unilateral stretching experiment of 3mm/min to sample, the sample marking distance elongation of maximum stretching force in obtaining testing and correspondence; 5s is in the time before this maximum stretching force occurs; Extract 5 tensile forces and corresponding sample marking distance elongation data equably; And 4s extracts 4 tensile forces and corresponding sample marking distance elongation data equably in the time after this maximum stretching force occurs, thereby obtains the tensile force and the sample marking distance elongation (F of 10 groups of experiments Exp, Δ l Exp) data are right;
Step 6, the constitutive parameter of mother metal under the acquisition two-dimensional state of stress
Figure FSB00000843223300031
With
Figure FSB00000843223300032
10 groups of tensile forces that step 5 is obtained through experiment and sample marking distance elongation (F Exp, Δ l Exp) reflection tensile force and the sample marking distance elongation combination (F of data to having set up in step 4 as input vector input; Δ l) with constitutive parameter combination (K; In the artificial neural network of the recessive mapping relations n), obtain the constitutive parameter of mother metal under two-dimensional state of stress
Figure FSB00000843223300033
With
Figure FSB00000843223300034
Step 7, the establishment of a single, double base material stress state the relationship between flow stress; given range value true strain ε = [0,0.5], and using equation (3) to be discretized into 100; obtained according to step 1 The base material in the uniaxial stress state constitutive parameters and
Figure FSB00000843223300036
using the formula
Figure FSB00000843223300037
get the base material in uniaxial stress state flow stress
Figure FSB00000843223300038
according to step 6 base material obtained biaxial stress state in the constitutive parameters
Figure FSB00000843223300039
and
Figure FSB000008432233000310
using the formula
Figure FSB000008432233000311
get parent material biaxial stress state in the flow stress
Figure FSB000008432233000312
using regression analytical methods to establish the base material under biaxial stress state flow stress and the base material under uniaxial stress state flow stress
Figure FSB000008432233000314
functional relationship between the two (4)
ε j=0.5/100×(j-1)(j=1,…,101) (3)
&sigma; bi b = f ( &sigma; uni b ) - - - ( 4 )
In formula (3), j is one of them discrete point after the logarithmic strain interval is separated into 100 sections, ε jIt is the corresponding logarithmic strain value of j discrete point.In formula (4);
Figure FSB000008432233000316
is the flow stress of mother metal under uniaxial stressed state; is the flow stress of mother metal under two-dimensional state of stress, and f is the funtcional relationship of the two;
Step 8 is carried out the microhardness experiment, confirms weld hardness HV wAnd mother metal hardness HV bAfter with sand paper welded tube surface finish to be measured being polished, along circumferentially pasting a slice coordinate paper, clip pipe fitting, be put on the testing table, begin to measure hardness from the weld seam center with anchor clamps on the pipe surface; Pipe is rotated 1mm, clamp pipe once more, measure once more; So repeat, till pipe rotated for 1 week, obtain the hardness HV of weld seam wAnd the hardness HV of mother metal b
Step 9 is confirmed the flow stress of weld seam under uniaxial stressed state Flow stress with mother metal under the uniaxial stressed state in the given logarithmic strain interval [0,0.5] of step 7 acquisition
Figure FSB000008432233000319
The weld seam and the mother metal hardness HV that obtain with step 8 w, HV bSubstitution formula (5), the flow stress of weld seam under the acquisition uniaxial stressed state
&sigma; uni , j w = HV w HV b &sigma; uni , j b ( j = 1 , &CenterDot; &CenterDot; &CenterDot; , 101 ) - - - ( 5 )
In the formula (5), HV w, HV bBe respectively weld seam and mother metal hardness, j is one of them discrete point after the logarithmic strain interval is separated into 100 sections, Be respectively weld seam and the mother metal flow stress under uniaxial stressed state;
Step 10; Confirm the given logarithmic strain interval [0 that the flow stress
Figure FSB00000843223300044
of weld seam under two-dimensional state of stress obtains step 9; 0.5] in
Figure FSB00000843223300045
substitution formula (4) in the scope, obtain the flow stress
Figure FSB00000843223300046
of weld seam in this logarithmic strain interval under the two-dimensional state of stress
Step 11 is confirmed the constitutive parameter of weld seam under two-dimensional state of stress
Figure FSB00000843223300047
With
Figure FSB00000843223300048
Flow stress according to weld seam under the two-dimensional state of stress in interval [0, the 0.5] scope of the logarithmic strain of step 10 acquisition
Figure FSB00000843223300049
With logarithmic strain ε jData, employing formula (6), formula (7) obtain the constitutive parameter of weld seam under two-dimensional state of stress With
Figure FSB000008432233000411
n bi w = 101 &CenterDot; &Sigma; j = 1 101 ( lg &epsiv; j ) &CenterDot; ( lg &sigma; bi , j w ) - &Sigma; j = 1 101 ( lg &epsiv; j ) &CenterDot; &Sigma; j = 1 101 ( lg &sigma; bi , j w ) 101 &Sigma; j = 1 101 ( lg &epsiv; j ) 2 - [ &Sigma; j = 1 101 ( lg &epsiv; j ) ] 2 - - - ( 6 )
K bi w = exp [ &Sigma; j = 1 101 ( lg &sigma; bi , j w ) - n bi w &Sigma; j = 1 101 ( lg &epsiv; j ) 101 ] - - - ( 7 )
In formula (6), (7),
Figure FSB000008432233000414
is the flow stress of weld material under two-dimensional state of stress; is the strength factor of weld material in the constitutive parameter under the two-dimensional state of stress;
Figure FSB000008432233000416
is the hardenability value of weld material in the constitutive parameter under the two-dimensional state of stress; ε is logarithmic strain.
2. the method for straight welded pipe welding-seam constitutive parameter under a kind of according to claim 1 definite two-dimensional state of stress; It is characterized in that; The porose specimen configuration size in the described step 3 and the physical dimension of the vertical standard arc tensile sample of total wall thickness are identical, and beat the through hole of Φ 5mm along thickness direction at the sample center.
CN201010535573A 2010-11-04 2010-11-04 Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state Active CN102004819B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201010535573A CN102004819B (en) 2010-11-04 2010-11-04 Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201010535573A CN102004819B (en) 2010-11-04 2010-11-04 Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state

Publications (2)

Publication Number Publication Date
CN102004819A CN102004819A (en) 2011-04-06
CN102004819B true CN102004819B (en) 2012-10-10

Family

ID=43812179

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201010535573A Active CN102004819B (en) 2010-11-04 2010-11-04 Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state

Country Status (1)

Country Link
CN (1) CN102004819B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102768312B (en) * 2011-04-30 2014-11-26 深圳光启高等理工研究院 Test point selection method and device for artificial electromagnetic material unit
CN102410957B (en) * 2011-07-25 2014-04-02 西北工业大学 Test sample and method for testing performance parameters of pipe under complex stress state
CN102680331B (en) * 2012-05-14 2014-01-15 湖北航天技术研究院总体设计所 Check method for shear strength of welding joint of linear welding seam
CN107330137A (en) * 2017-05-17 2017-11-07 武汉工程大学 A kind of metal material cuts the discrimination method of Parameters of constitutive model
CN109870362B (en) * 2019-03-04 2020-04-03 燕山大学 Method and system for establishing fracture forming limit diagram of high-strength aluminum alloy plate
CN113567238B (en) * 2021-06-25 2024-05-14 鞍钢股份有限公司 Uniaxial biaxial stretching curve processing method
CN116227282B (en) * 2023-02-01 2023-12-08 中国石油大学(北京) Method and equipment for determining stress-strain relation parameters of girth weld zone material

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101692028A (en) * 2009-09-10 2010-04-07 上海交通大学 Method for measuring large deformation flow stress curve of metal plate

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101379381B (en) * 2006-02-01 2012-08-22 新日本制铁株式会社 Breaking prediction method

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101692028A (en) * 2009-09-10 2010-04-07 上海交通大学 Method for measuring large deformation flow stress curve of metal plate

Also Published As

Publication number Publication date
CN102004819A (en) 2011-04-06

Similar Documents

Publication Publication Date Title
CN102004819B (en) Method for determining constitutive parameters of butt welded pipe welding seam in biaxial stress state
Zhao et al. Structural performance of stainless steel circular hollow sections under combined axial load and bending–Part 1: Experiments and numerical modelling
CN102288499B (en) Detection method for identifying static mechanical performance parameters of materials in different regions of weld joint
Ashraf et al. Finite element modelling of structural stainless steel cross-sections
CN102410957B (en) Test sample and method for testing performance parameters of pipe under complex stress state
Zribi et al. Experimental characterization and inverse constitutive parameters identification of tubular materials for tube hydroforming process
Tong et al. Experimental investigation on longitudinal residual stresses for cold-formed thick-walled square hollow sections
CN103048203A (en) Wall thickness linear model-based pipe mechanical property hydro-bugling testing method
Lee et al. Development of a hollow cylinder test for the elastic modulus distribution and the ultimate strength of bamboo
CN109396226A (en) A kind of bending pipes neutral line deviation post determines method
CN107121337B (en) The method that fracture toughness and intensity are determined by the small-size test piece of bilateral joint-cutting
Kibey et al. Tensile strain capacity equations for strain-based design of welded pipelines
Manes et al. The behaviour of an offshore steel pipeline material subjected to bending and stretching
Wang et al. Pin-ended press-braked S960 ultra-high strength steel angle section columns: Testing, numerical modelling and design
US8511178B2 (en) Screening test for stretch flanging a trimmed metal surface
CN106644712A (en) Testing method for automatically measuring thickness thinning rate by adopting tensile testing machine
CN103969128A (en) Method for detecting bending mechanical property of sample
Ren et al. Constraining effects of weld and heat-affected zone on deformation behaviors of welded tubes in numerical control bending process
Yang et al. Residual stress in high-strength-steel welded circular tube
CN106769439A (en) A kind of method of testing of line steel hot rolling roll bending yield strength
Chen et al. Parametric study and formulae of SCFs for positive large eccentricity CHS N-joints
CN105928784B (en) The method for measuring fracture toughness under hot rolling carbon steel plane stress condition
Shi-lang et al. Determination of crack initiation and equivalent crack length of low strength concrete using strain gauges
CN105158326A (en) Detection method for measuring content of martensite in austenitic stainless steel
Han et al. Experimental investigation and theoretical analysis of roll forming of electrical resistance welded pipes

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant