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CN111855458A - A method for solving the constitutive relation of porous materials based on nanoindentation theory - Google Patents

A method for solving the constitutive relation of porous materials based on nanoindentation theory Download PDF

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CN111855458A
CN111855458A CN202010715942.3A CN202010715942A CN111855458A CN 111855458 A CN111855458 A CN 111855458A CN 202010715942 A CN202010715942 A CN 202010715942A CN 111855458 A CN111855458 A CN 111855458A
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龙旭
贾啟普
李震
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Abstract

本发明涉及电子封装纳米力学性能测试技术领域,具体涉及一种基于纳米压痕理论的多孔材料本构关系求解方法。具体技术方案为:一种基于纳米压痕理论的多孔材料本构关系求解方法,使用纳米压头在多孔材料基体上进行多次压痕,得到多个位移‑载荷曲线,去除误差大的曲线,将其余的曲线进行平均曲线拟合,得到平均曲线,取平均曲线的平均弹性模量作为实验弹性模量E;然后确定特征应力σr,并根据无量纲函数确定硬化指数n;再确定特征应变εr和确定屈服应力σy;最终根据硬化指数n、屈服应力σy和弹性模量E得出本构曲线。本发明解决了现有技术中材料属性与应力应变曲线不是一一对应的关系,以及在仿真时迭代次数较多,所花时间较长的问题。The invention relates to the technical field of nanomechanical performance testing of electronic packaging, in particular to a method for solving the constitutive relationship of porous materials based on nanoindentation theory. The specific technical scheme is as follows: a method for solving the constitutive relationship of porous materials based on the nanoindentation theory, using a nanoindenter to perform multiple indentations on a porous material substrate to obtain multiple displacement-load curves, and remove the curves with large errors, The remaining curves are averaged to obtain the average curve, and the average elastic modulus of the average curve is taken as the experimental elastic modulus E; then the characteristic stress σ r is determined, and the hardening exponent n is determined according to the dimensionless function; then the characteristic strain is determined ε r and determine the yield stress σ y ; finally the constitutive curve is obtained according to the hardening exponent n, the yield stress σ y and the elastic modulus E. The invention solves the problems in the prior art that the material properties and the stress-strain curve are not in a one-to-one correspondence, and the number of iterations during simulation is relatively large and the time spent is relatively long.

Description

一种基于纳米压痕理论的多孔材料本构关系求解方法A method for solving the constitutive relation of porous materials based on nanoindentation theory

技术领域technical field

本发明涉及电子封装纳米力学性能测试技术领域,具体涉及一种基于纳米压痕理论的多孔材料本构关系求解方法。The invention relates to the technical field of nanomechanical performance testing of electronic packaging, in particular to a method for solving the constitutive relationship of porous materials based on nanoindentation theory.

背景技术Background technique

纳米压痕技术是评价涂层和薄膜材料力学性能的一种有效方法。压痕载荷和位移图作为一种先进的微/纳米尺度力学测试技术,被广泛应用于材料力学性能的研究。纳米压痕响应本质上与弹塑性各向同性材料通过不同压痕类型的纳米压痕的应力-应变曲线有关,材料的弹性模量、硬度和塑性可以通过压痕曲线来确定,通常现有的基于有限元模拟的分析方法可分为正演分析和反演分析两大类。正演分析是指在不借助有限元模拟的情况下,根据材料的一系列已知力学参数,预测材料的P-h曲线。正演分析是相当直接的,因为材料的性质是可用的,通常可以很好地验证有限元模型的计算精度。相反,反演分析是指根据已知的压痕P-h曲线来确定材料的力学性能,通常采用更为复杂的方法来研究。但显然,反演分析的作用更大,因为在工程实践中,一些材料的力学性能一直是未知的。Nanoindentation technology is an effective method to evaluate the mechanical properties of coatings and thin films. As an advanced micro/nano scale mechanical testing technique, indentation load and displacement maps are widely used in the study of mechanical properties of materials. The nanoindentation response is essentially related to the stress-strain curves of elastoplastic isotropic materials through nanoindentation of different indentation types. The elastic modulus, hardness and plasticity of materials can be determined from the indentation curves, usually existing The analysis methods based on finite element simulation can be divided into two categories: forward analysis and inversion analysis. Forward analysis refers to predicting the P-h curve of a material based on a series of known mechanical parameters of the material without the aid of finite element simulation. Forward analysis is fairly straightforward because the properties of the material are available and the computational accuracy of the finite element model can often be well verified. In contrast, inversion analysis refers to the determination of the mechanical properties of a material based on known indentation P-h curves, often with more sophisticated methods. But obviously, inversion analysis is more useful, because in engineering practice, the mechanical properties of some materials are always unknown.

此外,根据是否采用无量纲分析理论,反演分析方法可以归纳为两类。一是首先将有限元模拟结果与实验结果进行比较,调整参数,直至拟合误差可接受,最终达到材料的力学性能。在纳米压痕研究的早期阶段,这种基于反向分析的方法得到了广泛的应用。但其数值误差可能无法很好地控制,预测材料参数的正确性在很大程度上取决于输入材料参数的正确性,因此经常出现唯一性问题,材料与应力-应变曲线不是一一对应的关系,并且在仿真时迭代次数较多,所花时间较长。二是首先进行无量纲分析,将有限元结果与无量纲函数联系起来,形成一系列非线性拟合方程,通过计算这些无量纲方程,最终确定材料的力学本构关系。In addition, the inversion analysis methods can be classified into two categories according to whether the dimensionless analysis theory is adopted or not. One is to first compare the finite element simulation results with the experimental results, adjust the parameters until the fitting error is acceptable, and finally achieve the mechanical properties of the material. This inverse analysis-based approach was widely used in the early stages of nanoindentation research. However, its numerical error may not be well controlled, and the correctness of the predicted material parameters depends to a large extent on the correctness of the input material parameters, so the problem of uniqueness often occurs, and the relationship between materials and stress-strain curves is not one-to-one. , and the number of iterations during the simulation is large, which takes a long time. The second is to first carry out a dimensionless analysis, link the finite element results with the dimensionless functions, and form a series of nonlinear fitting equations. By calculating these dimensionless equations, the mechanical constitutive relationship of the material is finally determined.

发明内容SUMMARY OF THE INVENTION

针对现有技术的不足,本发明提供了一种基于纳米压痕理论的多孔材料本构关系求解方法,解决了现有技术中经常出现的唯一性问题,即材料属性与应力应变曲线不是一一对应的关系,以及在仿真时迭代次数较多,所花时间较长的问题。In view of the deficiencies of the prior art, the present invention provides a method for solving the constitutive relation of porous materials based on the nanoindentation theory, which solves the problem of uniqueness that often occurs in the prior art, that is, the material properties and the stress-strain curve are not one-to-one Corresponding relationship, as well as the problem that the number of iterations in the simulation is relatively large and it takes a long time.

为实现以上目的,本发明通过以下技术方案予以实现:To achieve the above purpose, the present invention is achieved through the following technical solutions:

本发明公开了一种基于纳米压痕理论的多孔材料本构关系求解方法,包括以下步骤:The invention discloses a method for solving the constitutive relation of porous materials based on nano-indentation theory, comprising the following steps:

(1)使用纳米压头在多孔基体材料上进行多次压痕,得到多个位移-载荷曲线,去除误差大的曲线,将其余的曲线进行平均曲线拟合,得到平均曲线,将平均曲线作为实验曲线,取平均曲线的平均弹性模量作为实验弹性模量E;(1) Use a nano-indenter to perform multiple indentations on the porous base material to obtain multiple displacement-load curves, remove the curves with large errors, and perform average curve fitting on the remaining curves to obtain the average curve. The average curve is used as For the experimental curve, take the average elastic modulus of the average curve as the experimental elastic modulus E;

(2)特征应力σr的确定:假设两个极端特征应力,采用二分法连续进行有限元模拟,直至有限元模拟得到的位移-载荷曲线与步骤(1)得到的实验曲线完全一致,从而确定特征应力;(2) Determination of the characteristic stress σ r : Assuming two extreme characteristic stresses, the finite element simulation is carried out continuously by the dichotomy method until the displacement-load curve obtained by the finite element simulation is completely consistent with the experimental curve obtained in step (1), so as to determine characteristic stress;

(3)根据无量纲函数确定硬化指数n;(3) Determine the hardening index n according to the dimensionless function;

(4)特征应变εr的确定:假设特征应变的范围,采用二分法连续进行有限元模拟,直到有限元模拟的位移-载荷曲线与步骤(1)得到的实验曲线完全一致,从而确定特征应变;(4) Determination of characteristic strain εr : Assuming the range of characteristic strain, the finite element simulation is carried out continuously by the dichotomy method until the displacement-load curve of the finite element simulation is completely consistent with the experimental curve obtained in step (1), so as to determine the characteristic strain ;

(5)确定屈服应力σy(5) Determine the yield stress σ y ;

(6)根据上述步骤计算得到的硬化指数n、屈服应力σy和弹性模量E得出本构曲线。(6) According to the hardening exponent n, the yield stress σ y and the elastic modulus E calculated by the above steps, the constitutive curve is obtained.

优选的,所述纳米压头为Berkovich压头,压头边缘和中心之间的角线为65.3°和77.05°。Preferably, the nano-indenter is a Berkovich indenter, and the angle between the edge and the center of the indenter is 65.3° and 77.05°.

优选的,硬化指数n的公式如下:Preferably, the formula of the hardening exponent n is as follows:

Figure BDA0002598105470000021
Figure BDA0002598105470000021

式中,A=0.010100×n2+0.0017639×n-0.0040837,In the formula, A=0.010100×n 2 +0.0017639×n-0.0040837,

B=0.14386×n2+0.018153×n-0.088198,B=0.14386×n 2 +0.018153×n-0.088198,

C=0.59505×n2+0.03407×n-0.65417,C=0.59505×n 2 +0.03407×n-0.65417,

D=0.58180×n2-0.088460×n-0.67290;D=0.58180×n 2 -0.088460×n-0.67290;

hr为步骤(2)中的位移-载荷曲线的残余深度。hr is the residual depth of the displacement-load curve in step (2).

优选的,

Figure BDA0002598105470000031
preferably,
Figure BDA0002598105470000031

式中,Ei为纳米压头的杨氏模量;where Ei is the Young's modulus of the nanoindenter;

V为基体材料的泊松比;V is the Poisson's ratio of the matrix material;

Vi为纳米压头的泊松比。Vi is the Poisson's ratio of the nanoindenter.

优选的,屈服应力σy的公式如下:Preferably, the formula of yield stress σ y is as follows:

Figure BDA0002598105470000032
Figure BDA0002598105470000032

式中,R为硬化系数。where R is the hardening coefficient.

优选的,硬化系数R的公式为:

Figure BDA0002598105470000033
Preferably, the formula for the hardening coefficient R is:
Figure BDA0002598105470000033

本发明具备以下有益效果:The present invention has the following beneficial effects:

1.本发明相对与正演分析来说,基于纳米力学相关理论的纳米多孔材料本构关系的求解方法更适用于工程上,并且更适用于未知材料属性的测定,而且方法更加简单。而且,本发明中得到的位移-载荷曲线与实验已知的曲线是完全重合的,从而使得到的未知材料参数是完全一样的,精确性好。1. Compared with forward analysis, the method for solving the constitutive relation of nanoporous materials based on the related theory of nanomechanics is more suitable for engineering, and is more suitable for the determination of unknown material properties, and the method is simpler. Moreover, the displacement-load curve obtained in the present invention completely coincides with the known experimental curve, so that the obtained unknown material parameters are exactly the same, and the accuracy is good.

2.本发明面向封装材料,并且不会出现唯一性问题(唯一性问题是指:多种材料的材料属性可能对应同一种应力应变关系);而且,在仿真中迭代次数少,所用的时间较少;相对于现有的方法拟合的情况更好,材料属性与应力-应变曲线是一一对应的关系。并且,在材料的弹性模量已知的情况下,通过一次压痕就可以得到想要的材料属性。2. The present invention is oriented to packaging materials, and there is no uniqueness problem (the uniqueness problem means that the material properties of multiple materials may correspond to the same stress-strain relationship); moreover, the number of iterations in the simulation is small, and the time used is relatively short. Compared with the existing method, the fitting situation is better, and there is a one-to-one correspondence between material properties and stress-strain curves. Moreover, when the elastic modulus of the material is known, the desired material properties can be obtained by one indentation.

附图说明Description of drawings

图1为本发明结构示意图;Fig. 1 is the structural representation of the present invention;

图2为Sn-Bi合金的压痕响应曲线;Fig. 2 is the indentation response curve of Sn-Bi alloy;

图3为Sn-Bi合金的压痕随深度变化的弹性模量曲线;Fig. 3 is the elastic modulus curve of Sn-Bi alloy indentation as a function of depth;

图4为实施例中特征应力确定图;Fig. 4 is the characteristic stress determination diagram in the embodiment;

图5为实验曲线Test 002与特征应力为80MPa输出的P-h曲线的对比;Figure 5 is the comparison between the experimental curve Test 002 and the P-h curve with a characteristic stress of 80MPa output;

图6为硬化指数确定图;Figure 6 is a diagram for determining the hardening index;

图7为实验曲线Test 002与特征应变为0.027输出的P-h曲线的对比;Figure 7 is the comparison between the experimental curve Test 002 and the P-h curve output with a characteristic strain of 0.027;

图8为屈服应力的确定;Figure 8 is the determination of yield stress;

图9不同参数下反推出的本构曲线;Fig. 9 Constitutive curves deduced under different parameters;

图10为经过有限元仿真得出的荷载-位移曲线;Figure 10 is the load-displacement curve obtained by finite element simulation;

图11为材料的应力应变曲线。Figure 11 shows the stress-strain curve of the material.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

若未特别指明,实施举例中所用的技术手段为本领域技术人员所熟知的常规手段。Unless otherwise specified, the technical means used in the implementation examples are conventional means well known to those skilled in the art.

本发明公开了一种基于纳米压痕理论的多孔材料本构关系求解方法,基本原理是根据abaqus软件,先后根据二分法推算出特征应力和特征应变,之后算出屈服应力,最后便可反推出该种材料的本构关系。The invention discloses a method for solving the constitutive relation of porous materials based on nano-indentation theory. The constitutive relationship of the materials.

具体包括以下步骤:Specifically include the following steps:

(1)参考图1所示,使用纳米压头在多孔材料基体上进行多次压痕,得到多个(或一系列)位移-载荷曲线,去除误差较大或有明显偏差的曲线,将其余的曲线进行平均曲线拟合,具体为在origin软件里进行平均曲线拟合,得到平均曲线,将平均曲线作为实验曲线,取平均曲线的平均弹性模量作为实验弹性模量E;其中,纳米压头为Berkovich压头,压头边缘和中心之间的角线为65.3°和77.05°。(1) Referring to Figure 1, use a nano-indenter to perform multiple indentations on the porous material substrate to obtain multiple (or a series) displacement-load curves, remove the curves with large errors or obvious deviations, and put the rest The average curve fitting is performed on the curve of the original, specifically, the average curve fitting is performed in the origin software to obtain the average curve, the average curve is used as the experimental curve, and the average elastic modulus of the average curve is taken as the experimental elastic modulus E; The head is a Berkovich indenter, and the angles between the edge and the center of the indenter are 65.3° and 77.05°.

(2)特征应力σr的确定:假设多孔材料基体为弹塑性材料,初始屈服应力为特征应力,则可以忽略特征应变的大小。假设两个极端特征应力,采用二分法连续进行有限元模拟,直至有限元模拟得到的位移-载荷曲线与步骤(1)得到的实验曲线完全一致,从而确定特征应力;应该理解的是:各种材料的特征应力的大概范围是清楚的,比如0-1000MPa,先假设特征应力为500MPa,放入有限元仿真软件中,导出位移-载荷曲线,将该曲线跟已知的实验曲线进行对比,如有差距,再在0-500MPa或者500MPa-1000MPa选取一个数,反复进行二分法,最终确定特征应力,特征应变的确定也是如此。(2) Determination of the characteristic stress σ r : Assuming that the matrix of the porous material is an elastic-plastic material and the initial yield stress is the characteristic stress, the magnitude of the characteristic strain can be ignored. Assuming two extreme characteristic stresses, the finite element simulation is carried out continuously by the dichotomy method until the displacement-load curve obtained by the finite element simulation is completely consistent with the experimental curve obtained in step (1), so as to determine the characteristic stress; it should be understood that: various The approximate range of the characteristic stress of the material is clear, such as 0-1000MPa, first assume that the characteristic stress is 500MPa, put it into the finite element simulation software, derive the displacement-load curve, and compare the curve with the known experimental curve, such as If there is a gap, select a number between 0-500MPa or 500MPa-1000MPa, repeat the dichotomy method, and finally determine the characteristic stress, and the same is true for the determination of the characteristic strain.

(3)根据无量纲函数确定硬化指数n,公式如下:(3) Determine the hardening index n according to the dimensionless function, the formula is as follows:

Figure BDA0002598105470000051
Figure BDA0002598105470000051

式中,A=0.010100×n2+0.0017639×n-0.0040837,In the formula, A=0.010100×n 2 +0.0017639×n-0.0040837,

B=0.14386×n2+0.018153×n-0.088198,B=0.14386×n 2 +0.018153×n-0.088198,

C=0.59505×n2+0.03407×n-0.65417,C=0.59505×n 2 +0.03407×n-0.65417,

D=0.58180×n2-0.088460×n-0.67290;D=0.58180×n 2 -0.088460×n-0.67290;

hr为步骤(2)中导出的位移-载荷曲线的残余深度,根据已知的实验曲线,便可测出残余深度hr。残余深度是位移-载荷曲线中完全卸载后的位移,如图10所示,图10中,We为弹性功,Wp为塑性功,Wtotal为压痕中的总功,其值等于We和Wp之和。最大荷载所对应的位移为最大位移hm,完全卸载时的位移为残余位移hr,另外在刚刚进入卸载时(最大荷载处)的斜率为刚度S。hr is the residual depth of the displacement-load curve derived in step (2). According to the known experimental curve, the residual depth hr can be measured. The residual depth is the displacement after complete unloading in the displacement-load curve, as shown in Figure 10, where We e is the elastic work, W p is the plastic work, and W total is the total work in the indentation, and its value is equal to W The sum of e and W p . The displacement corresponding to the maximum load is the maximum displacement h m , the displacement at the time of complete unloading is the residual displacement hr , and the slope just before unloading (at the maximum load) is the stiffness S.

Figure BDA0002598105470000052
Figure BDA0002598105470000052

式中,Ei为纳米压头的杨氏模量;where Ei is the Young's modulus of the nanoindenter;

V为基体材料的泊松比;V is the Poisson's ratio of the matrix material;

Vi为纳米压头的泊松比。Vi is the Poisson's ratio of the nanoindenter.

上述公式(1)适用于分析由Berkovich压头,并且压头边缘和中心之间的角线是65.3°和77.05°。The above formula (1) applies to the analysis of the indenter by Berkovich, and the angles between the edge and the center of the indenter are 65.3° and 77.05°.

(4)特征应变εr的确定:特征应变的确定过程与特征应力的确定类似,通过提供特征应变的可能范围,采用二分法连续进行有限元模拟,调整特征应变的值,直到有限元模拟的位移-载荷曲线与步骤(1)得到的实验曲线完全一致,从而确定特征应变;需要注意的是:与理想弹塑性不同,因幂律函数可以用来描绘金属及其合金的塑性行为,所以此步骤中本构特性是基于幂律函数模型进行估计的。(4) Determination of characteristic strain ε r : The determination process of characteristic strain is similar to the determination of characteristic stress. By providing the possible range of characteristic strain, the finite element simulation is carried out continuously by the bisection method, and the value of characteristic strain is adjusted until the finite element simulation is completed. The displacement-load curve is completely consistent with the experimental curve obtained in step (1), so as to determine the characteristic strain; it should be noted that, unlike the ideal elastic-plastic, the power-law function can be used to describe the plastic behavior of metals and their alloys, so this In-step constitutive properties are estimated based on a power-law function model.

(5)确定屈服应力σy,公式如下:(5) Determine the yield stress σ y , the formula is as follows:

Figure BDA0002598105470000061
Figure BDA0002598105470000061

式中,R为硬化系数,公式为:

Figure BDA0002598105470000062
In the formula, R is the hardening coefficient, and the formula is:
Figure BDA0002598105470000062

应理解为:总应变包括两部分εp和εy,εp代表总应变的非线性部分,参考图11所示,而且,εy很小,相对于εp来说可以忽略不计;图11中,在σ≤σy时属于弹性阶段,σ>σy之后为弹塑性阶段,屈服应力σy所对应的应变为εy,特征应力σr对应的应变为特征应变εr,εp代表总应变的非线性部分。It should be understood that the total strain includes two parts ε p and ε y , and ε p represents the nonlinear part of the total strain, as shown in Fig. 11, and ε y is very small and can be ignored relative to ε p ; Fig. 11 Among them, when σ≤σy belongs to the elastic stage, after σ> σy is the elastic-plastic stage, the strain corresponding to the yield stress σy is ε y , the strain corresponding to the characteristic stress σ r is the characteristic strain ε r , and ε p represents The nonlinear part of the total strain.

(6)根据上述步骤计算得到的硬化指数n、屈服应力σy和弹性模量E得出本构曲线。(6) According to the hardening exponent n, the yield stress σ y and the elastic modulus E calculated by the above steps, the constitutive curve is obtained.

实施例Example

参考图2和图3,根据桂林电子科技大学提供的关于Sn-Bi合金压痕方法测试的响应曲线和随深度变化的弹性模量曲线,本发明采用了图2实验曲线中的Test 001和Test002进行反演计算,弹性模量通过图3进行平均确定。Referring to Fig. 2 and Fig. 3, according to the response curve of Sn-Bi alloy indentation method test and the elastic modulus curve that changes with depth provided by Guilin University of Electronic Science and Technology, the present invention adopts Test 001 and Test 002 in the experimental curve of Fig. 2. An inversion calculation was performed, and the elastic modulus was determined by averaging in Figure 3.

在上述基础上,本发明以Test 002压痕结果为例,开展的详细反演分析,具体步骤如下:On the above basis, the present invention takes the test 002 indentation result as an example to carry out detailed inversion analysis, and the specific steps are as follows:

(1)先确定特征应力σr,如图4所示,假设多孔材料基体为理想弹塑性,给定两个极端特征应力,采用二分法连续进行有限元模拟,直至有限元模拟得到的位移-载荷曲线与实验曲线完全一致,从而确定特征应力σr=80MPa,结果如图5所示。图4中,εy为应力去到屈服应力时对应的应变。(σ=Rεn就是图4所描述的图形,σr=Rεr n是当应力为σr时(σr对应的应变为εr)的一个点的关系式,同理,σ=Eε为前半部分线性的阶段,σy=Eεy是ε为εy时的一个点的关系式)。(1) First determine the characteristic stress σ r , as shown in Fig. 4, assuming that the porous material matrix is ideal elastic-plastic, given two extreme characteristic stresses, the finite element simulation is carried out continuously by the dichotomy method, until the displacement obtained by the finite element simulation is - The load curve is completely consistent with the experimental curve, so that the characteristic stress σ r = 80MPa is determined, and the results are shown in Fig. 5 . In Fig. 4, ε y is the corresponding strain when the stress goes to the yield stress. (σ=Rε n is the graph described in Figure 4, σ r =Rε r n is the relational expression of a point when the stress is σ r (the strain corresponding to σ r is ε r ). Similarly, σ=Eε is In the first half of the linear stage, σ y =Eε y is a relational expression for a point when ε is ε y ).

(2)根据无量纲函数确定硬化指数n,结果如图6所示,根据上述公式(1)求解,硬化指数n=0.305。(2) The hardening exponent n is determined according to the dimensionless function, and the result is shown in Fig. 6 . According to the above formula (1), the hardening exponent n=0.305.

(3)确定特征应变εr,方法与确定特征应力σr的方法相同,确定的特征应变εr=0.027,结果如图7所示。(3) Determining the characteristic strain ε r , the method is the same as the method for determining the characteristic stress σ r , and the determined characteristic strain ε r = 0.027, and the result is shown in Fig. 7 .

(4)确定屈服应力σy,在确定特征应变的值之后,可根据公式(2)推算出屈服应力为20.5MPa,结果如图8所示。(4) Determine the yield stress σ y , after determining the value of the characteristic strain, the yield stress can be calculated to be 20.5 MPa according to formula (2), and the result is shown in Fig. 8 .

图8中式(2)的右边指的是

Figure BDA0002598105470000071
这个函数表达式,该表达式的曲线与80MPa的交点就是屈服应力的解。The right side of equation (2) in Figure 8 refers to
Figure BDA0002598105470000071
This functional expression, the intersection of the curve of this expression and 80MPa is the solution for the yield stress.

(5)根据上述步骤计算出的硬化指数n、屈服应力σy以及已知的弹性模量E,可画出反推的本构曲线,再根据本构曲线得到材料的屈服应力和弹性模量以及材料的应力应变关系。(5) According to the hardening exponent n, the yield stress σ y and the known elastic modulus E calculated by the above steps, the inverse constitutive curve can be drawn, and then the yield stress and elastic modulus of the material can be obtained according to the constitutive curve. and the stress-strain relationship of the material.

对比例Comparative ratio

采用图2实验曲线中的Test 001作为对照实验曲线,采用上述实施例的方法得出n=0.254,特征应力为80MPa,特征应变为0.029,屈服应力为26.8MPa,并且Test001和Test002的曲线差别主要是残余压痕深度和最大压痕深度不同,因此导致本构模型反演计算时参数n的取值不同,参考图9,图9为以Test 002和Test 001为对照试验曲线时所反推的本构曲线。Using Test 001 in the experimental curve of Fig. 2 as the control experimental curve, using the method of the above-mentioned embodiment to obtain n=0.254, the characteristic stress is 80MPa, the characteristic strain is 0.029, the yield stress is 26.8MPa, and the curve difference between Test001 and Test002 is mainly It is because the residual indentation depth and the maximum indentation depth are different, which leads to different values of the parameter n during the inversion calculation of the constitutive model. Referring to Figure 9, Figure 9 is the reverse inference when Test 002 and Test 001 are used as the control test curves. Constitutive Curve.

以上所述的实施例仅是对本发明的优选方式进行描述,并非对本发明的范围进行限定,在不脱离本发明设计精神的前提下,本领域普通技术人员对本发明的技术方案做出的各种变形和改进,均应落入本发明权利要求书确定的保护范围内。The above-mentioned embodiments are only to describe the preferred mode of the present invention, but not to limit the scope of the present invention. Without departing from the design spirit of the present invention, those of ordinary skill in the art can Variations and improvements should fall within the protection scope determined by the claims of the present invention.

Claims (6)

1. A porous material constitutive relation solving method based on a nanoindentation theory is characterized by comprising the following steps: the method comprises the following steps:
(1) carrying out multiple indentation on the porous matrix material by using a nanometer pressure head to obtain a plurality of displacement-load curves, removing curves with large errors, carrying out average curve fitting on the other curves to obtain an average curve, taking the average curve as an experimental curve, and taking the average elastic modulus of the average curve as an experimental elastic modulus E;
(2) characteristic stress sigmarDetermination of (1): assuming two extreme characteristic stresses, continuously performing finite element simulation by adopting a bisection method until a displacement-load curve obtained by finite element simulation is completely consistent with an experimental curve obtained in the step (1), and determining the characteristic stresses;
(3) determining a hardening index n according to a dimensionless function;
(4) characteristic strainrDetermination of (1): assuming the range of the characteristic strain, continuously performing finite element simulation by adopting a bisection method until a displacement-load curve simulated by the finite element is completely consistent with the experimental curve obtained in the step (1), and determining the characteristic strain;
(5) determination of the yield stress sigmay
(6) The hardening index n and the yield stress sigma are calculated according to the stepsyAnd the elastic modulus E to obtain the constitutive curve.
2. The method for solving the constitutive relation of the porous material based on the nanoindentation theory as recited in claim 1, wherein: the nano indenter was a Berkovich indenter with angular lines between the edge and the center of the indenter of 65.3 ° and 77.05 °.
3. The method for solving the constitutive relation of the porous material based on the nanoindentation theory as recited in claim 1, wherein: the formula for the hardening index n is as follows:
Figure FDA0002598105460000011
wherein A is 0.010100 Xn2+0.0017639×n-0.0040837,
B=0.14386×n2+0.018153×n-0.088198,
C=0.59505×n2+0.03407×n-0.65417,
D=0.58180×n2-0.088460×n-0.67290;
hr is the residual depth of the displacement-load curve in step (2).
4. The method for solving the constitutive relation of the porous material based on the nanoindentation theory as recited in claim 3, wherein:
Figure FDA0002598105460000021
wherein Ei is the Young modulus of the nanometer indenter;
v is the Poisson's ratio of the base material;
vi is the Poisson's ratio of the nanometer indenter.
5. The method for solving the constitutive relation of the porous material based on the nanoindentation theory as recited in claim 1, wherein: yield stress sigmayThe formula of (1) is as follows:
Figure FDA0002598105460000022
wherein R is a hardening coefficient.
6. The method for solving the constitutive relation of the porous material based on the nanoindentation theory as recited in claim 5, wherein: the hardening coefficient R is given by:
Figure FDA0002598105460000023
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