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CN112685945B - A magnetic-structural multiphysics topology optimization design method for additive manufacturing - Google Patents

A magnetic-structural multiphysics topology optimization design method for additive manufacturing Download PDF

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CN112685945B
CN112685945B CN202110031589.1A CN202110031589A CN112685945B CN 112685945 B CN112685945 B CN 112685945B CN 202110031589 A CN202110031589 A CN 202110031589A CN 112685945 B CN112685945 B CN 112685945B
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白影春
王子祥
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Beijing Institute of Technology BIT
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Abstract

本申请公开了一种面向增材制造的磁‑结构多物理场拓扑优化设计方法,包括:步骤10,结合待打印物体的单元打印密度,基于结构场和磁场材料插值模型和有限元分析方法,分析获得结构位移矢量和磁场矢量,据此建立目标函数,并结合体积约束条件,建立磁‑结构多物理场拓扑优化模型;步骤20,根据磁‑结构多物理拓扑优化模型,结合目标函数和约束对单元设计密度灵敏度,通过MMA算法对单元设计密度空间进行迭代更新,当判定磁‑结构多物理场拓扑优化模型中目标函数的相对误差小于预设阈值时,根据更新后的单元设计密度空间对待打印物体进行打印。通过本申请中的技术方案,在兼顾磁场和结构场性能的同时,实现了结构的自支撑打印,避免了支撑材料的使用。

Figure 202110031589

The present application discloses a magnetic-structure multi-physics field topology optimization design method for additive manufacturing, comprising: step 10, combining the unit printing density of the object to be printed, based on the structural field and magnetic field material interpolation model and the finite element analysis method, Analyzing and obtaining the structural displacement vector and the magnetic field vector, and establishing the objective function accordingly, and combining the volume constraints to establish a magnetic-structural multi-physics topology optimization model; Step 20, combining the objective function and constraints according to the magnetic-structural multi-physics topology optimization model For the cell design density sensitivity, the cell design density space is iteratively updated by the MMA algorithm. When it is determined that the relative error of the objective function in the magnetic-structural multiphysics topology optimization model is less than the preset threshold, the cell design density space is treated according to the updated cell design density space. Print the object for printing. Through the technical solution in the present application, the self-supporting printing of the structure is realized while taking into account the performance of the magnetic field and the structural field, and the use of supporting materials is avoided.

Figure 202110031589

Description

一种面向增材制造的磁-结构多物理场拓扑优化设计方法A magnetic-structural multiphysics topology optimization design method for additive manufacturing

技术领域technical field

本申请涉及工程结构与分析的技术领域,具体而言,涉及一种面向增材制造的磁-结构多物理场拓扑优化设计方法。The present application relates to the technical field of engineering structure and analysis, and in particular, to a magnetic-structural multiphysics topology optimization design method for additive manufacturing.

背景技术Background technique

近年来,伴随着装备自动化、智能化、轻量化的发展,对以新能源汽车电机和电磁执行器等为代表的部件的集成设计要求越来越高,这些部件既要满足磁场的性能要求,同时还要满足刚度和强度等机械性能要求。通过开展磁-结构多物理场的拓扑优化设计,使得在兼顾轻量化下有效提升磁场和结构场性能。In recent years, with the development of equipment automation, intelligence and light weight, the integrated design requirements for components represented by new energy vehicle motors and electromagnetic actuators have become higher and higher. These components must not only meet the performance requirements of the magnetic field, At the same time, mechanical properties such as stiffness and strength must be met. By carrying out the topology optimization design of the magnetic-structural multi-physics field, the performance of the magnetic field and the structural field can be effectively improved while taking into account the light weight.

增材制造技术的发展,对磁-结构多物理场拓扑设计构型,提供了制造保证。尽管增材制造相对于减材或等材制造而言,大大提高了设计和制造自由度。The development of additive manufacturing technology provides a manufacturing guarantee for the magnetic-structural multiphysics topology design configuration. Although additive manufacturing greatly increases design and manufacturing freedom relative to subtractive or isomaterial manufacturing.

然而仍存在一些制造性约束,如当拓扑构型超过最大悬挂约束时,需要添加支撑材料才能进行打印加工,导致增加了不必要的材料成本和后处理成本。However, there are still some manufacturing constraints, such as when the topological configuration exceeds the maximum suspension constraint, support materials need to be added to print, resulting in unnecessary material costs and post-processing costs.

文献“Garibaldi M,Gerada C,Ashcroft I A.Free-Form Design of ElectricalMachine Rotor Cores for Production Using Additive Manufacturing.Journal ofMechanical Design.2019,141(7):1-13”介绍了一种面向磁-机械场耦合的拓扑优化方法,并使用这种方法对电机转子进行设计。该文章中拓扑优化设计的目标函数是机械场柔度最小和转子磁场能量最小,约束条件是体积分数,最终得到的转子结构大大提升了转矩性能的同时减小了转子质量。但在考虑多物理场时没有考虑增材制造性约束,存在增材制造过程中需要用到支撑材料的问题,增加了材料成本和后处理成本。The paper "Garibaldi M, Gerada C, Ashcroft I A. Free-Form Design of ElectricalMachine Rotor Cores for Production Using Additive Manufacturing. Journal of Mechanical Design. 2019, 141(7): 1-13" introduces a magneto-mechanical field oriented Coupled topology optimization method, and use this method to design the motor rotor. The objective functions of the topology optimization design in this paper are the minimum mechanical field compliance and the minimum rotor magnetic field energy, and the constraint condition is the volume fraction. The final rotor structure greatly improves the torque performance and reduces the rotor mass. However, the additive manufacturing constraints are not considered when considering multiphysics, and there is a problem that support materials need to be used in the additive manufacturing process, which increases material costs and post-processing costs.

文献“Langelaar M.An additive manufacturing filter for topologyoptimization of print-ready designs.Structural and MultidisciplinaryOptimization,2017,55(3):871–83.”介绍了一种嵌入到SIMP方法中的增材制造过滤器,能够通过映射函数将蓝图密度转换为打印密度,最终得到的构型不违反45°的最大悬挂约束,所以能够自支撑打印。该工作主要考虑面向增材制造的机械场性能的拓扑优化设计,但其灵敏度优化运算较为复杂,对计算机硬件性能要求较高。The paper "Langelaar M. An additive manufacturing filter for topologyoptimization of print-ready designs. Structural and MultidisciplinaryOptimization, 2017, 55(3): 871–83." introduces an additive manufacturing filter embedded in the SIMP method, capable of The blueprint density is converted to the print density by the mapping function, and the final configuration does not violate the maximum suspension constraint of 45°, so it can be self-supporting printing. This work mainly considers the topology optimization design of the mechanical field performance for additive manufacturing, but its sensitivity optimization operation is relatively complex and requires high computer hardware performance.

发明内容SUMMARY OF THE INVENTION

本申请的目的在于:提高复杂装备磁-结构多物理场拓扑优化构型的增材制造性,在拓扑优化模型构建中充分考虑无支撑等增材制造约束。将增材制造约束嵌入磁-结构拓扑优化设计模型中,以实现结构的自支撑打印,提高结构的性能,减轻结构的质量,减少结构的制造成本。可以在兼顾轻量化的同时,有效提升磁场和机械场性能。The purpose of this application is to improve the additive manufacturing capability of the magnetic-structure multiphysics topology optimization configuration of complex equipment, and fully consider the additive manufacturing constraints such as unsupported in the construction of the topology optimization model. Additive manufacturing constraints are embedded in the magneto-structural topology optimization design model to enable self-supporting printing of structures, improve the performance of the structures, reduce the mass of the structures, and reduce the manufacturing costs of the structures. It can effectively improve the magnetic field and mechanical field performance while taking into account the light weight.

本申请的技术方案是:提供了一种面向增材制造的磁-结构多物理场拓扑优化设计方法,该方法包括:步骤10,将待打印物体的单元打印密度作为插值,计算整体位移向量和整体磁矢量势向量,并根据整体位移向量和整体磁矢量势向量,生成约束条件,建立磁-结构多物理场拓扑优化模型,其中,单元打印密度由单元设计密度空间确定;步骤20,根据灵敏度和磁-结构多物理场拓扑优化模型,对单元设计密度空间进行迭代更新,当判定磁-结构多物理场拓扑优化模型中目标函数的相对误差小于预设阈值时,根据更新后的单元设计密度空间对待打印物体进行打印。The technical solution of the present application is to provide a magnetic-structural multi-physics topology optimization design method for additive manufacturing, the method comprising: step 10, using the unit printing density of the object to be printed as an interpolation, calculating the overall displacement vector and The overall magnetic vector potential vector, and the constraint conditions are generated according to the overall displacement vector and the overall magnetic vector potential vector, and a magneto-structural multiphysics topology optimization model is established, wherein the unit printing density is determined by the unit design density space; Step 20, according to the sensitivity and the magnetic-structural multiphysics topology optimization model to iteratively update the element design density space. When it is determined that the relative error of the objective function in the magnetic-structural multiphysics topology optimization model is less than the preset threshold, the updated element design density Space to print the object to be printed.

上述任一项技术方案中,进一步地,步骤10,具体包括:步骤11,将待打印物体的设计域进行有限元网格划分,并对有限元网格的单元设计密度空间进行过滤,生成单元打印密度空间,单元打印密度空间为向量矩阵,单元打印密度空间包括多个单元打印密度;步骤12,根据单元打印密度空间中的单元打印密度,对每一个有限元网格的弹性模量和磁导率进行插值,获得单元弹性模量和单元磁导率;步骤13,根据单元弹性模量和单元磁导率,分别对结构场初始单元刚度矩阵、静磁场初始刚度矩阵进行修正,并根据修正后的结构场单元刚度矩阵、静磁场刚度矩阵,计算整体位移向量和整体磁矢量势向量;步骤14,根据整体位移向量和整体磁矢量势向量,计算多物理场问题优化目标函数,并结合体积约束条件,建立磁-结构多物理场拓扑优化模型。In any of the above technical solutions, further, step 10 specifically includes: step 11, performing finite element mesh division on the design domain of the object to be printed, and filtering the element design density space of the finite element mesh to generate a unit The printing density space, the unit printing density space is a vector matrix, and the unit printing density space includes a plurality of unit printing densities; step 12, according to the unit printing density in the unit printing density space, the elastic modulus and magnetic Interpolate the conductivity to obtain the element elastic modulus and element permeability; step 13, according to the element elastic modulus and element permeability, modify the initial element stiffness matrix of the structural field and the initial stiffness matrix of the static magnetic field respectively, and according to the correction After obtaining the structural field element stiffness matrix and the static magnetic field stiffness matrix, calculate the overall displacement vector and the overall magnetic vector potential vector; Step 14, according to the overall displacement vector and the overall magnetic vector potential vector, calculate the multi-physics problem optimization objective function, and combine the volume Constraints, a magnetic-structural multiphysics topology optimization model is established.

上述任一项技术方案中,进一步地,单元设计密度空间和单元打印密度空间为向量矩阵。In any of the above technical solutions, further, the cell design density space and the cell printing density space are vector matrices.

上述任一项技术方案中,进一步地,单元打印密度空间

Figure BDA0002892474140000031
的计算公式为:In any of the above technical solutions, further, the unit prints the density space
Figure BDA0002892474140000031
The calculation formula is:

Figure BDA0002892474140000032
Figure BDA0002892474140000032

Figure BDA0002892474140000033
Figure BDA0002892474140000033

式中,ρs表示单元支撑域,P为第一参数,ε为第二参数,

Figure BDA0002892474140000034
为单元支撑域ρs中的第k个单元的单元打印密度,Q为第三参数。In the formula, ρ s represents the unit support domain, P is the first parameter, ε is the second parameter,
Figure BDA0002892474140000034
is the cell print density for the kth cell in the cell support domain ρs , and Q is the third parameter.

上述任一项技术方案中,进一步地,单元弹性模量

Figure BDA0002892474140000035
和单元磁导率
Figure BDA0002892474140000036
的计算公式为:In any of the above technical solutions, further, the unit elastic modulus
Figure BDA0002892474140000035
and cell permeability
Figure BDA0002892474140000036
The calculation formula is:

Figure BDA0002892474140000041
Figure BDA0002892474140000041

Figure BDA0002892474140000042
Figure BDA0002892474140000042

其中,

Figure BDA0002892474140000043
为过滤后得到的单元打印密度,E0为材料的弹性模量,常数Emin为一常数,vr是材料的相对磁导率,P_s是结构场惩罚参数,P_m是磁场惩罚参数。in,
Figure BDA0002892474140000043
is the unit printing density obtained after filtering, E 0 is the elastic modulus of the material, the constant E min is a constant, v r is the relative magnetic permeability of the material, P_s is the structural field penalty parameter, and P_m is the magnetic field penalty parameter.

上述任一项技术方案中,进一步地,磁-结构多物理场拓扑优化模型中包括目标函数和约束条件,灵敏度为目标函数对单元设计密度空间的灵敏度,灵敏度的计算公式为:In any of the above technical solutions, further, the magnetic-structure multi-physics topology optimization model includes an objective function and a constraint condition, and the sensitivity is the sensitivity of the objective function to the unit design density space, and the calculation formula of the sensitivity is:

Figure BDA0002892474140000044
Figure BDA0002892474140000044

Figure BDA0002892474140000045
Figure BDA0002892474140000045

Figure BDA0002892474140000046
Figure BDA0002892474140000046

式中,ρsd,j-1和ρsd,j分别表示支撑域的第j-1和第j行的单元设计密度向量,c为目标函数,ρj为单元设计密度空间中第j个单元设计密度向量,

Figure BDA0002892474140000047
为单元打印密度空间中第j个单元打印密度向量,ns为支撑域中单元的个数,P为第一参数,ε为第二参数,Q为第三参数。In the formula, ρ sd,j-1 and ρ sd,j represent the element design density vector of the j-1th and jth row of the support domain, respectively, c is the objective function, ρ j is the jth element in the element design density space design density vector,
Figure BDA0002892474140000047
Print the density vector for the jth unit in the unit print density space, ns is the number of units in the support domain, P is the first parameter, ε is the second parameter, and Q is the third parameter.

本申请的有益效果是:The beneficial effects of this application are:

本申请中的技术方案,通过磁-结构多物理场拓扑优化技术,能够在实现轻量化的同时,大幅度提升磁场和机械场的性能,并通过引入增材制造约束成功的将多物理场拓扑优化和增材制造结合起来,使得利用磁-结构多物理场拓扑优化得到的结构,能够不借助支撑材料打印出待打印物体,减少了材料成本和后处理成本。The technical solution in this application, through the magnetic-structural multi-physics topology optimization technology, can greatly improve the performance of the magnetic field and the mechanical field while achieving light weight, and the multi-physics topology can be successfully transformed by introducing additive manufacturing constraints. The combination of optimization and additive manufacturing enables the structure obtained by using the magnetic-structural multiphysics topology optimization to print the object to be printed without the aid of support materials, reducing material costs and post-processing costs.

本申请提出的优化设计方法,稳定性较高、收敛速度较快,拓扑优化中出现的中间密度单元较少,能够很好地推广到面向增材制造其他多物理场拓扑优化设计应用。The optimization design method proposed in this application has high stability, fast convergence speed, and fewer intermediate density cells in topology optimization, which can be well extended to other multi-physics topology optimization design applications for additive manufacturing.

附图说明Description of drawings

本申请的上述和/或附加方面的优点在结合下面附图对实施例的描述中将变得明显和容易理解,其中:The advantages of the above and/or additional aspects of the present application will become apparent and readily understood from the following description of embodiments in conjunction with the accompanying drawings, wherein:

图1是根据本申请的一个实施例的面向增材制造的磁-结构多物理场拓扑优化设计方法的示意流程图;FIG. 1 is a schematic flowchart of a magnetic-structural multiphysics topology optimization design method for additive manufacturing according to an embodiment of the present application;

图2是根据本申请的一个实施例的结构场-磁场作用下的待打印物体的示意图;2 is a schematic diagram of an object to be printed under the action of a structural field-magnetic field according to an embodiment of the present application;

图3是根据本申请的一个实施例的密度空间的示意图;3 is a schematic diagram of a density space according to one embodiment of the present application;

图4是根据本申请的一个实施例的单物理场作用和多物理场作用下的拓扑优化结果示意图;4 is a schematic diagram of a topology optimization result under the action of a single physics field and a multi-physics field according to an embodiment of the present application;

图5是根据本申请的一个实施例的不同打印方向下打印结果的示意图。FIG. 5 is a schematic diagram of printing results in different printing directions according to an embodiment of the present application.

具体实施方式Detailed ways

为了能够更清楚地理解本申请的上述目的、特征和优点,下面结合附图和具体实施方式对本申请进行进一步的详细描述。需要说明的是,在不冲突的情况下,本申请的实施例及实施例中的特征可以相互结合。In order to more clearly understand the above objects, features and advantages of the present application, the present application will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be noted that the embodiments of the present application and the features of the embodiments may be combined with each other unless there is conflict.

在下面的描述中,阐述了很多具体细节以便于充分理解本申请,但是,本申请还可以采用其他不同于在此描述的其他方式来实施,因此,本申请的保护范围并不受下面公开的具体实施例的限制。In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can also be implemented in other ways different from those described herein. Therefore, the protection scope of the present application is not subject to the following disclosure. Restrictions to specific embodiments.

如图1和图2所示,本实施例提供了一种面向增材制造的磁-结构多物理场拓扑优化设计方法,首先对设计域划分有限元网格,并设置初始单元设计密度空间,结合增材制造过滤器的映射,得到单元打印密度空间,在单元打印密度空间的基础上对弹性模量和磁导率进行插值,并利用有限元方法求得磁场机和机械场的响应,在此基础上构建多物理场拓扑优化模型,并采用加权法构造目标函数,最后用优化准则法求解磁-结构多物理场拓扑优化模型,得到最终材料分布,以实现磁-结构多物理场拓扑优化设计。As shown in Figures 1 and 2, this embodiment provides a magnetic-structural multiphysics topology optimization design method for additive manufacturing. First, the design domain is divided into finite element meshes, and the initial element design density space is set. Combined with the mapping of the additive manufacturing filter, the unit printing density space is obtained, the elastic modulus and magnetic permeability are interpolated on the basis of the unit printing density space, and the response of the magnetic field machine and the mechanical field is obtained by using the finite element method. On this basis, a multi-physics topology optimization model is constructed, and the weighted method is used to construct the objective function. Finally, the optimization criterion method is used to solve the magnetic-structural multi-physics topology optimization model, and the final material distribution is obtained to realize the magnetic-structural multi-physics topology optimization. design.

该方法包括:The method includes:

步骤10,将待打印物体的单元打印密度作为插值,计算整体位移向量和整体磁矢量势向量,并根据所述整体位移向量和所述整体磁矢量势向量,生成约束条件,建立磁-结构多物理场拓扑优化模型,其中,所述单元打印密度由单元设计密度空间确定。Step 10: Use the unit printing density of the object to be printed as an interpolation value, calculate the overall displacement vector and the overall magnetic vector potential vector, and generate constraints according to the overall displacement vector and the overall magnetic vector potential vector, and establish a magnetic-structure multi-component. The physics topology optimization model, wherein the cell printing density is determined by the cell design density space.

在本实施例中,步骤10具体包括:In this embodiment, step 10 specifically includes:

步骤11,将待打印物体的设计域进行有限元网格划分,并对有限元网格的单元设计密度空间ρ进行过滤,生成单元打印密度空间

Figure BDA0002892474140000061
其中,单元设计密度空间ρ与单元打印密度空间
Figure BDA0002892474140000062
为向量矩阵,包括多个元素,即ρ=[ρe],
Figure BDA0002892474140000063
ρe为单元设计密度空间ρ中的任一单元的密度,称为单元设计密度,
Figure BDA0002892474140000064
为单元打印密度空间
Figure BDA0002892474140000065
中的任一单元的密度,称为单元打印密度;Step 11: Perform finite element mesh division on the design domain of the object to be printed, and filter the element design density space ρ of the finite element mesh to generate a unit printing density space
Figure BDA0002892474140000061
Among them, the cell design density space ρ and the cell printing density space
Figure BDA0002892474140000062
is a vector matrix, including multiple elements, that is, ρ=[ρ e ],
Figure BDA0002892474140000063
ρ e is the density of any unit in the unit design density space ρ, which is called the unit design density,
Figure BDA0002892474140000064
print density space for cells
Figure BDA0002892474140000065
The density of any unit in the unit is called the unit printing density;

具体的,如图3所示,设定待打印物体(执行器)的衔铁部分为设计域,它既受到了磁场的作用,又受到了结构场的作用,该设计域用于确定磁-结构场作用的边界条件。对由上至下对设计域进行有限元网格划分,划分为30×50的网格,网格类型为四边形单元,将每一个有限元网格作为一个单元。Specifically, as shown in Figure 3, the armature part of the object to be printed (actuator) is set as a design domain, which is affected by both the magnetic field and the structural field, and the design domain is used to determine the magnetic-structure Boundary conditions for field action. The design domain is divided into finite element mesh from top to bottom, divided into 30×50 meshes, the mesh type is quadrilateral element, and each finite element mesh is regarded as a unit.

需要说明的是,本实施例中的结构场可以为机械场。It should be noted that the structural field in this embodiment may be a mechanical field.

本实施例中,给定单元设计密度空间ρ中每一个有限元网格对应的单元设计密度ρe的初始值,设为0.6。设定打印方向为由下至上,对单元设计密度空间ρ进行过滤,得到单元打印密度空间

Figure BDA0002892474140000071
本实施例中对的过滤方法并不限定,如可以采用增材制造过滤器进行过滤。In this embodiment, the initial value of the element design density ρ e corresponding to each finite element mesh in the given element design density space ρ is set to 0.6. Set the printing direction as bottom-up, filter the unit design density space ρ, and obtain the unit printing density space
Figure BDA0002892474140000071
The filtering method in this embodiment is not limited, for example, an additive manufacturing filter can be used for filtering.

需要说明的是,本实施例对单元设计密度空间ρ的过滤是以层为单位,从最底层开始逐层过滤到最顶层,所以,单元打印密度空间

Figure BDA0002892474140000072
中最底层单元的密度即为单元设计密度空间ρ中最底层单元的密度,单元打印密度空间
Figure BDA0002892474140000073
具体的计算公式如下:It should be noted that the filtering of the unit design density space ρ in this embodiment is based on layers, starting from the bottom layer to the top layer by layer. Therefore, the unit printing density space
Figure BDA0002892474140000072
The density of the bottom unit is the density of the bottom unit in the unit design density space ρ, and the unit print density space
Figure BDA0002892474140000073
The specific calculation formula is as follows:

Figure BDA0002892474140000074
Figure BDA0002892474140000074

Figure BDA0002892474140000075
Figure BDA0002892474140000075

式中,ρs表示单元支撑域,即支撑该单元(有限元网格)所需下一层单元的所在区域,第一参数P为控制平滑性参数,第二参数ε为控制近似性参数,这里可以分别取60和10-3,ns为支撑域中单元的个数,这里取值为3,

Figure BDA0002892474140000076
为单元支撑域ρs中的第k个单元的单元打印密度,第三参数Q的计算方式如下:In the formula, ρ s represents the element support domain, that is, the region where the next layer of elements required to support the element (finite element mesh) is located, the first parameter P is the control smoothness parameter, and the second parameter ε is the control approximation parameter, Here we can take 60 and 10 -3 respectively, n s is the number of units in the support domain, here the value is 3,
Figure BDA0002892474140000076
For the cell print density of the kth cell in the cell support domain ρs , the third parameter Q is calculated as follows:

Figure BDA0002892474140000077
ρs0=0.5
Figure BDA0002892474140000077
ρ s0 =0.5

通过对第三参数Q的计算,能够提高单元支撑域计算的准确性,进而保证后续获取到的单元弹性模量

Figure BDA0002892474140000081
和单元磁导率
Figure BDA0002892474140000082
的可靠性,有助于提高磁-结构多物理场拓扑优化模型的精度,保证了待打印物体单元打印密度空间计算的准确性,最终实现了能够不借助支撑材料打印出待打印物体,减少了材料成本和后处理成本。Through the calculation of the third parameter Q, the accuracy of the calculation of the element support domain can be improved, thereby ensuring the subsequent obtained elastic modulus of the element
Figure BDA0002892474140000081
and cell permeability
Figure BDA0002892474140000082
It helps to improve the accuracy of the magnetic-structural multiphysics topology optimization model, ensures the accuracy of the spatial calculation of the printing density of the object to be printed, and finally realizes that the object to be printed can be printed without the aid of supporting materials, reducing the need for Material cost and post-processing cost.

步骤12,根据所述单元打印密度空间

Figure BDA0002892474140000083
中的单元打印密度
Figure BDA0002892474140000084
对每一个有限元网格(单元)的弹性模量E和磁导率ν进行插值,获得单元弹性模量
Figure BDA0002892474140000085
和单元磁导率
Figure BDA0002892474140000086
Step 12, print the density space according to the unit
Figure BDA0002892474140000083
Cell Print Density in
Figure BDA0002892474140000084
Interpolate the elastic modulus E and magnetic permeability ν of each finite element mesh (element) to obtain the element elastic modulus
Figure BDA0002892474140000085
and cell permeability
Figure BDA0002892474140000086

本实施例中,基于SIMP框架搭建拓扑优化算法,对材料的弹性模量和磁导率进行材料插值,得到弹性模量和磁导率对于单元打印密度空间

Figure BDA0002892474140000087
的函数,具体插值后的单元弹性模量
Figure BDA0002892474140000088
和单元磁导率
Figure BDA0002892474140000089
的计算公式如下:In this embodiment, a topology optimization algorithm is built based on the SIMP framework, and material interpolation is performed on the elastic modulus and magnetic permeability of the material to obtain the elastic modulus and magnetic permeability for the unit printing density space
Figure BDA0002892474140000087
The function of , the specific interpolated elastic modulus of the element
Figure BDA0002892474140000088
and cell permeability
Figure BDA0002892474140000089
The calculation formula is as follows:

Figure BDA00028924741400000810
Figure BDA00028924741400000810

Figure BDA00028924741400000811
Figure BDA00028924741400000811

其中,

Figure BDA00028924741400000812
为过滤后得到的单元打印密度,E0为材料的弹性模量,常数Emin为一较小弹性模量值,用于避免结构场整体刚度矩阵奇异,这里取值为10-3;vr是材料的相对磁导率,P_s是结构场惩罚参数,P_m是磁场惩罚参数。in,
Figure BDA00028924741400000812
is the unit printing density obtained after filtering, E 0 is the elastic modulus of the material, and the constant E min is a small elastic modulus value, which is used to avoid the singularity of the overall stiffness matrix of the structure field, and the value here is 10 -3 ; v r is the relative permeability of the material, P_s is the structural field penalty parameter, and P_m is the magnetic field penalty parameter.

步骤13,根据所述单元弹性模量

Figure BDA00028924741400000813
和所述单元磁导率
Figure BDA00028924741400000814
分别对结构场初始单元刚度矩阵、静磁场初始刚度矩阵进行修正,并根据修正后的结构场单元刚度矩阵、静磁场刚度矩阵,计算整体位移向量和整体磁矢量势向量。Step 13, according to the element elastic modulus
Figure BDA00028924741400000813
and the cell permeability
Figure BDA00028924741400000814
The initial element stiffness matrix of the structural field and the initial stiffness matrix of the static magnetic field are revised respectively, and the overall displacement vector and the overall magnetic vector potential vector are calculated according to the revised structural field element stiffness matrix and the static magnetic field stiffness matrix.

根据插值后的单元弹性模量

Figure BDA00028924741400000815
和单元磁导率
Figure BDA00028924741400000816
修正结构场初始单元刚度矩阵和静磁场初始单元刚度矩阵,对应的计算公式为:According to the interpolated element elastic modulus
Figure BDA00028924741400000815
and cell permeability
Figure BDA00028924741400000816
Modify the initial element stiffness matrix of the structural field and the initial element stiffness matrix of the static magnetic field, and the corresponding calculation formula is:

Figure BDA0002892474140000091
Figure BDA0002892474140000091

Figure BDA0002892474140000092
Figure BDA0002892474140000092

其中,

Figure BDA0002892474140000093
为结构场初始单元刚度矩阵,
Figure BDA0002892474140000094
为静磁场初始刚度矩阵,两者可以由有限元方法中的能量原理推导而来。in,
Figure BDA0002892474140000093
is the initial element stiffness matrix of the structural field,
Figure BDA0002892474140000094
is the initial stiffness matrix of the static magnetic field, both of which can be derived from the energy principle in the finite element method.

需要说明的是,在进行有限元网格划分之后,对每个有限元网格的节点,即有限元网格的顶点,进行编号,具体编号方式本实施例并不限定。It should be noted that, after the finite element mesh division is performed, the nodes of each finite element mesh, that is, the vertices of the finite element mesh, are numbered, and the specific numbering method is not limited in this embodiment.

根据有限元网格的节点编号,分别对修正后的结构场单元刚度矩阵ke,s、静磁场刚度矩阵ke,m进行组装,获得对应的整体刚度矩阵,通过求解结构场和静磁场控制方程,可获得结构场响应—整体位移向量

Figure BDA0002892474140000095
和静磁场响应—整体磁矢量势向量
Figure BDA0002892474140000096
对应的计算公式为:According to the node number of the finite element mesh, the modified structural field element stiffness matrix ke,s and the static magnetic field stiffness matrix ke,m are assembled respectively to obtain the corresponding overall stiffness matrix. By solving the structural field and static magnetic field control equation to obtain the structural field response-global displacement vector
Figure BDA0002892474140000095
and the static magnetic field response—the global magnetic vector potential vector
Figure BDA0002892474140000096
The corresponding calculation formula is:

Figure BDA0002892474140000097
Figure BDA0002892474140000097

Figure BDA0002892474140000098
Figure BDA0002892474140000098

式中,

Figure BDA0002892474140000099
为组装后的结构场整体刚度矩阵,
Figure BDA00028924741400000910
是整体位移向量,F是整体力载荷向量,
Figure BDA00028924741400000911
为组装后的静磁场整体刚度矩阵,
Figure BDA00028924741400000912
是整体磁矢量势向量,P是整体激励向量;In the formula,
Figure BDA0002892474140000099
is the overall stiffness matrix of the assembled structural field,
Figure BDA00028924741400000910
is the global displacement vector, F is the global force load vector,
Figure BDA00028924741400000911
is the overall stiffness matrix of the static magnetic field after assembly,
Figure BDA00028924741400000912
is the overall magnetic vector potential vector, and P is the overall excitation vector;

步骤14,根据所述整体位移向量和所述整体磁矢量势向量,计算多物理场问题优化目标函数,并结合体积约束条件,建立磁-结构多物理场拓扑优化模型,所述磁-结构多物理场拓扑优化模型中包括目标函数和所述约束条件。Step 14, according to the overall displacement vector and the overall magnetic vector potential vector, calculate the multi-physics problem optimization objective function, and combine the volume constraints to establish a magnetic-structure multi-physics topology optimization model, the magnetic-structure multi-physics topology optimization model is established. The objective function and the constraints are included in the physics topology optimization model.

本实施例中,目标函数min c是机械柔度最小和磁柔度最小的归一化函数,约束条件至少包括物理场控制方程、构件体积约束和单元设计密度约束,其中,物理场控制方程包括结构场和静磁场控制方程,由所述整体位移向量和所述整体磁矢量势向量决定,磁-结构多物理场拓扑优化模型的计算公式为:In this embodiment, the objective function min c is a normalized function with minimum mechanical compliance and minimum magnetic compliance, and the constraints at least include physical field control equations, component volume constraints and element design density constraints, wherein the physical field control equations include The control equations of the structure field and the static magnetic field are determined by the overall displacement vector and the overall magnetic vector potential vector. The calculation formula of the magneto-structural multiphysics field topology optimization model is:

Figure BDA0002892474140000101
Figure BDA0002892474140000101

Figure BDA0002892474140000102
Figure BDA0002892474140000102

Figure BDA0002892474140000103
Figure BDA0002892474140000103

Figure BDA0002892474140000104
Figure BDA0002892474140000104

0<ρmin≤ρe≤10<ρ min ≤ρ e ≤1

式中,cmeh为结构场目标函数值,cmag为磁场目标函数值,ue是单元位移向量,ae是单元磁矢量势向量,两者可以根据有限元原理通过有限元网格的节点编号分别从整体位移向量

Figure BDA0002892474140000105
和整体磁矢量势向量
Figure BDA0002892474140000106
中提取,ρe是单元设计密度,ke,s为结构场单元刚度矩阵,ke,m静磁场刚度矩阵,In the formula, c meh is the objective function value of the structure field, c mag is the objective function value of the magnetic field, ue is the element displacement vector, and a e is the element magnetic vector potential vector, both of which can pass through the nodes of the finite element mesh according to the finite element principle. Id separately from the overall displacement vector
Figure BDA0002892474140000105
and the overall magnetic vector potential vector
Figure BDA0002892474140000106
Extracted from , ρ e is the element design density, ke,s is the structural field element stiffness matrix, ke,m static magnetic field stiffness matrix,

Cref_mech和Cref_mag是归一化系数,N为设计域内单元个数,本实施例中为1500;ve和V0分别为单元体积和许用体积;ρmin为单元设计密度下限,通常为一较小数值,以防止刚度矩阵奇异;w1和w2为权重系数,可以根据实际工程问题进行调节。C ref_mech and C ref_mag are normalization coefficients, N is the number of units in the design domain, which is 1500 in this embodiment; ve and V 0 are the unit volume and allowable volume, respectively; ρ min is the lower limit of the unit design density, usually A small value to prevent the stiffness matrix from being singular; w 1 and w 2 are weight coefficients, which can be adjusted according to actual engineering problems.

本实例中示出一种权重系数调整的方法,即根据结构场目标函数值cmech、磁场目标函数值cmag,计算权重系数,对应的计算公式为:In this example, a method for adjusting the weight coefficient is shown, that is, the weight coefficient is calculated according to the structure field objective function value c mech and the magnetic field objective function value c mag , and the corresponding calculation formula is:

Figure BDA0002892474140000111
Figure BDA0002892474140000111

Figure BDA0002892474140000112
Figure BDA0002892474140000112

本实施例还示出一种灵敏度的计算方法。This embodiment also shows a calculation method of sensitivity.

具体的,拓扑优化过程中灵敏度至关重要,它是单元设计密度空间更新的依据,因为增材制造过滤器的存在,所以目标函数对初始密度的灵敏度,需要通过链式法则求的:Specifically, the sensitivity is very important in the topology optimization process. It is the basis for updating the density space of the unit design. Because of the existence of the additive manufacturing filter, the sensitivity of the objective function to the initial density needs to be calculated by the chain rule:

Figure BDA0002892474140000113
Figure BDA0002892474140000113

式中c是目标函数,

Figure BDA0002892474140000114
是过滤后的单元密度,ρe是设计单元密度。式中,
Figure BDA0002892474140000115
需要借助伴随方法求得:where c is the objective function,
Figure BDA0002892474140000114
is the filtered cell density and ρ e is the design cell density. In the formula,
Figure BDA0002892474140000115
It needs to be obtained with the help of the accompanying method:

Figure BDA0002892474140000116
Figure BDA0002892474140000116

Figure BDA0002892474140000117
Figure BDA0002892474140000117

Figure BDA0002892474140000118
Figure BDA0002892474140000118

式中的

Figure BDA0002892474140000119
项目计算较为复杂,因为单元打印密度空间中每行元素都是其下层支撑域内单元设计密度空间所有单元的函数,设铺层的顶层为第1层,最底层为第n层,计算单元打印密度空间中第i行对单元设计密度空间中第j行的导数:in the formula
Figure BDA0002892474140000119
The project calculation is more complicated, because each row of elements in the cell printing density space is a function of all the cells in the cell design density space in its underlying support domain. The top layer of the layup is the first layer, and the bottom layer is the nth layer. Calculate the cell printing density Derivative of the ith row in the space to the jth row in the element design density space:

Figure BDA0002892474140000121
Figure BDA0002892474140000121

式中,δij是克罗内克符号,i=j,δij=1或i≠j,δij=0。单元打印密度空间第i行是其单元设计密度空间中下层所有行单元设计密度的函数,因此上式只在i≤j的时候成立,当i>j时,

Figure BDA0002892474140000122
In the formula, δ ij is the Kronecker symbol, i=j, δ ij =1 or i≠j, δ ij =0. The i-th row of the cell printing density space is a function of the cell design density of all the lower rows in its cell design density space, so the above formula is only true when i≤j, and when i>j,
Figure BDA0002892474140000122

本实施例中,目标函数对单元设计密度空间的灵敏度计算公式为:In this embodiment, the calculation formula of the sensitivity of the objective function to the cell design density space is:

Figure BDA0002892474140000123
Figure BDA0002892474140000123

式中未知项

Figure BDA0002892474140000124
Figure BDA0002892474140000125
的计算公式为:The unknown term in the formula
Figure BDA0002892474140000124
and
Figure BDA0002892474140000125
The calculation formula is:

Figure BDA0002892474140000126
Figure BDA0002892474140000126

Figure BDA0002892474140000127
Figure BDA0002892474140000127

式中,ρsd,j-1和ρsd,j分别表示支撑域的第j-1和第j行的单元设计密度向量。where ρ sd,j-1 and ρ sd,j represent the element design density vectors of the j-1th and jth rows of the support domain, respectively.

步骤20,根据灵敏度和磁-结构多物理场拓扑优化模型,通过MMA算法,对单元设计密度空间进行迭代更新,当判定磁-结构多物理场拓扑优化模型中目标函数的相对误差小于预设阈值时,根据更新后的单元设计密度空间对待打印物体进行打印。Step 20, according to the sensitivity and the magnetic-structure multi-physics topology optimization model, through the MMA algorithm, iteratively update the cell design density space, when it is determined that the relative error of the objective function in the magnetic-structure multi-physics topology optimization model is less than a preset threshold value , print the object to be printed according to the updated unit design density space.

具体的,根据灵敏度和磁-结构多物理场拓扑优化模型,通过优化准则法,对单元设计密度空间ρ进行迭代更新,其中,灵敏度为目标函数对单元设计密度空间的灵敏度,可以通过上述计算公式进行计算确定。Specifically, according to the sensitivity and the magnetic-structure multi-physics topology optimization model, the element design density space ρ is iteratively updated through the optimization criterion method, where the sensitivity is the sensitivity of the objective function to the element design density space, which can be calculated by the above formula. Calculate to determine.

若目标函数的相对误差δ小于预设阈值,可设为0.1%,则认为单元设计密度空间ρ收敛,停止迭代,根据更新后的单元设计密度空间ρ,对所述待打印物体进行打印;如果没有达到要求,即目标函数的相对误差δ大于或等于0.1%,则令ρk=ρk+1并返回到步骤11,进行下一轮单元设计密度空间ρ的求解,直到达到收敛条件,得到最终的单元设计密度空间。其中,目标函数的相对误差δ的计算公式为:If the relative error δ of the objective function is less than the preset threshold, which can be set to 0.1%, it is considered that the unit design density space ρ is converged, the iteration is stopped, and the object to be printed is printed according to the updated unit design density space ρ; if If the requirement is not met, that is, the relative error δ of the objective function is greater than or equal to 0.1%, then set ρ k = ρ k+1 and return to step 11 to solve the next round of element design density space ρ until the convergence condition is reached, and obtain Final cell design density space. Among them, the calculation formula of the relative error δ of the objective function is:

Figure BDA0002892474140000131
Figure BDA0002892474140000131

式中,n为迭代次数。where n is the number of iterations.

图4分别给出了仅考虑结构场(机械场)获得的拓扑构型(w1=1,w2=0)、仅考虑磁场作用获得的拓扑构型(w1=0,w2=1)、以及两场同时作用(w1≠0,w2≠1)获得的拓扑构型。由获得的拓扑构型来看,最终结果都可满足45°的最大悬挂角约束,因此满足增材制造约束。图5给出了不同打印方向下得到的磁-结构多物理场拓扑优化构型。Figure 4 shows the topological configuration (w 1 =1,w 2 =0) obtained by considering only the structural field (mechanical field), and the topological configuration (w 1 =0,w 2 =1) obtained by only considering the action of the magnetic field ), and the topological configuration obtained by the simultaneous action of the two fields (w 1 ≠0, w 2 ≠1). From the obtained topological configuration, the final result can satisfy the maximum suspension angle constraint of 45°, thus satisfying the additive manufacturing constraint. Figure 5 shows the magneto-structural multiphysics topology-optimized configurations obtained under different printing directions.

本发明最后输出的构型是单元打印密度空间中的单元呈现的优化构型,由于嵌入了增材制造过滤器的缘故,所有违反最大悬挂角度—45°的部分都被过滤掉,从而保证结构能够实现自支撑打印。The final output configuration of the present invention is the optimized configuration presented by the unit in the unit printing density space. Due to the embedded additive manufacturing filter, all parts that violate the maximum hanging angle of -45° are filtered out, thereby ensuring the structure. Able to achieve self-supporting printing.

以上结合附图详细说明了本申请的技术方案,本申请提出了一种面向增材制造的磁-结构多物理场拓扑优化设计方法,包括:步骤10,将待打印物体的单元打印密度作为插值,计算整体位移向量和整体磁矢量势向量,并根据整体位移向量和整体磁矢量势向量,生成约束条件,建立磁-结构多物理场拓扑优化模型;步骤20,根据灵敏度和磁-结构多物理场拓扑优化模型,对单元设计密度空间进行迭代更新,当判定磁-结构多物理场拓扑优化模型中目标函数的相对误差小于预设阈值时,根据更新后的单元设计密度空间对待打印物体进行打印。通过本申请中的技术方案,实现了结构的自支撑打印,避免了支撑材料的使用。The technical solution of the present application has been described in detail with reference to the accompanying drawings. The present application proposes a magnetic-structural multi-physics topology optimization design method for additive manufacturing, including: step 10, using the unit printing density of the object to be printed as an interpolation , calculate the overall displacement vector and the overall magnetic vector potential vector, and generate constraints according to the overall displacement vector and the overall magnetic vector potential vector, and establish a magnetic-structural multiphysics topology optimization model; Step 20, according to the sensitivity and magnetic-structural multiphysics Field topology optimization model, iteratively updates the cell design density space, when it is determined that the relative error of the objective function in the magnetic-structural multiphysics topology optimization model is less than the preset threshold, print the object to be printed according to the updated cell design density space . Through the technical solution in the present application, the self-supporting printing of the structure is realized, and the use of supporting materials is avoided.

本申请中的步骤可根据实际需求进行顺序调整、合并和删减。The steps in this application can be adjusted, combined and deleted in sequence according to actual needs.

本申请装置中的单元可根据实际需求进行合并、划分和删减。The units in the device of the present application can be combined, divided and deleted according to actual needs.

尽管参考附图详地公开了本申请,但应理解的是,这些描述仅仅是示例性的,并非用来限制本申请的应用。本申请的保护范围由附加权利要求限定,并可包括在不脱离本申请保护范围和精神的情况下针对发明所作的各种变型、改型及等效方案。Although the present application has been disclosed in detail with reference to the accompanying drawings, it should be understood that these descriptions are merely exemplary and are not intended to limit the application of the present application. The protection scope of the present application is defined by the appended claims, and may include various modifications, alterations and equivalent solutions for the invention without departing from the protection scope and spirit of the present application.

Claims (5)

1. An additive manufacturing-oriented magnetic-structure multi-physical field topological optimization design method is characterized by comprising the following steps:
step 10, taking the unit printing density of the object to be printed as an interpolation, calculating an integral displacement vector and an integral magnetic vector potential vector, generating a constraint condition according to the integral displacement vector and the integral magnetic vector potential vector, and establishing a magnetic-structure multi-physical-field topological optimization model, wherein the unit printing density is determined by a unit design density space, the magnetic-structure multi-physical-field topological optimization model comprises a target function and the constraint condition, the sensitivity is the sensitivity of the target function to the unit design density space, and the calculation formula of the sensitivity is as follows:
Figure FDA0003139055770000011
Figure FDA0003139055770000012
Figure FDA0003139055770000013
in the formula, ρsd,j-1And ρsd,jCell design density vectors representing the jth-1 and jth rows of the support domain, respectively, c being the objective function, ρjDesigning a density vector for a jth cell in the cell design density space,
Figure FDA0003139055770000014
printing density for the cellThe jth unit in space prints the density vector, nsThe number of units in the support domain, P is a first parameter, epsilon is a second parameter, and Q is a third parameter;
and 20, iteratively updating the unit design density space according to the sensitivity and the magnetic-structure multi-physical-field topological optimization model, and printing the object to be printed according to the updated unit design density space when the relative error of the objective function in the magnetic-structure multi-physical-field topological optimization model is judged to be smaller than a preset threshold value.
2. The additive manufacturing-oriented magnetic-structure multi-physical-field topological optimization design method according to claim 1, wherein the step 10 specifically comprises:
step 11, performing finite element mesh division on the design domain of the object to be printed, and filtering a unit design density space of the finite element mesh to generate a unit print density space, wherein the unit print density space is a vector matrix and comprises a plurality of unit print densities;
step 12, interpolating the elastic modulus and the magnetic permeability of each finite element grid according to the unit printing density in the unit printing density space to obtain a unit elastic modulus and a unit magnetic permeability;
step 13, respectively correcting the structural field initial unit stiffness matrix and the static magnetic field initial stiffness matrix according to the unit elastic modulus and the unit magnetic permeability, and calculating an integral displacement vector and an integral magnetic vector potential vector according to the corrected structural field unit stiffness matrix and the static magnetic field stiffness matrix;
and 14, calculating a multi-physical-field problem optimization objective function according to the integral displacement vector and the integral magnetic vector potential vector, and establishing the magnetic-structure multi-physical-field topological optimization model by combining with a volume constraint condition.
3. The additive manufacturing oriented magnetic-structure multiphysics field topological optimization design method of claim 2, wherein the cell design density space and the cell print density space are vector matrices.
4. Additive manufacturing oriented magnetic-structure multi-physical field topology optimization design method according to claim 2 or 3, wherein the unit print density space
Figure FDA0003139055770000021
The calculation formula of (2) is as follows:
Figure FDA0003139055770000022
Figure FDA0003139055770000023
in the formula, ρsRepresenting the cell support domain, P is a first parameter, ε is a second parameter,
Figure FDA0003139055770000024
supporting the domain p for the cellsThe unit print density of the kth cell in (1), Q is a third parameter, ρ is a cell design density space, ρeDensity is designed for the cell.
5. The additive manufacturing-oriented magnetic-structure multi-physical-field topological optimization design method of claim 2, wherein the unit elastic modulus
Figure FDA0003139055770000031
And permeability of the cell
Figure FDA0003139055770000032
The calculation formula of (2) is as follows:
Figure FDA0003139055770000033
Figure FDA0003139055770000034
wherein,
Figure FDA0003139055770000035
for the unit print density obtained after filtration, E0Is the modulus of elasticity, constant E, of the materialminIs a constant number of times, and is,ris the relative permeability of the material, P _ s is the structural field penalty parameter, and P _ m is the magnetic field penalty parameter.
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