CN113312821B - B-spline density method-based topological optimization design method for three-dimensional self-supporting structure - Google Patents

B-spline density method-based topological optimization design method for three-dimensional self-supporting structure Download PDF

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CN113312821B
CN113312821B CN202110620489.2A CN202110620489A CN113312821B CN 113312821 B CN113312821 B CN 113312821B CN 202110620489 A CN202110620489 A CN 202110620489A CN 113312821 B CN113312821 B CN 113312821B
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张卫红
王彻
周璐
高彤
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Northwestern Polytechnical University
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Abstract

The invention relates to a three-dimensional self-supporting structure topology optimization design method based on a B-spline density method. By arranging uniform detection points in the structural domain, the relationship between density values at the detection points is controlled, and the elimination of the reverse taper-like region is realized. By constraining the direction of the density field gradient at the design domain boundary, the special V-shaped cross-sectional features present at the design domain boundary are eliminated. The calculation of the inclination angle of the structural boundary in the invention is more convenient and accurate. The suspension angle constraints introduced by the invention are irrelevant to the finite element grids, so that finite element analysis can be carried out by adopting irregularly-shaped units aiming at a complex-shaped design domain in engineering, and the optimal design of the self-supporting structure under any forming direction is realized.

Description

B-spline density method-based three-dimensional self-supporting structure topology optimization design method
Technical Field
The invention relates to a three-dimensional structure topology optimization design method, in particular to a three-dimensional self-supporting structure topology optimization design method based on a B spline density method.
Background
Additive manufacturing technology is a manufacturing technology that has emerged in recent years to shape structural components by the build-up of materials layer by layer. Compared with the traditional manufacturing technology, the additive manufacturing technology has higher manufacturing freedom degree, and parts with complex shapes can be molded, so that the design space of the structure is enlarged, and the combination of the additive manufacturing technology and the topological optimization design method becomes a hot spot. However, there are still several limitations in additive manufacturing technology, and the dangling portion is one of them. In a conventional additive manufacturing technology, if a suspended portion with a small inclination angle exists in a structure, an auxiliary support structure needs to be added below the suspended portion to prevent collapse in the manufacturing process. The use of support structures results in increased manufacturing costs and time, and may result in damage to the surface of the structure when later removed. Therefore, the self-supporting constraint is introduced into the structural topology optimization design stage, so that the designed structure can be manufactured without adding a support, the practicability of a design result can be effectively improved, and the method has very important engineering application value.
The document "Zhang K, chemical g.three-dimensional high resolution timing dimensioning constraints [ J ] adaptive Manufacturing engineering, 2020,35 101224" discloses a method for the topologically optimised design of three-dimensional self-supporting structures. The method proposed by the literature is based on a density method, firstly adopts an 18-element strategy, and estimates the gradient direction of a density field according to local density distribution around elements in a finite element model, thereby calculating the suspension angle and constructing suspension angle constraint. And secondly, introducing square constraint in the horizontal direction to enable the density of each unit to be larger than the average value of the densities of the units in the four support sets in the horizontal direction, thereby eliminating a suspended area in the structure. By combining the two constraints, the topological optimization design of the three-dimensional self-supporting structure is realized.
Although the method proposed by the literature can obtain a self-supporting structure, the 18-unit strategy adopted by the method obtains the gradient direction of the density field through linear interpolation, and the calculation mode is complex. In addition, the constraints proposed by the method are based on the regular grids and the regular shape design domain, and when the unit shapes and the arrangement modes are irregular or any forming direction is considered, certain limitations exist, so that the method is difficult to apply to engineering practice.
Disclosure of Invention
The invention solves the technical problems that: in order to overcome the defect that the existing topological optimization design method of the three-dimensional self-supporting structure is poor in practicability, the invention provides a topological optimization design method of the three-dimensional self-supporting structure based on a B spline density method. According to the method, three relevant constraints are constructed on the basis of a B-spline parameterized density field so as to realize the optimal design of a self-supporting structure. Firstly, obtaining the gradient of a structure density field by derivation of a B spline function, identifying a boundary region of the structure according to a gradient mode and the curvature radius of a space curve, and controlling the surface inclination angle of the structure in the boundary region to be larger than a specified critical angle of equipment. Secondly, according to different forming directions, a cuboid region containing a structural domain is constructed, a certain number of uniformly distributed detection points are arranged in the region, and the relationship between density values of the detection points is controlled to eliminate the reverse-tapered-like region. And finally, eliminating the special V-shaped section characteristics at the boundary of the design domain by restricting the gradient direction of the density field at the boundary of the design domain.
The technical scheme of the invention is as follows: a three-dimensional self-supporting structure topological optimization design method based on a B spline density method comprises the following steps:
step 1: structuring the structural density field: building the structural design Domain omega of the white support Structure d Defining a level set function phi representing the region d And constructing a density field rho representing the structural design domain d (ii) a Designing Domain Ω according to Structure d The shape of (2), the structural design domain omega d A rectangular parallelepiped region Ω included therein; constructing a three-dimensional B-spline function field inside a cuboid region omega as a B-spline density field rho of the region; and (4) performing Heaviside projection on the B spline density field rho to obtain a projected B spline density field
Figure BDA0003099683530000021
Figure BDA0003099683530000022
Wherein β is the Heaviside projectionη is the projection limit of the Heaviside projection; projecting the B-spline density field
Figure BDA0003099683530000023
And a density field ρ representing a structural design domain d Performing Boolean intersection operation to obtain the final density field of the structure
Figure BDA0003099683530000024
Step 2: identifying the boundary region of the structure:
Figure BDA0003099683530000025
and step 3: constructing inclination angle constraint: for the boundary region omega obtained in step 2 b Arranging a plurality of integration points therein and calculating the gradient of the B-spline density field rho at each integration point
Figure BDA0003099683530000031
And further calculating cosine values cos alpha of the boundary inclination angles alpha at the integration points:
Figure BDA0003099683530000032
wherein b is a unit vector with a direction pointing in the direction of additive manufacturing molding,
Figure BDA0003099683530000033
a gradient mode representing the B-spline density field; according to the inclination angle alpha and the critical angle alpha specified by the equipment 0 Difference of cosine values of (a) in a boundary region omega of the structure b And (3) internally integrating to obtain an inclination angle constraint value q:
Figure BDA0003099683530000034
where L (δ) is a piecewise function with respect to a variable δ, L (δ) =0 when δ < 0; when the value of delta is greater than 0,L(δ)=δ 2 (ii) a And establishing an inclination angle constraint function by using the inclination angle constraint value q:
Figure BDA0003099683530000035
wherein epsilon q Is an extremely small number introduced for relaxing the tilt angle constraint, and the tilt angle constraint is applied to ensure that the tilt angle of any point at the structure boundary is larger than the specified critical angle of the equipment;
and 4, step 4: the elimination of the reverse taper-like region in the optimization result is realized, and the method comprises the following substeps:
step 4.1: constructing a new rectangular parallelepiped region Ω including the rectangular parallelepiped region Ω according to the molding direction of additive manufacturing t :Ω t One side of the rectangular area is parallel to the additive manufacturing forming direction, and the other two sides are not limited and can contain the rectangular area omega;
and 4.2: in a rectangular region omega t A plurality of detection points are uniformly arranged along the directions of the three edges, and the detection points are positioned in a structural design domain omega d The detection point at one side of the bottom edge towards the additive manufacturing and forming direction is an effective detection point; final density field according to structure
Figure BDA0003099683530000036
Calculating the density value of the effective detection point, wherein the density value is positioned in the structural design field omega d The density value of the outer effective detection point is 0 to obtain the density value vector of the effective detection point
Figure BDA0003099683530000037
Step 4.3: in the effective detection points, n is remained after excluding the lowest detection point in the additive manufacturing molding direction t The detection points are detection points needing to participate in calculation, and for the ith detection point needing to participate in calculation, the density value of the point is constrained
Figure BDA0003099683530000041
Should be less than n in the region of the pyramid below it c The maximum of the density values at the points is formulated as:
Figure BDA0003099683530000042
wherein n is c The point refers to n in the layer below the ith detection point needing to participate in calculation c The points comprise a plurality of points in a square area taking a point right below the ith detection point needing to participate in calculation as a central point, and the n points are formed together c The point of the light source is a point,
Figure BDA0003099683530000043
respectively representing the density values of nc points in a pyramid region below the ith detection point, the first item i in the subscript representing the corresponding serial number of the detection point at the top of the pyramid region, and the second items 1-n c Respectively representing n inside the pyramid region c And (3) in order to facilitate optimization by using a gradient algorithm, approximating a max function in the above formula by using a KS function, and calculating an integral constraint value:
Figure BDA0003099683530000044
where w is a parameter in the KS function,. Epsilon 1 Is a very small number introduced to balance the approximation error of the KS function, and h (δ) is a function of the variable δ in the form:
Figure BDA0003099683530000045
wherein the magnitude of the parameter mu determines the severity of the change of the function at delta =0,
step 4.4: with this constraint value g, an overall constraint function can be established:
Figure BDA0003099683530000046
wherein epsilon 2 Is a very small number introduced to relax the tilt constraint; by applying the constraint, the elimination of the reverse-tapered-like region in the optimization result is realized;
and 5: for the domain located in the structural design Ω d Is of d A point with an upper coordinate of (x, y, z), which is perpendicular to the structure boundary and points to the interior of the structure, can be represented as
Figure BDA0003099683530000047
Let the plane perpendicular to the additive manufacturing forming direction and passing through the point (x, y, z) be denoted as m 3 Then the level set function phi d Gradient of (2)
Figure BDA0003099683530000051
In plane m 3 The projection vector d on can be expressed as:
Figure BDA0003099683530000052
and ensure that:
Figure BDA0003099683530000053
according to the projection vector d of a plurality of integral points on the boundary of the structural design domain and the gradient of the B-spline density field
Figure BDA0003099683530000054
At structural design domain boundary Γ d And integrating to obtain an integral constraint value:
Figure BDA0003099683530000055
wherein the L (δ) function is the same as in step 3; using the constraint value, an overall constraint function can be established:
Figure BDA0003099683530000056
by applying the constraint, the elimination of the special V-shaped section characteristics at the boundary of the structural design domain in the optimization result is realized;
and 6: in the structural design domain omega d Dispersing the materials into finite element units, and defining load and boundary conditions simultaneously;
and 7: the topology optimization problem is defined as:
Figure BDA0003099683530000057
Figure BDA0003099683530000058
Figure BDA0003099683530000059
where P denotes the value of the control point of the B-spline function field constructed in the rectangular region omega, n x 、n y 、n z Respectively representing the number of control points in three directions of a cuboid region omega; p is i The middle subscript i represents the serial number of the control point; c represents the degree of structural compliance;
Figure BDA0003099683530000061
respectively representing the final density fields of three different structures, and respectively representing the total rigidity matrix, the total load vector and the displacement vector of the structure by K, F and U; v 0 Denotes the total volume of the structure, V d And
Figure BDA0003099683530000062
respectively representing projection limits of eta d Time structure final density field
Figure BDA0003099683530000063
Current volume fraction and volume fraction upper limit;
and 8: and (6) solving the topological optimization problem in the step (6) by adopting an optimization algorithm to obtain an optimal result.
The further technical scheme of the invention is as follows: the three density fields in step 7 are obtained by selecting three different projection limits η when performing the Heaviside projection in step 1 e 、η i 、η d And obtaining the product, wherein the values of the product are between 0 and 1.
Effects of the invention
The invention has the technical effects that: compared with the design method in the background art, the density field gradient is directly obtained through derivation calculation, so that the calculation of the inclination angle of the structure boundary is more convenient and accurate. According to the method, a B-spline function is used for constructing a structure density field, the gradient of the density field is obtained through derivation, a structure boundary area is further identified, and a boundary inclination angle is obtained in the boundary area according to the gradient direction of the density field, so that the size of a suspension angle is controlled. Meanwhile, the elimination of the reverse taper-like region is realized by arranging uniform detection points in the structural domain and controlling the relation between density values at the detection points. Finally, by constraining the direction of the density field gradient at the design domain boundary, the special V-shaped cross-sectional features appearing at the design domain boundary are eliminated. Compared with the design method of the background art, the gradient of the density field is directly obtained through derivation calculation, so that the calculation of the inclination angle of the structure boundary is more convenient and accurate. In addition, the suspension angle constraints introduced by the invention are irrelevant to the finite element grids, so that the finite element analysis can be carried out by adopting units with irregular shapes aiming at the design domain with complicated shapes in the engineering, the optimal design of the self-supporting structure in any forming direction is realized, and the invention has stronger engineering practicability. Without considering self-support, the structural compliance obtained with the same initial structural optimization was 43.4188, thus achieving structural self-support at the expense of 12.28% compliance.
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FIG. 1 is a diagram illustrating the geometry and boundary conditions of a model according to an embodiment of the present invention.
FIG. 2 is a diagram illustrating distribution of detection points within a domain according to an embodiment of the present invention.
FIG. 3 is a schematic diagram of the detection points and the pyramid area below the detection points in an embodiment of the present invention.
FIG. 4 is a diagram of the design results of an embodiment of the present invention.
Detailed Description
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations or positional relationships based on those shown in the drawings, merely for convenience of description and simplification of the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.
Referring to fig. 1-4, the technical solution adopted by the present invention to solve the technical problem is as follows: a three-dimensional self-supporting structure topological optimization design method based on a B spline density method is characterized by comprising the following steps:
step 1: a structural density field is constructed. Building a structural design Domain omega of a self-supporting Structure d Writing a level set function phi representing the region d And constructing a density field rho representing the structural design domain d . Design of Domain Ω according to Structure d Is configured to design the structure into a domain omega d A rectangular parallelepiped region Ω included therein. And constructing a three-dimensional B-spline function field inside the cuboid region omega as a B-spline density field rho of the region. Subjecting the B-spline density field rho to Heaviside projection to obtain a projected B-spline density field
Figure BDA0003099683530000071
Figure BDA0003099683530000072
Where β is the parameter of the Heaviside projection and η is the projection limit of the Heaviside projection. The B-spline density field after projection
Figure BDA0003099683530000073
And a density field ρ representing a structural design domain d Performing Boolean intersection operation to obtain the final density field of the structure
Figure BDA0003099683530000074
Step 2: a boundary region of the structure is identified. For a point with coordinates (x, y, z) in the structural design domain, its final density field
Figure BDA0003099683530000075
Gradient of (2)
Figure BDA0003099683530000076
And gradient mode
Figure BDA0003099683530000077
Can be obtained by derivation of B-spline functions:
Figure BDA0003099683530000078
Figure BDA0003099683530000079
wherein x, y, z are the coordinates in a cartesian coordinate system, respectively. A lower limit of a gradient mode is preset
Figure BDA00030996835300000710
When the gradient norm at point (x, y, z) is greater than the lower limit, it is temporarily identified as a boundary. Structural boundaries omega identified from gradient modes b Can be expressed as:
Figure BDA0003099683530000081
in order to eliminate the small corner region pair above the hole in the structure or at the intersection of two rodsThe influence of the tilt angle constraint to be applied requires the above-mentioned structural boundary Ω b The region with the smaller inner radius of curvature is excluded. Also for a point with coordinates (x, y, z) in the design domain of the structure, the iso-surface m1 of the final density field of the structure at that point and the gradient at that point are calculated
Figure BDA0003099683530000082
Plane m formed by additive manufacturing and forming direction 2 M can be obtained by a curvature radius calculation formula of the space curve 1 And m 2 The radius of curvature r (x, y, z) at the point (x, y, z). A lower limit r of the radius of curvature is specified min Then the boundary region omega after the small fillet is removed b Can be re-expressed as:
Figure BDA0003099683530000083
and step 3: and constructing an inclination angle constraint. For the boundary region omega obtained in step 2 b Arranging a plurality of integration points therein and calculating gradients of the B-spline density field rho at each integration point
Figure BDA0003099683530000084
And further calculating cosine values cos alpha of the boundary inclination angles alpha at the integration points:
Figure BDA0003099683530000085
wherein b is a unit vector with a direction pointing in the direction of additive manufacturing molding,
Figure BDA0003099683530000086
the gradient mode of the B-spline density field is represented. According to the inclination angle alpha and the critical angle alpha specified by the equipment 0 Difference of cosine values of (a) in a boundary region omega of the structure b And (3) internally integrating to obtain an inclination angle constraint value q:
Figure BDA0003099683530000087
where L (δ) is a piecewise function with respect to a variable δ, L (δ) =0 when δ < 0; when δ > 0, L (δ) = δ 2 . And establishing an inclination angle constraint function by using the inclination angle constraint value q:
Figure BDA0003099683530000088
wherein epsilon q Is a very small number introduced to relax the tilt constraint. By applying the tilt angle constraint, the tilt angle of any point at the structure boundary is made larger than the critical angle specified by the device.
And 4, step 4: constructing a new rectangular parallelepiped region Ω including the rectangular parallelepiped region Ω according to the molding direction of additive manufacturing t ,Ω t One side of the rectangular area is parallel to the additive manufacturing and forming direction, and the other two sides are not limited and can contain the rectangular area omega. In a rectangular region omega t A plurality of detection points are uniformly arranged along the directions of three edges and positioned in a structural design domain omega d The detection point at one side of the bottom edge towards the additive manufacturing and forming direction is an effective detection point. Final density field according to structure
Figure BDA0003099683530000091
Calculating the density value of the effective detection point, wherein the density value is positioned in the structural design domain omega d The density value of the outer effective detection point is 0 to obtain the density value vector of the effective detection point
Figure BDA0003099683530000092
In the effective detection points, n is remained after excluding the lowest detection point in the additive manufacturing molding direction t The detection points are detection points which need to participate in calculation.
For the ith detection point needing to participate in calculation, the density value at the point is constrained
Figure BDA0003099683530000093
Should be smaller than the pyramid area below itN within a domain c The maximum of the density values at the points is formulated as:
Figure BDA0003099683530000094
the lower region here means a lower region defined in the additive manufacturing forming direction. n is a radical of an alkyl radical c The point refers to n in the layer below the ith detection point needing to participate in calculation c The points comprise a plurality of points in a square area taking a point right below the ith detection point needing to participate in calculation as a central point, and the n points are formed together c And (4) points.
Figure BDA0003099683530000095
Respectively represents n in a pyramid region below the ith detection point c Density value of points, the first item i in subscript represents the corresponding serial number of the detection point at the top of pyramid region, and the second items 1-n c Respectively representing n inside the pyramid region c And detecting points. To facilitate optimization using the gradient algorithm, the KS function is used to approximate the max function in the above equation and the overall constraint value is calculated:
Figure BDA0003099683530000096
where w is a parameter in the KS function,. Epsilon 1 Is a very small number introduced to balance the KS function approximation error, and h (δ) is a function of the variable δ, of the form:
Figure BDA0003099683530000097
wherein the magnitude of the parameter μ determines the severity of the change of the function at δ =0. With this constraint value g, an overall constraint function can be established:
Figure BDA0003099683530000101
wherein epsilon 2 Is a very small number introduced to relax the tilt constraint. By applying this constraint, elimination of the reverse-tapered-like region in the optimization result is achieved.
And 5: for a domain located in the structural design domain Ω d Is of d A point with an upper coordinate (x, y, z), which is perpendicular to the structure boundary and points in the direction of the structure interior, can be represented as
Figure BDA0003099683530000102
I.e. the level set function phi representing the structural design domain d Of the gradient of (c). Let the plane perpendicular to the additive manufacturing forming direction and passing through the point (x, y, z) be denoted as m 3 Then the level set function phi d Gradient of (2)
Figure BDA0003099683530000103
In plane m 3 The projection vector d on can be expressed as:
Figure BDA0003099683530000104
in order to avoid the appearance of special V-shaped section characteristics at the boundary of the structural design domain, the gradient of the B-spline density field rho at the boundary of the design domain needs to be ensured
Figure BDA0003099683530000105
The dot product with the projection vector d is equal to or greater than 0, that is:
Figure BDA0003099683530000106
according to the projection vector d of a plurality of integral points on the boundary of the structural design domain and the gradient of the B-spline density field
Figure BDA0003099683530000107
At structural design domain boundary Γ d And integrating to obtain an integral constraint value:
Figure BDA0003099683530000108
where the L (δ) function is the same as in step 3. Using the constraint values, an overall constraint function can be established:
Figure BDA0003099683530000109
by applying the constraint, elimination of special V-shaped section characteristics at the boundary of the structural design domain in the optimization result is realized.
Step 6: in the structural design domain omega d Discretized into finite element elements, defining load and boundary conditions.
And 7: the topology optimization problem is defined as:
Figure BDA00030996835300001010
Figure BDA0003099683530000111
Figure BDA0003099683530000112
where P denotes the value of the control point of the B-spline function field constructed in the rectangular region omega, n x 、n y 、n z The number of control points in three directions of the rectangular region Ω is respectively indicated. P i The middle subscript i indicates the number of the control points, and all control points have values between 0 and 1. C represents the degree of structural compliance.
Figure BDA0003099683530000113
Three different structural final density fields are respectively represented, which are obtained by selecting three different projection limits eta when performing the Heaviside projection in step 1 e 、η i 、η d So as to obtain the compound with the characteristics of,the values are all between 0 and 1. K. F and U represent the overall stiffness matrix, the overall load vector and the displacement vector of the structure, respectively. V 0 Denotes the total volume of the structure, V d And
Figure BDA0003099683530000114
respectively representing projection limits of eta d Time structure final density field
Figure BDA0003099683530000115
And a current volume fraction of (d) and a volume fraction upper limit.
And 8: and (6) solving the topological optimization problem in the step (6) by adopting an optimization algorithm to obtain an optimal result.
Reference is made to fig. 1-4. The invention is illustrated by taking a three-dimensional simple beam structure under fixed load as an example. Due to the symmetry of the simply supported beam, only the right half part of the simply supported beam is taken for optimal design. Its Young's modulus is 1 and Poisson's ratio is 0.3. The molding direction defining the structure is represented by a vector b = (0, 1), and the critical molding angle of the printing apparatus is α 0 =45 °. The material distribution in the simply supported beam is selected and designed to enable the flexibility of the simply supported beam to be minimum, and the volume fraction of the total material consumption is maximum 20%. The method comprises the following specific steps:
1. a structural density field is constructed. First, write out the structural design domain Ω d Level set function of (phi) d Density field rho of structural design domain d . Constructing the rectangular region Ω will design the region Ω d And (4) carrying out interpolation by adopting the B spline basis function of the uniform node for 3 times to obtain a B spline density field rho in the cuboid region omega. Performing Heaviside projection on the B-spline density field, wherein the projection parameter beta is 1, the projection limit eta is 0.5, and obtaining the projected B-spline density field
Figure BDA0003099683530000121
Projecting the B-spline density field
Figure BDA0003099683530000122
And the design domain density field ρ d Performing Boolean intersection operation to obtain the final density field of the structure
Figure BDA0003099683530000123
2. Structural boundaries are identified. The lower limit of the gradient mode predefined in this example is
Figure BDA0003099683530000124
Lower limit of curvature radius r min =2, thus the boundary region Ω b Is shown as
Figure BDA0003099683530000125
3. And constructing an inclination angle constraint. In the boundary region omega b Selecting integral points, calculating the gradient at the integral points by derivation and further calculating the cosine value of the inclination angle, wherein the calculation formula is
Figure BDA0003099683530000126
Based on the difference between the tilt angle cosine and the cosine of the equipment-specified critical angle, the method is performed in a region omega b And (3) internally integrating to construct a dip angle constraint function:
Figure BDA0003099683530000127
the allowable region Ω in this embodiment b The angle of inclination of the inner part is subject to a tolerance of 0.5 deg., so that q Is calculated as
Figure BDA0003099683530000128
4. Constructing a new rectangular region omega including the rectangular region omega according to the molding direction of additive manufacturing t . The new cuboid region omega in this example t The same as the rectangular parallelepiped region Ω. In a rectangular region omega t A plurality of detection points are uniformly arranged along the directions of the three edges,the total number of detection points in this example is 60 × 24 × 60, and all the detection points are valid detection points. Final density field according to structure
Figure BDA0003099683530000129
Calculating to obtain the density values at the effective detection points
Figure BDA00030996835300001210
Wherein is located in the structural design domain Ω d The density value of the outer effective detection point is 0. The number of detection points which are left to participate in calculation after the lowest detection point in the effective detection points is removed is 60 multiplied by 24 multiplied by 59. The overall constraints are:
Figure BDA00030996835300001211
in the formula n t =84960,w=20,n c =25,ε 1 =0.15,ε 2 =5×10 -6 . The value of the parameter μ in the h (δ) function is μ =40.
5. At structural design domain boundary Γ d And selecting an integral point and calculating a projection vector d of the integral point. According to the projection vector d of a plurality of integral points on the boundary of the structural design domain and the gradient of the B-spline density field
Figure BDA0003099683530000131
At structural design domain boundary Γ d And integrating, constructing an integral constraint:
Figure BDA0003099683530000132
6. design domain omega of structure by adopting patch grids d Discretizing and defining relevant boundary conditions.
7. Defining a topology optimization problem:
Figure BDA0003099683530000133
Figure BDA0003099683530000134
Figure BDA0003099683530000135
where P represents the value of all control points, with an initial value of 0.5 and upper and lower limits of 1 and 0, respectively. n is x =30,n y =12,n z =30. Three different structural final density fields
Figure BDA0003099683530000136
By selecting the projection limit η at the Heaviside projection, respectively e =0.7、η i =0.5、η d And = 0.3. The projection parameter β of the Heaviside projection takes 1 at 100 steps before optimization and then multiplies by a factor of 1.7 every 100 steps until it reaches its maximum value 25.
8. Finite element analysis and optimization solution. And carrying out finite element analysis on the established model, and respectively carrying out sensitivity analysis on the target function and the constraint function. And (4) selecting a global convergence moving asymptote optimization algorithm (GCMMA) to carry out optimization design to obtain an optimization result.
The method obtains an optimized design result after iteration of the step 450 of the embodiment. The volume fraction of the initial structure is 20%, the flexibility is 842.0703, and the volume fraction of the structure in the optimized result is 20%, the flexibility is 48.7511, and the flexibility is reduced by 94.21%. Without considering self-support, the structural compliance achieved with the same initial structural optimization was 43.4188, thus achieving a structural self-support sacrifice of 12.28% compliance. Compared with the design method in the background art, the density field gradient is directly obtained through derivation calculation, so that the calculation of the inclination angle of the structure boundary is more convenient and accurate. In addition, the suspension angle constraints introduced by the invention are irrelevant to the finite element grids, so that the finite element analysis can be carried out by adopting units with irregular shapes aiming at the design domain with complicated shapes in the engineering, the optimal design of the self-supporting structure in any forming direction is realized, and the invention has stronger engineering practicability.

Claims (2)

1. A three-dimensional self-supporting structure topological optimization design method based on a B spline density method is characterized by comprising the following steps:
step 1: structuring the structural density field: building a structural design domain omega of a self-supporting structure d Defining a level set function phi representing the region d And constructing a density field rho representing the structural design domain d (ii) a Designing Domain Ω according to Structure d The structural design domain omega is constructed d A rectangular parallelepiped region Ω included therein; constructing a three-dimensional B-spline function field inside a cuboid region omega as a B-spline density field rho of the region; subjecting the B-spline density field rho to Heaviside projection to obtain a projected B-spline density field
Figure FDA0003099683520000011
Figure FDA0003099683520000012
Wherein β is a parameter of the Heaviside projection and η is a projection limit of the Heaviside projection; projecting the B-spline density field
Figure FDA0003099683520000013
And a density field ρ representing a structural design domain d Performing Boolean intersection operation to obtain the final density field of the structure
Figure FDA0003099683520000014
Step 2: identifying the boundary region of the structure:
Figure FDA0003099683520000015
and 3, step 3: constructing inclination angle constraint: for the edge obtained in step 2Boundary region omega b Arranging a plurality of integration points therein and calculating the gradient of the B-spline density field rho at each integration point
Figure FDA0003099683520000016
And further calculating cosine values cos alpha of the boundary inclination angles alpha at the integration points:
Figure FDA0003099683520000017
wherein b is a unit vector with a direction pointing in the direction of additive manufacturing molding,
Figure FDA0003099683520000018
a gradient mode representing the B-spline density field; according to the inclination angle alpha and the specified critical angle alpha of the equipment 0 The difference between cosine values of (a) in a boundary region omega of the structure b And (3) internally integrating to obtain an inclination angle constraint value q:
Figure FDA0003099683520000019
where L (δ) is a piecewise function with respect to a variable δ, when δ < 0, L (δ) =0; when δ > 0, L (δ) = δ 2 (ii) a And establishing an inclination angle constraint function by using the inclination angle constraint value q:
Figure FDA0003099683520000021
wherein epsilon q The minimum number is introduced for relaxing the inclination angle constraint, and the inclination angle constraint is applied to ensure that the inclination angle of any point at the structure boundary is larger than the specified critical angle of the equipment;
and 4, step 4: the elimination of the reverse taper-like region in the optimization result is realized, and the method comprises the following substeps:
step 4.1: constructing a new rectangular region including a rectangular region omega according to a molding direction of additive manufacturingBody region omega t :Ω t One side of the rectangular area is parallel to the additive manufacturing forming direction, and the other two sides are not limited and can contain the rectangular area omega;
step 4.2: in a rectangular region omega t A plurality of detection points are uniformly arranged along the directions of the three edges, and the detection points are positioned in a structural design domain omega d The detection points on one side of the bottom edge towards the additive manufacturing forming direction are effective detection points; final density field according to structure
Figure FDA0003099683520000022
Calculating the density value of the effective detection point, wherein the density value is positioned in the structural design domain omega d The density value of the outer effective detection point is 0 to obtain the density value vector of the effective detection point
Figure FDA0003099683520000023
Step 4.3: in the effective detection points, n is remained after excluding the lowest detection point in the additive manufacturing molding direction t The detection points are detection points needing to participate in calculation, and for the ith detection point needing to participate in calculation, the density value of the point is constrained
Figure FDA0003099683520000024
Should be less than n in the region of the pyramid below it c The maximum of the density values at the points is formulated as:
Figure FDA0003099683520000025
wherein n is c The point refers to n in the next layer of the ith detection point needing to participate in calculation c The points comprise a plurality of points in a square area taking the point right below the ith detection point needing to participate in calculation as a central point, and the n points are formed together c The point of the light beam is the point,
Figure FDA0003099683520000026
respectively representN in pyramid area below ith detection point c Density value of points, the first item i in subscript represents the corresponding serial number of the detection point at the top of pyramid region, and the second items 1-n c Respectively representing n inside the pyramid region c And (3) in order to facilitate optimization by using a gradient algorithm, approximating a max function in the above formula by using a KS function, and calculating an integral constraint value:
Figure FDA0003099683520000031
where w is a parameter in the KS function,. Epsilon 1 Is a very small number introduced to balance the KS function approximation error, and h (δ) is a function of the variable δ, of the form:
Figure FDA0003099683520000032
wherein the magnitude of the parameter mu determines the severity of the change of the function at delta =0,
step 4.4: with this constraint value g, an overall constraint function can be established:
Figure FDA0003099683520000033
wherein epsilon 2 Is a very small number introduced to relax the tilt constraint; by applying the constraint, the elimination of the reverse-tapered-like region in the optimization result is realized;
and 5: for the domain located in the structural design Ω d Is of d A point with an upper coordinate (x, y, z), which is perpendicular to the structure boundary and points in the direction of the structure interior, can be represented as
Figure FDA0003099683520000034
Let the plane perpendicular to the additive manufacturing forming direction and passing through the point (x, y, z) be denoted as m 3 The gradient of the level set function phid
Figure FDA0003099683520000035
In plane m 3 The projection vector d on can be expressed as:
Figure FDA0003099683520000036
and ensure that:
Figure FDA0003099683520000037
according to the projection vector d of a plurality of integral points on the boundary of the structural design domain and the gradient of the B-spline density field
Figure FDA0003099683520000038
At structural design domain boundary Γ d And integrating to obtain an integral constraint value:
Figure FDA0003099683520000039
wherein the L (δ) function is the same as in step 3; using the constraint values, an overall constraint function can be established:
Figure FDA00030996835200000310
by applying the constraint, the elimination of the special V-shaped section characteristics at the boundary of the structural design domain in the optimization result is realized;
and 6: dispersing the structure design domain omega d into finite element units, and defining load and boundary conditions at the same time;
and 7: the topology optimization problem is defined as:
Figure FDA0003099683520000041
Figure FDA0003099683520000042
Figure FDA0003099683520000043
where P denotes the value of the control point of the B-spline function field constructed in the rectangular region omega, n x 、n y 、n z Respectively representing the number of control points in three directions of a cuboid region omega; p i The middle subscript i represents the serial number of the control point; c represents the degree of structural compliance;
Figure FDA0003099683520000044
respectively representing the final density fields of three different structures, and respectively representing the total rigidity matrix, the total load vector and the displacement vector of the structure by K, F and U; v 0 Denotes the total volume of the structure, V d And
Figure FDA0003099683520000045
respectively representing projection limits of eta d Time structure final density field
Figure FDA0003099683520000046
Current volume fraction and volume fraction upper limit;
and 8: and (6) solving the topological optimization problem in the step (6) by adopting an optimization algorithm to obtain an optimal result.
2. The method for topologically optimally designing a three-dimensional self-supporting structure based on the B-spline density method as claimed in claim 1, wherein the three density fields in the step 7 are obtained by selecting three different projection limits η when performing the Heaviside projection in the step 1 e 、η i 、η d And obtaining the product, wherein the values of the product are between 0 and 1.
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