Research progress on optimization design methods for continuous fiber direction and path of composites
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摘要: 连续纤维增强复合材料因其优异的比刚度、比强度等特性,在航空航天、国防军工、医疗器件等高端装备领域得到了广泛的关注和应用。其中,纤维方向对连续纤维增强复合材料的力学性能有着重要影响,但是由于常规制造工艺的局限,纤维路径通常沿0°、45°、90°等规律一致的方向来设定,连续纤维增强复合材料的优势无法被充分利用。如今,3D打印技术促进了制造具有复杂曲线纤维路径复合材料的发展,其对应的纤维方向及路径优化设计方法正逐步引起国内外专家学者的重点关注。本文围绕纤维增强复合材料的纤维方向及路径优化设计方法,介绍了正交各向异性材料方向优化理论,回顾了纤维角度优化方法,总结了现有纤维路径规划算法,探讨了相关前沿问题并做出了未来展望。本文为高性能连续纤维增强复合材料的优化设计和制造提供了重要信息,有助于推动高性能连续纤维增强复合材料的快速发展和广泛应用。Abstract: Continuous fiber reinforced composites have gained wide attention and application in high-end equipment fields such as aerospace, defense, and medical devices, due to their excellent specific stiffness, specific strength, and other properties. The fiber orientation has a significant impact on the mechanical performance of continuous fiber reinforced composites. However, due to the limitations of conventional manufacturing processes, the fiber paths are usually set along regular directions such as 0°, 45°, 90°, etc., which hinders the full utilization of the advantages of continuous fiber reinforced composites. Nowadays, the development of 3D printing technology has facilitated the manufacturing of composites with complex curved fiber paths, and the corresponding optimization methods for fiber orientation and path design have gradually attracted attention from experts and scholars worldwide. In this article, we focus on the optimization methods for fiber orientation and path design of fiber reinforced composites. We introduce the theory of orthogonal anisotropic material direction optimization, review the methods for fiber angle optimization, summarize the existing fiber path planning algorithms, discuss relevant cutting-edge issues, and provide future prospects. This review provides important information for the design optimization and manufacturing of high-performance continuous fiber reinforced composites, which will contribute to the rapid development and wide application of continuous fiber reinforced composites.
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Key words:
- composites /
- 3D printing /
- fiber orientation /
- fiber path /
- optimal design
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图 1 CFRC拓扑设计:(a)四点弯曲梁[40],(b) 具有负泊松比效应的超结构[41],(c) 三维悬臂梁结构[42],(d) 多载荷情况下的三维梁结构[42]
Figure 1. Topological design CFRC: (a) Four-point bending beam[40],(b) Meta-structures with negative Poisson’s ratio[41], (c) Three-dimension cantilever beam[42], (d) Three-dimension beam structure under multiple-loads[42]
图 6 不同子区间数量情况下悬臂梁的优化结果[71]:(a) 1个子集;(b) 2个子集;(c) 3个子集
Figure 6. Optimization results of cantilever beams under different number of subintervals: (a) One subinterval; (b) Two subintervals; (c) Three subintervals
图 15 基于LSF的连续纤维增强复合材料超结构设计:(a)(b) 复合材料超结构中基于LSF得到的连续纤维路径;(c)(d)复合材料超结构的3D打印纤维路径;(e) 复合材料超结构力学性能随调控参数的变化[41]
Figure 15. Design of continuous fiber reinforced meta-composites based on LSF: (a)(b) Continuous fiber path of meta-composite based on LSF; (c)(d) Actually printing path of meta-composite; (e) Variation of mechanical properties of meta-composite versus tailorable parameter[41]
图 19 基于流线方法所设计的连续纤维路径:(a) 复合材料悬臂梁的平均载荷传递方向和连续纤维路径;(b) 复合材料悬臂梁的连续纤维打印路径;(c) 具有负泊松比效应的复合材料超结构;(d) 高弹性模量复合材料格栅结构的连续纤维打印路径[11,116]
Figure 19. Continuous fiber paths designed based on streamline methods: (a) The average load transmission orientation and continuous fiber paths of the cantilever beam; (b) The continuous fiber printing paths of the cantilever beam; (c) The meta-structures with negative Poisson’s ratio; (d) The composite grid structures of enhanced effective elastic modulus and their continuous fiber printing paths [11,116]
图 21 基于应力场的连续纤维打印路径规划算法:(a) 求解主应力矢量场;(b) 基于MST确定的主应力矢量场;(c) 识别主应力矢量紊乱的区域;(d) 移除混乱的主应力矢量;(e) 完整的主应力矢量场;(f) 连续纤维路径;(g) 最终的纤维打印路径[118]
Figure 21. Continuous fiber printing path planning algorithm based on stress field; (a) Solving the principal stress vector field; (b) Principal stress vectors field determined by MST; (c) Identify the region of disturbed principal stress vector; (d) Remove the principal stress vector from the disturbed area; (e) Full principal stress vector field; (f) Continuous fiber path; (g) Final fiber printing path[118]
图 23 含有孔洞的复合材料平板优化设计:(a) 设计域和载荷;(b) 优化得到的纤维方向和纤维含量;(c) 根据材料汇编算法得到的纤维路径;(d) 用于可视化的3D打印样件[120]
Figure 23. Design optimization of a composite plate structure with a hole: (a) Design domain and loads; (b) Optimized fiber direction and fiber content; (c) Fiber path obtained by material compilation; (d) 3D printed sample for visualization[120]
表 1 基于应力方法得到的纤维极值角度
Table 1. Fiber extreme angle obtained from stress based method
Cases Condition Extreme angle 1 $ d > 0 $
and
4$ {d}^{2}\left[{({\sigma }_{1}-{\sigma }_{2})}^{2}+4{\sigma }_{12}^{2}\right] > {c}^{2}{\left({\sigma }_{1}+{\sigma }_{2}\right)}^{2} $$ {\theta }_{1}=\mathrm{a}\mathrm{r}\mathrm{c}\mathrm{t}\mathrm{a}\mathrm{n}\left(\dfrac{2 b{\gamma }_{12}+\sqrt{4{b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+{\gamma }_{12}^{2}\right]-{a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2}}}{2 b\left({\varepsilon }_{1}-{\varepsilon }_{2}\right)-a({\varepsilon }_{1}+{\varepsilon }_{2})}\right) $
$ {\theta }_{1}=\mathrm{a}\mathrm{r}\mathrm{c}\mathrm{t}\mathrm{a}\mathrm{n}\left(\dfrac{2 b{\gamma }_{12}+\sqrt{4{b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+{\gamma }_{12}^{2}\right]-{a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2}}}{2 b\left({\varepsilon }_{1}-{\varepsilon }_{2}\right)-a({\varepsilon }_{1}+{\varepsilon }_{2})}\right) $2 $ d > 0 $
and
4$ {d}^{2}\left[{({\sigma }_{1}-{\sigma }_{2})}^{2}+4{\sigma }_{12}^{2}\right] < {c}^{2}{\left({\sigma }_{1}+{\sigma }_{2}\right)}^{2} $$ {\theta }_{1}={\theta }_{I} $
$ {\theta }_{1}={\theta }_{II} $3 $ d < 0 $ $ {\theta }_{1}={\theta }_{I} $ 表 2 基于应变方法得到的纤维极值角度
Table 2. Fiber extreme angle obtained from strain based method
Cases Condition Extreme angle 1 $ b < 0 $
and
4$ {b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+4{\varepsilon }_{12}^{2}\right] > {a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2} $$ {\theta }_{1}=\mathrm{a}\mathrm{r}\mathrm{c}\mathrm{t}\mathrm{a}\mathrm{n}\left(\dfrac{2 b{\gamma }_{12}+\sqrt{4{b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+{\gamma }_{12}^{2}\right]-{a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2}}}{2 b\left({\varepsilon }_{1}-{\varepsilon }_{2}\right)-a({\varepsilon }_{1}+{\varepsilon }_{2})}\right) $
$ {\theta }_{1}=\mathrm{a}\mathrm{r}\mathrm{c}\mathrm{t}\mathrm{a}\mathrm{n}\left(\dfrac{2 b{\gamma }_{12}-\sqrt{4{b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+{\gamma }_{12}^{2}\right]-{a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2}}}{2 b\left({\varepsilon }_{1}-{\varepsilon }_{2}\right)-a({\varepsilon }_{1}+{\varepsilon }_{2})}\right) $2 $ b < 0 $
and
4$ {b}^{2}\left[{({\varepsilon }_{1}-{\varepsilon }_{2})}^{2}+4{\varepsilon }_{12}^{2}\right] > {a}^{2}{\left({\varepsilon }_{1}+{\varepsilon }_{2}\right)}^{2} $$ {\theta }_{1}={\theta }_{I} $ 表 3 不同情况下的极值角度[55]
Table 3. The extreme angle under different circumstance.
Extreme angle $ {\theta }_{e} $ Relatively “low” shear stiffness $ {\alpha }_{3} > 0 $ Relatively “high” shear stiffness $ {\alpha }_{3} < 0 $ $ \gamma < -1 $ $ -1 < \gamma < 1 $ $ \gamma > 1 $ $ \gamma < -1 $ $ -1 < \gamma < 1 $ $ \gamma > 1 $ $ {0}^\circ $ Global min Global max Global max Global max Local min Globa min $ {90}^\circ $ Global max Local max Global min Global min Global min Global max $ \mathrm{cos}\left(2{\theta }_{e}\right)=-\gamma $ Global min Global max 表 4 DFOO 算法以及一个离散单元所需设计变量个数
Table 4. DFOO algorithms and the number of required design variables for a discrete element.
Method The number of design variables required Discrete material optimization (DMO)[59] $ {n}_{e} $ Shape function with penalization (SFP) [60] $ {n}_{e}/2 $ Bi-value coding parameterization (BCP) [61] $ \left\lceil {{log}_{2}{n}_{e}} \right\rceil $ Bipartite interpolation optimization (BIO) [62] $\left\lceil {{log}_{2}{n}_{e}} \right\rceil $ Normal distribution fiber optimization (NDFO)[63] 1 表 5 若干种处理CFOO问题的方法及其优缺点
Table 5. Several approaches to CFOO and their advantages and disadvantages
Method Advantage Disadvantage Reference Shepard interpolation for fiber angle The continuity of fiber angle is guaranteed The optimization result depends on the
initial design;
Ends at local optimal solution[69] Gradient descent method Superior convergence properties Poor continuity of fiber angles [70] Discrete-continuous
parameterizationThe solution space is complete;
It reduces the risk of local optimalDifficulty in determining the number of subintervals [71] Principal stress orientation interpolated continuous fiber angle Reduce the phenomenon of local fiber
discontinuity;
Higher convergence efficiencyOptimization results depend on the
direction of principal stress[72] Full-scale topology
optimizationThe difficulty of optimization is low;
Can generate continuous fiber pathsHigh computational cost [73] Deep neural network models Reduces the number of optimization iterations and decreases computational costs Post-processing step required;
Problem-dependent[74] 表 6 三类连续纤维路径优化设计方法
Table 6. Three types of continuous fiber path optimization design methods
Method Optimized variables The representation of fiber paths Advantage Disadvantage Based on continuous and differentiable functions Functional
coefficientsFunction trajectory Convenient for adding
manufacturing
constraintsLow design freedom;
Optimization results depend on the selection of fiber representation functionsBased on level set function Level set function
or expansion
coefficientIso-contours of level set function Fiber paths without gaps and overlaps Fiber path may occur sharp corners Based on stress vector fields Stream function Streamline More robust and
StraightforwardPost-processing step required -
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