Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (4): 232351.doi: 10.7527/S1000-6893.2025.32351
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles Next Articles
Yongli ZHANG1, Zhiqi NIU1(
), Lei YU1, Junhui MENG2, Feng SUN1
Received:2025-06-03
Revised:2025-06-30
Accepted:2025-07-23
Online:2025-08-12
Published:2025-08-11
Contact:
Zhiqi NIU
E-mail:niuzhiqi@126.com
Supported by:CLC Number:
Yongli ZHANG, Zhiqi NIU, Lei YU, Junhui MENG, Feng SUN. Advances and prospects in application of key structural technologies for intelligent ammunition[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(4): 232351.
Table 2
Additive manufacturing process constraints
| 工艺约束 | 概念 | 优化目标 |
|---|---|---|
| 几何尺寸 | 受限于3D打印设备成形精度,几何特征尺寸(如细小孔径、薄壁结构、细杆结构等)约束需要合理控制,而拓扑优化往往会产生不利于制造的细小分支结构 | 最大/最小尺寸 |
| 连通性 | 增材制造成形后依据不同工艺需去除残余的未固化树脂、未熔融粉末、辅助支撑,要求结构内部不能含有封闭空腔 | 结构连通性保障 |
| 自支撑角 | 当结构存在较大悬空角时,需额外增加辅助支撑结构以避免成形过程中材料塌陷,辅助支撑结构降低了材料利用率,并增加了后期工艺困难、时间成本 | 支撑体积最小化 |
| 残余应力与变形 | 金属增材制造过程中反复地快速加热与急速冷却会造成零件内部明显的残余应力累积,导致成形构件大变形或开裂等问题 | 屈服强度匹配 |
Table 3
Materials/structure multi-scale collaborative topology optimization difficulties
| 难点 | 具体问题 |
|---|---|
| 多类微结构协同优化难题 | 高阶衔接性缺失:多类微结构(如金字塔点阵+手性晶格)界面易出现应力集中,因微结构拓扑构型不兼容导致局部应力超限,引发疲劳失效 |
| 数值求解复杂度:多类微结构优化变量数量指数级增长(例如10⁶→10⁹量级),传统SIMP(Solid Isotropic Material with Penalization)算法难以收敛,需开发新型优化框架 | |
| 制造-设计跨尺度失耦 | 晶粒尺度效应未建模:微观晶粒尺寸分布显著影响材料力学性能,但当前优化模型未耦合晶体塑性理论 |
| 多物理场耦合缺陷 | 热-力-电磁场强耦合工况下,多尺度优化目标函数冲突(如隐身要求低密度点阵和承载要求高密度点阵),缺乏统一权衡准则 |
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