中国机械工程 ›› 2026, Vol. 37 ›› Issue (6): 1462-1471.DOI: 10.3969/j.issn.1004-132X.2026.06.019
• 生物制造 • 上一篇
收稿日期:2025-05-30
出版日期:2026-06-25
发布日期:2026-07-17
通讯作者:
冯浩
作者简介:冯浩*(通信作者),男,2000年生,硕士研究生。研究方向为CAD/CAM。E-mail:13665118522@163.com。基金资助:
FENG Hao1(
), JI Xiaogang1,2, NIU Guofa1, XU Xinji1
Received:2025-05-30
Online:2026-06-25
Published:2026-07-17
Contact:
FENG Hao
摘要:
马蹄形微结构具有强拉伸性、高透气性及拓扑可编程性等优异特性,广泛应用于生物医学设备、柔性显示器、组织工程等重要领域。基于BCT2000测试原理与GB/T 24218.5—2016钢球顶破法,构建了针对马蹄形微结构的面外变形测试方法,系统研究了三角形、Kagome形及蜂窝形三种仿生马蹄形微结构的面外变形行为。通过数值模拟和实验分析对三种马蹄形微结构的顶破载荷-位移曲线进行研究,分析了应力分布情况以及结构的面外变形情况,并以三角直线结构作为对照组。从四个方面建立了柔弹性能评价标准,分析了四种因素对柔弹性能的影响。三角形微结构展现出最优异的柔弹性综合性能,相较于传统直线型结构有明显柔弹性优势,最大面外位移增大了88.9%,低载荷承载位移增大了428.1%,面外刚度降低了59.3%,能量吸收量提高了31.5%。
中图分类号:
冯浩, 纪小刚, 牛国法, 徐新纪. 仿生马蹄形微结构的面外变形行为与柔弹性研究[J]. 中国机械工程, 2026, 37(6): 1462-1471.
FENG Hao, JI Xiaogang, NIU Guofa, XU Xinji. Study on Out-of-plane Deformation Behaviors and Flexibility-elasticity of Bionic Horseshoe-shaped Microstructures[J]. China Mechanical Engineering, 2026, 37(6): 1462-1471.
| 晶格类型 | R0/mm | ω/mm | θ0/(°) | ω0 | l/mm | |
|---|---|---|---|---|---|---|
| 三角形 | ![]() | 3.0 | 0.75 | 180 | 0.25 | 12 |
| Kagome形 | ![]() | 1.5 | 0.75 | 180 | 0.50 | 6 |
| 蜂窝形 | ![]() | 1.5 | 1.125 | 180 | 0.75 | 6 |
表1 三种晶格结构尺寸
Tab.1 Three lattice - structure dimensions
| 晶格类型 | R0/mm | ω/mm | θ0/(°) | ω0 | l/mm | |
|---|---|---|---|---|---|---|
| 三角形 | ![]() | 3.0 | 0.75 | 180 | 0.25 | 12 |
| Kagome形 | ![]() | 1.5 | 0.75 | 180 | 0.50 | 6 |
| 蜂窝形 | ![]() | 1.5 | 1.125 | 180 | 0.75 | 6 |
| 工艺参数配置项 | 具体参数 |
|---|---|
| 层厚/mm | 0.02 |
| 曝光时间/s | 6 |
| 关灯时间/s | 1 |
| 底部曝光时间/s | 35 |
| 底部层数 | 4 |
| 抗锯齿等级 | 4 |
| Z轴抬升距离/mm | 5 |
| Z轴抬升速度/(mm∙s | 2 |
| Z轴回退速度/(mm∙s | 2 |
表2 DLP工艺参数选择
Tab.2 Selection of DLP process parameters
| 工艺参数配置项 | 具体参数 |
|---|---|
| 层厚/mm | 0.02 |
| 曝光时间/s | 6 |
| 关灯时间/s | 1 |
| 底部曝光时间/s | 35 |
| 底部层数 | 4 |
| 抗锯齿等级 | 4 |
| Z轴抬升距离/mm | 5 |
| Z轴抬升速度/(mm∙s | 2 |
| Z轴回退速度/(mm∙s | 2 |
| 本构系数 | |||
|---|---|---|---|
| C10 | C01 | D1 | |
| 数值 | 0.317 | 0.076 | 0.254 |
表3 Mooney-Rivlin本构模型相关参数拟合结果
Tab.3 Fitting results of relevant parameters of the Mooney - Rivlin constitutive model
| 本构系数 | |||
|---|---|---|---|
| C10 | C01 | D1 | |
| 数值 | 0.317 | 0.076 | 0.254 |
| 试样 | 最大顶破位移Smax/mm | 最大顶破载荷N0max/N |
|---|---|---|
| 三角直线形 | 19.58 | 5.40 |
| 三角形 | 36.99 | 5.34 |
| Kagome形 | 28.45 | 3.58 |
| 蜂窝形 | 28.45 | 3.46 |
表4 四种结构的面外变形实验数据
Tab.4 Out-of-plane deformation experimental data of four structures
| 试样 | 最大顶破位移Smax/mm | 最大顶破载荷N0max/N |
|---|---|---|
| 三角直线形 | 19.58 | 5.40 |
| 三角形 | 36.99 | 5.34 |
| Kagome形 | 28.45 | 3.58 |
| 蜂窝形 | 28.45 | 3.46 |
结构 类型 | 最大面外 位移/mm | 面外刚度/ (N∙m | 吸收的能量/J | 低载荷承载 位移/mm |
|---|---|---|---|---|
| 三角形 | 36.99 | 172.41 | 0.075 | 8.99 |
| Kagome形 | 28.45 | 175.01 | 0.037 | 7.65 |
| 蜂窝形 | 28.45 | 201.25 | 0.034 | 7.69 |
表5 三种结构的柔弹性能评价指标
Tab.5 Evaluation indicators of the flexible-elastic properties of three structures
结构 类型 | 最大面外 位移/mm | 面外刚度/ (N∙m | 吸收的能量/J | 低载荷承载 位移/mm |
|---|---|---|---|---|
| 三角形 | 36.99 | 172.41 | 0.075 | 8.99 |
| Kagome形 | 28.45 | 175.01 | 0.037 | 7.65 |
| 蜂窝形 | 28.45 | 201.25 | 0.034 | 7.69 |
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