A novel method to eliminate the bending-induced collapse of hexagonal honeycomb

材料科学 蜂巢 弯曲 曲率 六方晶系 蜂窝结构 复合材料 变形(气象学) 半径 弯曲半径 压缩(物理) 曲率半径 结构工程 几何学 结晶学 平均曲率 数学 计算机科学 工程类 流量平均曲率 计算机安全 化学
作者
Yujun Li,Zhiyong Zhao,Chuang Liu,Qi Liu,Lishuai Sun,Junbiao Wang
出处
期刊:Chinese Journal of Aeronautics [Elsevier]
卷期号:36 (10): 262-274 被引量:6
标识
DOI:10.1016/j.cja.2023.05.005
摘要

A novel grooving method for eliminating the bending-induced collapse of hexagonal honeycombs has been proposed, which lies in determining the appropriate grooving parameters, including the grooving spacing, angle, and depth. To this end, a framework built upon the experiment-based, machine learning approach for grooving parameters prediction was presented. The continuously grooved honeycomb bending experiments with various radii, honeycomb types, and thicknesses were carried out, and then the deformation level of honeycombs at different grooving spacing was quantitatively evaluated. A criterion for determining the grooving spacing was proposed by setting an appropriate tolerance for the out-of-plane compression strength. It was found that as the curvature increases, the grooving spacing increases due to the deformation level of honeycombs being more severe at a smaller bending radius. Besides, the grooving spacing drops as the honeycomb thickness increases, and the cell size has a positive effect on the grooving spacing, while the relative density has a negative effect on the grooving spacing. Furthermore, the data-driven Gaussian Process (GP) was trained from the collected data to predict the grooving spacing efficiently. The grooving angle and depth were calculated using the geometrical relationship of honeycombs before and after bending. Finally, the grooving parameters design and verification of a honeycomb sandwich fairing part were conducted based on the proposed grooving method.

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