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仿生波纹夹层结构耐撞性分析及优化
引用本文:黄晗,许述财,陈姮.仿生波纹夹层结构耐撞性分析及优化[J].爆炸与冲击,2021,41(8):33-43.
作者姓名:黄晗  许述财  陈姮
作者单位:1.南京航空航天大学航天学院,江苏 南京 211106
基金项目:国家自然科学基金(11902157);中国博士后科学基金(2018M641338);南京航空航天大学校人才科研启动基金(1011-YAH20001)
摘    要:为提高薄壁夹层结构耐撞性,以虾螯为仿生原型,设计梯度分布的仿生波纹形夹层结构,包括单层、双层和三层波纹结构。以初始峰值载荷Fp、比吸能Es为耐撞性指标,利用有限元法分析了单元高宽比γ(γ1、γ2和γ3分别为单元第1层、第2层和第3层的高宽比)对波纹夹层结构耐撞性的影响,采用多目标粒子群优化方法得到了夹层结构最优参数。结果表明,单层波纹结构耐撞性随单元高宽比γ的增大逐渐变差,双层波纹结构下层结构单元高宽比γ对耐撞性的影响大于上层结构单元高宽比γ对耐撞性的影响,较小的γ值有利于提高三层波纹结构的比吸能。结构优化结果表明:单层结构最优尺寸γ1为0.8;双层结构最优尺寸为γ1 = 0.5和γ2 = 1.2;三层结构最优组合为γ1 = 0.6,γ2 = 0.6和γ3 = 0.9。上述结果可为薄壁夹层结构轻量化设计提供新思路。

关 键 词:薄壁夹层结构    耐撞性    结构优化    工程仿生    冲击
收稿时间:2020-08-11

Crashworthiness analysis and optimization of bionic corrugated sandwich structures
HUANG Han,XU Shucai,CHEN Heng.Crashworthiness analysis and optimization of bionic corrugated sandwich structures[J].Explosion and Shock Waves,2021,41(8):33-43.
Authors:HUANG Han  XU Shucai  CHEN Heng
Institution:1.Academy of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, Jiangsu, China2.State Key Laboratory of Automotive Safety and Energy, Tsinghua University, Beijing 100084, China3.Field Engineering College, Army Engineering University of PLA, Nanjing 210001, Jiangsu, China
Abstract:To improve the crashworthiness of thin-walled sandwich structures, a series of bionic corrugated sandwich structures with triangular elements (the height-to-width ratios of the elements are defined as γ) were designed inspired by the structures of shrimp chelas, including single-layer, double-layer and three-layer corrugated sandwich structures (γ1, γ2 and γ3 denotes the height-to-width ratios of single-layer, double-layer and three-layer elements, respectively). To analyze the deformation and mechanical response of the bionic thin-walled structures, the finite element method was adopted based on LS-DYNA and HyperMesh. By taking the initial peak load Fp and specific energy absorption Es as crashworthiness indexes, the influences of γ on the crashworthiness of the corrugated sandwich structures were discussed. The crashworthiness of the single-layer sandwich structures becomes worse gradually when the parameters γ exceed a certain value. For the double-layer sandwich structures, the influences of the parameters γ2 in the lower layers on the crashworthiness is greater than that of the parameters γ1 in the upper layers.. The Fp decreases by 37.8% with the increase of γ2, which means the greater γ2 of the lower layer is beneficial to improve the crashworthiness of the structure. For the three-layer sandwich structures, the influence of γ on crashworthiness indexes was investigated by range and variance analysis methods. The results show that the γ3 has the most significant influence on Es, and the significance level reaches 0.1. Finally, the optimal parameters of the bionic corrugated sandwich structures were obtained by using the multi-objective particle swarm optimization method based on a polynomial regression (PR) meta model. The optimal results show that the crashworthiness of the single-layer corrugated sandwich structures improves with the increase of γ. For the double-layer corrugated sandwich structures, The γ of the lower layer affects the crashworthiness more significantly than the γ of the upper layer. The three-layer corrugated sandwich structure with lower γ has higher Es. The optimal dimensions of the single-layer, double-layer and three-layer structures are γ = 0.8; γ1 = 0.5 and γ2 = 1.2; γ1 = 0.6, γ2 = 0.6 and γ3 = 0.9, respectively. The above results are helpful for the design of the thin-walled sandwich structures.
Keywords:
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