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兵工学报 ›› 2024, Vol. 45 ›› Issue (5): 1497-1513.doi: 10.12382/bgxb.2022.1212

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新型星形负泊松比抗冲击结构设计与入水冲击

金泽华1, 刘清洋1, 马文朝1, 孟军辉1,2,*()   

  1. 1 北京理工大学 宇航学院, 北京 100081
    2 北京理工大学重庆创新中心, 重庆 401135
  • 收稿日期:2022-12-03 上线日期:2023-04-04
  • 通讯作者:
  • 基金资助:
    国家自然科学基金项目(11902029)

Design of Anti-impact Structure with Novel Star-shaped Negative Poisson’s Ratio and Research on Water-entry Impact

JIN Zehua1, LIU Qingyang1, MA Wenchao1, MENG Junhu1,2,*()   

  1. 1 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
    2 Chongqing Innovation Center of Beijing Institute of Technology, Chongqing 401135, China
  • Received:2022-12-03 Online:2023-04-04

摘要:

针对跨介质飞行器入水过程中受到较大冲击载荷的问题,提出一种基于工程需求的负泊松比抗冲击结构拓扑优化设计方法,通过将弹性模量和泊松比引入拓扑优化设计的目标函数,得到满足抗冲击性能需求的负泊松比星形-四边形蜂窝(Star-quadrangular Honeycomb,SQH)结构。在建立SQH结构理论分析模型的基础上,推导冲击载荷下的平台应力解析公式,并通过数值模拟仿真进行校验。通过与星形-圆环蜂窝(Star-circle Honeycomb,SCH)等多种负泊松比结构的比吸能进行对比,得到SQH结构在低速、中速、高速冲击下的比吸能分别高于SCH结构28.74%、45.2%、7.03%。通过流固耦合仿真分析,对所设计的SQH夹层结构进行入水冲击降载研究,进一步讨论SQH夹层结构主要尺寸参数对入水冲击特性的影响。研究结果表明,在尺寸允许范围内,SQH单元倾角和单元壁厚的增大均使得结构产生的加速度峰值减小,动能转化为结构的变形能也减小,验证了用于工程需求的负泊松比结构拓扑优化设计的有效性。

关键词: 跨介质飞行器, 负泊松比, 拓扑优化, 冲击吸能, 平台应力

Abstract:

To solve the problem that the trans-media flight vehicle will be subjected to large impact load in the process of entering water, a topology optimization design method for anti-impact structure with of negative Poisson’s ratio based on engineering requirements is proposed. A star-quadrangular honeycomb (SQH) structure with negative Poisson’s ratio which meets the requirements of impact resistance is obtained by adding the elastic modulus and Poisson’s ratio into the objective function of topology optimization design. Based on the theoretical analysis model of SQH structure, the analytical formula of plateau stress under impact load is deduced and verified by numerical simulation. Compared with the specific energy absorption of star-circle honeycomb (SCH) and other negative Poisson’s ratio structures, the specific energy absorptions of SQH structure under low-speed, medium-speed and high-speed impact are 28.74%, 45.2% and 7.03% higher than that of SCH structure, respectively. Through the fluid-solid coupling simulation analysis, the designed SQH sandwich structure is studied for load reduction by water- entry impact, and the influence of the main size parameters of SQH sandwich structure on the impact characteristics of water entry is further discussed. The results show that, within the allowable range of size, the increase in the inclination angle and wall thickness of SQH unit will reduce the peak acceleration of the structure and the transformation of kinetic energy into the deformation energy of the structure, which verifies the effectiveness of the negative Poisson’s ratio structure topology optimization design for engineering requirements.

Key words: trans-media flight vehicle, negative Poisson’s ratio, topology optimization, energy absorption, plateau stress

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