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仿竹设计在无人机起落架结构中的应用

赵知辛 郭强 黄鸣远 刘家良

赵知辛,郭强,黄鸣远, 等. 仿竹设计在无人机起落架结构中的应用[J]. 机械科学与技术,2021,40(11):1798-1804 doi: 10.13433/j.cnki.1003-8728.20200565
引用本文: 赵知辛,郭强,黄鸣远, 等. 仿竹设计在无人机起落架结构中的应用[J]. 机械科学与技术,2021,40(11):1798-1804 doi: 10.13433/j.cnki.1003-8728.20200565
ZHAO Zhixin, GUO Qiang, HUANG Mingyuan, LIU Jialiang. Application of Imitation Bamboo Design in Unmanned Aerial Vehicle Landing Gear Structures[J]. Mechanical Science and Technology for Aerospace Engineering, 2021, 40(11): 1798-1804. doi: 10.13433/j.cnki.1003-8728.20200565
Citation: ZHAO Zhixin, GUO Qiang, HUANG Mingyuan, LIU Jialiang. Application of Imitation Bamboo Design in Unmanned Aerial Vehicle Landing Gear Structures[J]. Mechanical Science and Technology for Aerospace Engineering, 2021, 40(11): 1798-1804. doi: 10.13433/j.cnki.1003-8728.20200565

仿竹设计在无人机起落架结构中的应用

doi: 10.13433/j.cnki.1003-8728.20200565
基金项目: 陕西省科技厅重点研发计划项目(2019GY-068)与陕西省教育厅专项科研计划项目(16JK1147)
详细信息
    作者简介:

    赵知辛(1973−),讲师,博士,研究方向为有限元分析,49989803@qq.com

  • 中图分类号: V226+.1

Application of Imitation Bamboo Design in Unmanned Aerial Vehicle Landing Gear Structures

  • 摘要: 应用于无人机的滑撬式起落架多使用弓形梁结构,几何特征上梁是一种细长弹性体,与竹子结构(具有较大细长比)相似。为了提高滑撬式起落架的结构性能,首先参考竹子的微观结构,设计了三种类维管束的仿生圆管,采用有限元法对仿生管轴向与径向碰撞吸能进行了仿真与计算;其次通过有限元静力学与动力学分析,对比了原结构与仿竹结构在相同载荷下的力学性能。仿真结果表明:静力学分析中,仿竹结构的最大应力相较于原结构降低约44%,并改善了弓形梁与滑筒连接处应力集中现象;动力学分析通过多工况模拟了起落架可能出现的平稳着陆与非平稳着陆,采用仿竹结构多工况的最大应力平均降低约22%,有效地提升了着陆性能。
  • 图  1  竹子微观截面

    图  2  仿生截面

    图  3  轴向冲击特性曲线

    图  4  径向冲击特性曲线

    图  5  冲击特性曲线

    图  6  起落架结构图

    图  7  设计结构

    图  8  有限元静力学分析云图

    图  9  动力学分析结果对比图

    图  10  竹节结构

    表  1  材料属性

    材料 泊松比 密度/
    (g·cm−3)
    弹性
    模量/GPa
    屈服
    极限/MPa
    6063铝 0.33 2.7 68 170
    20CrMo钢 0.3 7.85 205 685
    下载: 导出CSV
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出版历程
  • 收稿日期:  2020-12-27
  • 刊出日期:  2021-11-05

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