光固化充气机翼的设计与动力学分析
DOI:
作者:
作者单位:

1.南京航空航天大学;2.中国民航大学

作者简介:

通讯作者:

中图分类号:

A

基金项目:


Design and Dynamic Analysis of Light-cured Inflatable Wings
Author:
Affiliation:

Nanjing University of Aeronautics and Astronautics

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    为提高充气机翼的可靠性和稳定性,本文针对现有充气机翼提出一种利用环氧树脂的光固化特性来增强机翼刚度的方法。机翼由浸渍过环氧树脂的玻璃纤维制成,在紫外线照射下发生固化从而提高充气机翼的强度和刚度,进一步对其进行整体建模和仿真分析,验证力学特性是否满足需求。分析结果表明:光固化后的机翼可以在无内压的情况下维持其基本外形,并且模态频率具有显著的提高,通过分析固化后的机翼在受集中力和均布力情况下的数据与实验数据的对比结果发现,在集中力载荷作用下机翼的最大位移平均降低了90.26%,在均布力载荷作用下机翼的最大位移平均降低了86.7%。

    Abstract:

    To improve the reliability and stability of inflatable wings, In this paper, a method for enhancing the stiffness of existing inflatable wings is proposed by utilizing the light-curing properties of epoxy resins. The wings are made of glass fibers impregnated with epoxy resin, which are cured under ultraviolet light to improve the strength and stiffness of the aerated wing. Further modeling and simulation analysis of the aerated wing are carried out to verify whether the mechanical properties meet the requirements. The analysis results show that the light-cured wing can maintain its basic shape without internal pressure, and the modal frequency has a significant increase. The comparison between the data and the experimental data shows that the maximum displacement of the wing is reduced by 90.26% on average under the action of concentrated force load, and the maximum displacement of the wing under the action of uniform force load is reduced by 86.7% on average.

    参考文献
    相似文献
    引证文献
引用本文

李家辉,王成发,许锋. 光固化充气机翼的设计与动力学分析[J]. 科学技术与工程, , ():

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2022-04-29
  • 最后修改日期:2022-10-26
  • 录用日期:2022-11-06
  • 在线发布日期:
  • 出版日期:
×
亟待确认版面费归属稿件,敬请作者关注