航空动力学报2024,Vol.39Issue(11) :21-29.DOI:10.13224/j.cnki.jasp.20220876

纤维增强截顶圆锥壳固有特性计算及分析

Natural characteristics calculation and analysis of fiber reinforced truncated conical shell

许卓 许沛尧 郑利胜 李晖 李鹤 顾大卫 何明阳 韩清凯 闻邦椿
航空动力学报2024,Vol.39Issue(11) :21-29.DOI:10.13224/j.cnki.jasp.20220876

纤维增强截顶圆锥壳固有特性计算及分析

Natural characteristics calculation and analysis of fiber reinforced truncated conical shell

许卓 1许沛尧 2郑利胜 3李晖 4李鹤 4顾大卫 5何明阳 2韩清凯 4闻邦椿4
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作者信息

  • 1. 东北电力大学机械工程学院,吉林 132011;东北大学机械工程与自动化学院,沈阳 110819
  • 2. 东北电力大学机械工程学院,吉林 132011
  • 3. 温州市工业科学研究院,浙江温州 325028
  • 4. 东北大学机械工程与自动化学院,沈阳 110819;东北大学航空动力装备振动及控制教育部重点实验室,沈阳 110819
  • 5. 东北大学航空动力装备振动及控制教育部重点实验室,沈阳 110819;浙江工业大学机械工程学院,杭州 310014
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摘要

以理论与实践相结合的方式分析了纤维增强截顶圆锥壳的固有特性.针对纤维增强复合圆锥壳的结构特性引入半锥角系数,考虑复合结构各向异性的影响,基于经典层合理论对其进行了理论建模;利用Rayleigh-Ritz法和正交多项式法求解了结构的固有特性.通过搭建相应的实验系统,以TC300/环氧树脂复合圆锥壳为研究对象进行测试,结果表明:该方法所获得固有频率的结果与试验测试结果间的误差在1.4%~2.3%之间,进而验证了所提出模型的正确性.最后,讨论了半锥角大小、不同约束方式和不同纤维铺层角度等参数对结构固有特性的影响规律.

Abstract

The natural characteristics of composite conical shells were calculated and verified by combining theory and experiment.Based on the classical lamination theory and considering the influence of anisotropy of composite structures,the theoretical model was established by introducing half-cone angle coefficients.Then,the natural characteristics of the structures were obtained by utilizing the Rayleigh-Ritz method and orthogonal polynomial method.A natural characteristic experiment system of TC300/epoxy resin composite conical shell was established and the natural characteristics were acquired.The results showed that the error between the calculated and test results was between 1.4%and 2.3%,which further verified the correctness of the proposed model.Finally,the influences of different parameters,such as the half cone angle,the boundary conditions and the fiber ply angles,on the natural characteristics of the structure were discussed.

关键词

纤维增强复合结构/截顶圆锥壳/固有特性/Rayleigh-Ritz法/正交多项式

Key words

fiber reinforced composite structures/truncated conical shell/natural characteristics/Rayleigh-Ritz/orthogonal polynomial

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出版年

2024
航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
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