国防科技大学学报2023，Vol.45Issue(6)：20-31,12.DOI:10.11887/j.cn.202306003
尾座式电动飞机复合材料机翼结构优化设计
Structural optimization for composite wings of tail-sitter electric aircraft
摘要
Abstract
According to the requirements of material delivery platform in the complex terrain area,the research on the structural design of the composite wing of the tail-sitter electric aircraft was carried out.Based on the load analysis,the structural configuration and lay out designs were studied,and the structural design scheme of the composite wing was proposed.The finite element model of the composite wing was developed and the static strength analyses under different operating conditions were completed.The deformation,structural stress,and Tsai-Wu failure factor distribution of the wing structure were obtained.The structural optimal analysis of the composite wing was performed on the basis of the stepwise optimization strategy with the layer thicknesses and angles as design variables.The optimal results show that the structural mass is reduced by 47.77％under the constraints of structural stiffness and strength,which can provide the important reference for the design and development of the tail-sitter electric aircraft structure.关键词
尾座式电动飞机/复合材料机翼/有限元分析/结构优化设计Key words
tail-sitter electric aircraft/composite wings/finite element analysis/structural optimization分类
航空航天引用本文复制引用
麻震宇,张祎桀,张琪,邓小龙,于乃辉..尾座式电动飞机复合材料机翼结构优化设计[J].国防科技大学学报,2023,45(6):20-31,12.基金项目
国家自然科学基金资助项目(51605484) （51605484）
国家重大专项支持项目资助项目(GFZX040201) （GFZX040201）
