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柔性变形翼结构设计、建模与分析研究进展

李琦 杨宇 王志刚 崔龙 张峰 王宏伟 邓扬晨

航空科学技术2024,Vol.35Issue(6):1-11,11.
航空科学技术2024,Vol.35Issue(6):1-11,11.DOI:10.19452/j.issn1007-5453.2024.06.001

柔性变形翼结构设计、建模与分析研究进展

Research Progress on the Design,Modeling and Analysis of Flexible Deformable Wing Structures

李琦 1杨宇 2王志刚 2崔龙 3张峰 3王宏伟 3邓扬晨4

作者信息

  • 1. 辽宁大学,辽宁 沈阳 110036
  • 2. 中国飞机强度研究所,陕西 西安 710065
  • 3. 中国科学院沈阳自动化研究所,辽宁 沈阳 110016
  • 4. 航空工业沈阳飞机设计研究所,辽宁 沈阳 110035
  • 折叠

摘要

Abstract

The design of future aircraft will face severe challenges such as the continuous expansion of airspace domain and the speed domain,and the increasing requirements for the mission adaptability.The morphing aircraft can provide new ideas and methods for improving the flight performance and expanding the flight envelope.The use of the flexible skin combined with corresponding support structures has become the main solution to overcome the shortcomings of traditional morphing aircrafts.Firstly,the status of the research of flexible skin,honeycomb support structure,and other new smart material in the morphing aircraft design is reviewed.Then,the design,modeling and analysis methods of the flexible deformable wing structures in the existing literature are discussed.Finally,the existing problems in the modeling and analysis methods of flexible deformable wing structures and possible future research directions are proposed.

关键词

变体飞行器/柔性蒙皮/建模分析/支撑结构/智能材料

Key words

morphing aircraft/flexible skin/modeling and analysis/support structure/smart material

分类

航空航天

引用本文复制引用

李琦,杨宇,王志刚,崔龙,张峰,王宏伟,邓扬晨..柔性变形翼结构设计、建模与分析研究进展[J].航空科学技术,2024,35(6):1-11,11.

基金项目

国家自然科学基金(U2013208) National Natural Science Foundation of China(U2013208) (U2013208)

航空科学技术

1007-5453

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