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航空学报 >

2022 , Vol. 43 >Issue 6: 526851 - 526851

DOI: https://doi.org/10.7527/S1000-6893.2022.26851

综述

高性能航空复合材料结构的关键力学问题研究进展

  • 赵天 ,
  • 李营 ,
  • 张超 ,
  • 姚辽军 ,
  • 黄怿行 ,
  • 黄治新 ,
  • 陈诚 ,
  • 汪万栋 ,
  • 祖磊 ,
  • 周华民 ,
  • 裘进浩 ,
  • 邱志平 ,
  • 方岱宁
展开
  • 1. 北京理工大学 先进结构技术研究院, 北京 100081;
    2. 南京航空航天大学 航空学院, 南京 210016;
    3. 哈尔滨工业大学 航天学院, 哈尔滨 150001;
    4. 华中科技大学 材料科学与工程学院, 武汉 430074;
    5. 西北工业大学 民航学院, 西安 710072;
    6. 合肥工业大学 机械工程学院, 合肥 230009;
    7. 北京航空航天大学 航空科学与工程学院, 北京 100083

收稿日期: 2021-12-23

  修回日期: 2022-04-02

  网络出版日期: 2022-03-30

基金资助

国家自然科学基金（11902031，11902098，12002006，52171290）；航空科学基金（2020Z055072002）；北京理工大学青年教师学术启动计划

收起

Fundamental mechanical problems in high-performance aerospace composite structures: State-of-art review

  • ZHAO Tian ,
  • LI Ying ,
  • ZHANG Chao ,
  • YAO Liaojun ,
  • HUANG Yixing ,
  • HUANG Zhixin ,
  • CHEN cheng ,
  • WANG Wandong ,
  • ZU Lei ,
  • ZHOU Huamin ,
  • QIU Jinhao ,
  • QIU Zhiping ,
  • FANG Daining
Expand
  • 1. Institute of Advanced Structure Technology, Beijing Institute of Technology, Beijing 100081, China;
    2. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    3. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China;
    4. School of Materials Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China;
    5. School of Civil Aviation, Northwestern Polytechnical University, Xi'an 710072, China;
    6. School of Mechanical Engineering, Hefei University of Technology, Hefei 230009, China;
    7. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China

Received date: 2021-12-23

  Revised date: 2022-04-02

  Online published: 2022-03-30

Supported by

National Natural Science Foundation of China (11902031, 11902098, 12002006, 52171290);Aviation Science Foundation (2020Z055072002);Beijing Insitute of Technology Research Fund Program for Young Scholars

Fold

摘要

复合材料具备基于多种材料有机融合后所产生的"1+1>2"的优势，是实现航空飞行器结构轻量化、功能化与智能化的有效途径。然而，由于复合材料高各向异性、结构多尺度化等方面的特征，导致设计、制造及表征评价等方面都存在诸多问题与挑战。高性能复合材料结构在航空装备中的发展是一个涉及力学、材料、机械、控制等多学科融合的交叉性问题。本文针对其中涉及的若干关键力学问题，重点围绕近年来国内外在航空复合材料结构力学设计与性能评估、功能化设计以及制造工艺力学等3个方面的研究进展进行了概述，并对未来航空复合材料结构在这3方面的发展趋势进行了展望。

关键词： 航空飞行器; 复合材料结构; 力学性能; 功能化设计; 制造工艺力学

本文引用格式

赵天 , 李营 , 张超 , 姚辽军 , 黄怿行 , 黄治新 , 陈诚 , 汪万栋 , 祖磊 , 周华民 , 裘进浩 , 邱志平 , 方岱宁 . 高性能航空复合材料结构的关键力学问题研究进展[J]. 航空学报, 2022 , 43(6) : 526851 -526851 . DOI: 10.7527/S1000-6893.2022.26851

Abstract

Benefitting from the superiorities brought by the organic fusion of different materials, high-performance composites are considered as an effective approach to achieving light-weight design, multi-functionality and intelligentization of aviation aircraft. However, the high anisotropy and multi-scale structural properties of the composites also produce significant problems and challenges for structural design, fabrication and characterization. The application and development of high-performance composite materials in aircraft is a multi-disciplinary problem involving, material science, mechanical engineering and control technology. Focusing on several related fundamental mechanical problems, this paper mainly presents a critical review on the recent research progress in mechanical design and property evaluation, functional design and manufacturing mechanics of aircraft composite structures. An outlook for the research directions in aircraft composite structures is provided in the final part.

Key words： aviation aircraft; composite structure; mechanical property; functional design; manufacturing mechanics

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