航空航天装备的轻量化：挑战与未来

张卫红; 唐长红

doi:10.7527/S1000-6893.2023.29965

航空学报 >

2024 , Vol. 45 >Issue 5: 529965 - 529965

DOI: https://doi.org/10.7527/S1000-6893.2023.29965

综述

航空航天装备的轻量化：挑战与未来

张卫红 ,
唐长红

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^1.西北工业大学陕西省空天结构技术重点实验室，西安 710072
^2.航空工业第一飞机设计研究院，西安 710089

．E-mail： zhangwh@nwpu.edu.cn

收稿日期: 2023-11-05

修回日期: 2023-11-20

录用日期: 2023-12-15

网络出版日期: 2023-12-18

基金资助

国家自然科学基金(12032018)

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Lightweighting of aerospace and aeronautical equipment: Challenges and perspectives

Weihong ZHANG ,
Changhong TANG

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^1.Shaanxi Key Laboratory of Aerospace Structures，Northwestern Polytechnical University，Xi’an 710072，China
^2.AVIC the First Aircraft Institute，Xi’an 710089，China

E-mail： zhangwh@nwpu.edu.cn

Received date: 2023-11-05

Revised date: 2023-11-20

Accepted date: 2023-12-15

Online published: 2023-12-18

Supported by

National Natural Science Foundation of China(12032018)

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摘要

轻量化是航空航天装备研发领域永恒的主题，它对装备的综合性能和服役效能具有决定性影响。在过去的数十年里，一系列高性能优化设计方法、新材料和制造工艺技术的研发和应用，不断推动航空航天装备轻量化水平的提升。然而，随着新一代装备对综合性能和多功能需求的不断增加，现有的轻量化设计制造技术正面临着日益严峻的挑战。因此，本文重点探讨了航空航天装备研发的总体设计、机电系统设计、材料与结构、高性能制造与装配等主要环节，并分析了轻量化技术在未来的发展趋势。

关键词： 航空航天装备; 轻量化设计与制造; 装备总体技术; 材料与结构技术; 高性能制造与装配

本文引用格式

张卫红 , 唐长红 . 航空航天装备的轻量化：挑战与未来[J]. 航空学报, 2024 , 45(5) : 529965 -529965 . DOI: 10.7527/S1000-6893.2023.29965

Abstract

Lightweight is a substantial theme in the research and development of aerospace and aeronautical equipment due to its decisive impact on the comprehensive performance and operational efficiency of the equipment. Over the past decades， a handful of innovative optimization design approaches， emerging high-performance materials， and revolutionary manufacturing technologies have been uninterruptedly developed， and the level of lightweighting in aerospace and aeronautical equipment has been significantly advanced. However， the increasing demands for comprehensive performance and multifunctionality of the next generation of equipment present serious challenges to existing lightweight design and manufacturing technologies. Therefore， with a particular emphasis on the layout design， electromechanical system design， materials and structures， high-performance manufacturing and assembly， this paper analyzes the posed challenges and future perspectives.

Key words： aerospace and aeronautical equipment; lightweight design and manufacturing; equipment layout technology; material and structure technology; high-performance manufacturing and assembly

参考文献

1	中华人民共和国国务院新闻办公室. 2021中国的航天［R/OL］. （2022-01-28）［2023-09-11］. .
	The State Council Information Office of the People’s Republic of China. White paper： China’s space program： a 2021 perspective ［R/OL］. （2022-01-28）［2023-09-11］. （in Chinese）.
2	中国航空工业集团有限公司. 通用航空产业发展白皮书（2022）［R/OL］. （2022-11-09）［2023-09-11］. .
	Aviation Industry Corporation of China， Ltd. White paper： General aviation industry development ［R/OL］. （2022-11-09）［2023-09-11］. （in Chinese）.
3	National Aeronautics and Space Administration. NASA selects proposals for ultra-lightweight materials for journey to Mars and beyond ［EB/OL］. （2015-04-09）［2023-09-11］. .
4	Royal Netherlands Aerospace Centre. White paper： Aircraft structural design in the future ［R/OL］. （2021-03-01）［2023-09-11］. .
5	MERLIN P W. Green light for green flight： NASA’s contributions to environmentally responsible aviation ［R］. Washington： National Aeronautics and Space Administration， 2020.
6	National Aeronautics and Space Administration. NASA issues award for greener， more fuel-efficient airliner of future ［EB/OL］. （2023-1-19）［2023-9-16］. .
7	National Aeronautics and Space Administration. NASA’s new material built to withstand extreme conditions ［EB/OL］. （2022-06-03）［2023-9-16］. .
8	LOBNER P. DARPA/ Lockheed Martin-ISIS stratospheric airship ［R/OL］. （2023-6-16）［2023-9-16］. .
9	KARNOZOV V. Russia targets low cost， high performance with Su-75 Checkmate fighter ［EB/OL］. （2021-07-21）［2023-9-16］. .
10	MARSH G. Airbus takes on Boeing with reinforced plastic A350 XWB［J］. Reinforced Plastics， 2007， 51（11）： 26-29.
11	SANJAY M R， PARAMESWARANPILLAI J， SIENG? CHIN S， et al. Lightweight polymer composite structures： design and manufacturing techniques［M］. 2020.
12	ZHU J H， ZHANG W H， XIA L. Topology optimization in aircraft and aerospace structures design［J］. Archives of Computational Methods in Engineering， 2016， 23（4）： 595-622.
13	全栋梁，时光辉，关成启，等. 结构优化技术在高速飞行器上的应用与面临的挑战［J］. 力学与实践， 2019， 41（4）： 373-381.
	QUAN D L， SHI G H， GUAN C Q， et al. Applications and challenges of structural optimization in high-speed aerocraft［J］. Mechanics in Engineering， 2019， 41（4）： 373-381 （in Chinese）.
14	张卫红，周涵，李韶英. 航天高性能薄壁构件的材料-结构一体化设计［J］. 航空学报， 2023， 44（9）： 627428.
	ZHANG W H， ZHOU H， LI S Y， et al. Material-structure integrated design for high-performance aerospace thin-walled component ［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（9）： 627428 （in Chinese）.
15	ZHU J， ZHANG W， BECKERS P. Integrated layout design of multi‐component system［J］. International Journal for Numerical Methods in Engineering， 2009， 78（6）： 631-651.
16	LI L， ZHANG K， CHENG H， et al. Experimental and simulation investigations on the morphology of aerosol jet printed polymer traces under in-situ UV and thermal curing conditions［J］. Additive Manufacturing， 2023， 69： 103515.
17	MENG L， ZHANG W H， QUAN D， et al. From topology optimization design to additive manufacturing： Today’s success and tomorrow’s roadmap ［J］. Archives of Computational Methods in Engineering， 2020， 27（3）： 805-830.
18	MENG L， SHI J， YANG C， et al. An emerging class of hyperbolic lattice exhibiting tunable elastic properties and impact absorption through chiral twisting ［J］. Extreme Mechanics Letters， 2020， 40： 100869.
19	XU Y， ZHU J， WU Z， et al. A review on the design of laminated composite structures： constant and variable stiffness design and topology optimization ［J］. Advanced Composites and Hybrid Materials， 2018， 1（3）： 460-477.
20	MENG L， QIU X， GAO T， et al. An inverse approach to the accurate modelling of 3D-printed sandwich panels with lattice core using beams of variable cross-section ［J］. Composite Structures， 2020， 247： 112363.
21	CORDIS （Community Research and Development Information Service）. Zero-defect manufacturing of composite parts in the aerospace industry［EB/OL］. （2019-9-30）［2023-9-16］. .
22	侯杰，朱继宏，王创，等. 考虑机械连接载荷和疲劳性能的装配结构拓扑优化设计方法［J］. 科学通报， 2019， 64（1）： 79-86.
	HOU J， ZHU J H， WANG C， et al. Topology optimization of the multi-fasteners jointed structure considering joint load constraint and fatigue constraints ［J］. Chinese Science Bulletin， 2019， 64（1）： 79-86 （in Chinese）.
23	YANG Y， YUAN J W， LIU H C， et al. Generalized model for dynamics and stability of milling of titanium alloys by integrating process damping， multiple modes and multiple delays ［J］. Journal of Manufacturing Processes， 2023， 102： 718-735.
24	ZHANG K， LI H， CHENG H， et al. Combined effects of seawater ageing and fatigue loading on the bearing performance and failure mechanism of CFRP/CFRP single-lap bolted joints ［J］. Composite Structures， 2020， 234： 111677.
25	悦增建. 案例展示［EB/OL］. （2021-07-21）［2023-9-16］. .
	YUE Z J. Case showcase ［EB/OL］. （2021-07-21）［2023-9-16］. （in Chinese）.

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