特殊布局飞机高承载开口结构优化设计

doi:10.7527/S1000-6893.2025.32447

Abstract

Abstract:

The present study addresses the challenges of stiffness and strength design for large-opening structures in special configuration aircraft such as blended wing-body aircraft. By combining mechanical principles and numerical simulation methods， this research investigates the stability analysis of long-span opening load-bearing beams. A method for analyzing the buckling characteristics of opening beams under the influence of multiple elastic supports from frames is established， providing design requirements for frame stiffness. Additionally， the study explores the collaborative optimization of structural arrangement and stiffness for opening beams and frames. Through case studies， the interaction between frame spacing and cross-sectional parameters of beams and frames is revealed. Furthermore， the research conducts failure analysis and load-bearing capacity prediction for aircraft opening structures， developing a coupled failure analysis method using a Nastran-Abaqus based multi-level non-intrusive model coupling analysis. Experimental validation is performed using typical large-opening structure failure tests. Comparative results show that finite element simulation effectively captures the nonlinear load and deformation behavior during testing， with maximum errors of 8.8% and 7.1% in load and deformation predictions， respectively. The simulation results also demonstrate good agreement with experimental buckling phenomena and failure modes.

Key words: special configuration aircraft, large-opening structures, stiffness and strength, optimization design, non-intrusive model coupling analysis

CLC Number:

V215.2

Yanjie LIU, Mingqiang LI, Xuan GUO, Yanfei SU, Bintuan WANG, Yingju XUE. Optimization design of high-load-bearing opening structures in special configuration aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(21): 532447.

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References 21

[1]	刘建，陈勇，曹洲. 考虑剪切变形影响的开口薄壁梁约束扭转的扭转角分析［J］. 应用力学学报， 2016， 33（4）： 678-683， 742.
	LIU J， CHEN Y， CAO Z. Torsion angle analysis of restrained torsion theory for open thin walled beams considering shear deformation［J］. Chinese Journal of Applied Mechanics， 2016， 33（4）： 678-683， 742 （in Chinese）.
[2]	李慧，王琳. 扇性正应力在工程结构计算中的应用［J］. 贵州大学学报（自然科学版）， 2014， 31（6）： 17-19.
	LI H， WANG L. Application of sector normal stress in engineering structure calculation［J］. Journal of Guizhou University （Natural Sciences）， 2014， 31（6）： 17-19 （in Chinese）.
[3]	苏雁飞，谭申刚，薛应举，等. 运输类飞机机身大开口结构加强方式理论研究［J］. 力学与实践， 2013， 35（6）： 59-64.
	SU Y F， TAN S G， XUE Y J， et al. The strengthening of aero-transport with large opening［J］. Mechanics in Engineering， 2013， 35（6）： 59-64 （in Chinese）.
[4]	王玉，薛应举，谷迎松. 大型运输机机身大开口结构强度设计方法［J］. 机械科学与技术， 2015， 34（7）： 1144-1148.
	WANG Y， XUE Y J， GU Y S. Strength design of fuselage structure for large scale aero-transport with large opening［J］. Mechanical Science and Technology for Aerospace Engineering， 2015， 34（7）： 1144-1148 （in Chinese）.
[5]	李保江，邵济明，王长焕，等. 天地往返飞行器大开口舱门关键技术及其解决途径［J］. 航空学报， 2016， 37（）： 8-15.
	LI B J， SHAO J M， WANG C H， et al. Key technologies and solutions for large extensible door of re-entry space vehicle［J］. Acta Aeronautica et Astronautica Sinica， 2016， 37（Sup 1）： 8-15 （in Chinese）.
[6]	苏雁飞，赵占文，李明强. 飞机槽型大开口结构刚度加强研究［J］. 固体力学学报， 2022， 43（6）： 783-790.
	SU Y F， ZHAO Z W， LI M Q. Study on rigidity strengthening for aircraft with slots of large openings［J］. Chinese Journal of Solid Mechanics， 2022， 43（6）： 783-790 （in Chinese）.
[7]	苏雁飞，赵占文，王斌团. 受扭多槽矩型开口结构载荷分布与应力计算［J］. 机械研究与应用， 2022， 35（1）： 58-61， 64.
	SU Y F， ZHAO Z W， WANG B T. Load distribution and stress analysis of the rectagular multi-cabin opening structure under torque moment［J］. Mechanical Research & Application， 2022， 35（1）： 58-61， 64 （in Chinese）.
[8]	毛晓晔，邵志华，舒送，等. 中间支撑刚度对双跨梁屈曲稳定性的影响［J］. 振动与冲击， 2022， 41（11）： 1-9， 17.
	MAO X Y， SHAO Z H， SHU S， et al. Effect of intermediate support stiffness on buckling stability of a double-span beam［J］. Journal of Vibration and Shock， 2022， 41（11）： 1-9， 17 （in Chinese）.
[9]	陈悦，朱锡，李华东，等. 复合材料夹芯梁屈曲破坏模式及极限承载［J］. 复合材料学报， 2016， 33（5）： 991-997.
	CHEN Y， ZHU X， LI H D， et al. Buckling failure mode and ultimate load of composite sandwich beam［J］. Acta Materiae Compositae Sinica， 2016， 33（5）： 991-997 （in Chinese）.
[10]	刘向民，姚卫星，陈方. 复合材料层合板结构冲击损伤数值模拟的损伤力学模型［J］. 航空学报， 2016， 37（10）： 3054-3063.
	LIU X M， YAO W X， CHEN F. Damage mechanics model for simulating impact responses of composite laminated structures［J］. Acta Aeronautica et Astronautica Sinica， 2016， 37（10）： 3054-3063 （in Chinese）.
[11]	苏少普，常文魁，陈先民. 飞机典型壁板结构剪切屈曲疲劳试验与分析方法［J］. 航空学报， 2022， 43（5）： 225219.
	SU S P， CHANG W K， CHEN X M. Fatigue buckling test and analytical approach of aircraft typical panel structures［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（5）： 225219 （in Chinese）.
[12]	芦冠达，黄争鸣. 应用桥联理论与有限元模型的航空复合材料结构失效分析［J］. 航空学报， 2018， 39（6）： 221646.
	LU G D， HUANG Z M. Failure analysis of aeronautic composite structures incorporated with bridging model and FE model［J］. Acta Aeronautica et Astronautica Sinica， 2018， 39（6）： 221646 （in Chinese）.
[13]	解江，宋山山，宋东方，等. 复合材料C型柱轴压失效分析的层合壳建模方法［J］. 航空学报， 2019， 40（2）： 522395.
	XIE J， SONG S S， SONG D F， et al. Stacked shell modeling method for failure analysis of composite C-channels subject to axial compression［J］. Acta Aeronautica et Astronautica Sinica， 2019， 40（2）： 522395 （in Chinese）.
[14]	黄旌，卢钧，毕大园，等. 基于有限元分析的机翼损伤评估的建模［J］. 长江大学学报A（自然科学版）， 2006， 3（2）： 59-62， 8.
	HUANG J， LU J， BI D Y， et al. Modeling on air plane wing damage evaluation based on finite element analysis［J］. Journal of Yangtze University （Natural Science Edition）， 2006， 3（2）： 59-62， 8 （in Chinese）.
[15]	冯振宇，解江，李恒晖，等. 大飞机货舱地板下部结构有限元建模与适坠性分析［J］. 航空学报， 2019， 40（2）： 522394.
	FENG Z Y， XIE J， LI H H， et al. Finite element modeling and crashworthiness analysis of large aeroplane sub-cargo structure［J］. Acta Aeronautica et Astronautica Sinica， 2019， 40（2）： 522394 （in Chinese）.
[16]	陈彦达，范振民，李军. 飞机螺栓双剪连接结构有限元应力分析［J］. 民用飞机设计与研究， 2020（3）： 17-23.
	CHEN Y D， FAN Z M， LI J. Finite element stress analysis of aircraft double shear bolted connection［J］. Civil Aircraft Design & Research， 2020（3）： 17-23 （in Chinese）.
[17]	聂珊珊，聂小华. 多层级有限元模型数据库综合设计与应用［J］. 工程与试验， 2021， 61（4）： 84-86.
	NIE S S， NIE X H. Comprehensive design and application of multi-level finite element model database［J］. Engineering & Test， 2021， 61（4）： 84-86 （in Chinese）.
[18]	黄勇，李三平. 民用飞机结构强度设计中的全机精细有限元分析技术及其应用［J］. 计算机辅助工程， 2018， 27（3）： 35-38， 53.
	HUANG Y， LI S P. Global detailed finite element analysis technique and its application in structural strength design of civil aircraft［J］. Computer Aided Engineering， 2018， 27（3）： 35-38， 53 （in Chinese）.
[19]	LIU Y J， SUN Q， FAN X L. A non-intrusive global/local algorithm with non-matching interface： Derivation and numerical validation［J］. Computer Methods in Applied Mechanics and Engineering， 2014， 277： 81-103.
[20]	GENDRE L， ALLIX O， GOSSELET P， et al. Non-intrusive and exact global/local techniques for structural problems with local plasticity［J］. Computational Mechanics， 2009， 44（2）： 233-245.
[21]	BETTINOTTI O， ALLIX O， MALHERBE B. A coupling strategy for adaptive local refinement in space and time with a fixed global model in explicit dynamics［J］. Computational Mechanics， 2014， 53（4）： 561-574.

Optimization design of high-load-bearing opening structures in special configuration aircraft

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