论文:2021,Vol:39,Issue(3):586-592
引用本文:
郭妍宁, 马玉娥, 孙文博, 薛勇, 邝春伟. 残余应力对多焊缝整体加筋壁板稳定性影响研究[J]. 西北工业大学学报
GUO Yanning, MA Yu'e, SUN Wenbo, XUE Yong, KUANG Chunwei. Effects of residual stress on the stability of multi-welded integral stiffened panels[J]. Northwestern polytechnical university

残余应力对多焊缝整体加筋壁板稳定性影响研究
郭妍宁1, 马玉娥1, 孙文博1, 薛勇2, 邝春伟2
1. 西北工业大学 航空学院, 陕西 西安 710072;
2. 中航通飞华南飞机工业有限公司, 广东 珠海 519000
摘要:
为明确残余应力对2024-T3搅拌摩擦焊多焊缝整体加筋壁板稳定性的影响,采用ANSYS有限元软件建立了2种典型搅拌摩擦焊接多焊缝加筋壁板数值计算模型。通过热力耦合算法分别计算了2种加筋壁板(A,B)的残余应力分布,并对其进行屈曲和后屈曲分析。结果表明:多焊缝整体加筋壁板的残余应力受焊接顺序影响,加筋壁板A的残余应力主要集中在长桁右侧,加筋壁板B的残余应力则集中在焊接顺序靠后的长桁处。残余应力对加筋壁板稳定性影响较大。考虑残余应力后,加筋壁板A的临界屈曲载荷降低了14.2%,加筋壁板B降低了12.4%。
关键词:    搅拌摩擦焊    加筋壁板    多焊缝    残余应力    稳定性    承载力   
Effects of residual stress on the stability of multi-welded integral stiffened panels
GUO Yanning1, MA Yu'e1, SUN Wenbo1, XUE Yong2, KUANG Chunwei2
1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. China Aviation Industry General Aircraft Co., Ltd, Zhuhai 519000, China
Abstract:
In order to clarify the influence of residual stress on the stability of 2024-T3 friction stir welded(FSWed) integral stiffened panels with multi-welds, the ANSYS software was used to establish the finite element models of two typical multi-FSWed stiffened panels. The residual stresses of two typical multi-welded stiffened panels (Panel A and Panel B) were calculated respectively using the thermal-mechanical coupling method. And the buckling and post-buckling responses of the stiffened plates were analyzed. It is shown that the residual stress distribution of stiffened panel was affected by the welding sequence. The maximum residual stress of Panel A mainly appears on the right side of the stringer, and that of Panel B appears on the stringer that is welded later. The residual stress has a great influence on the stability of the welded stiffened panels. When the residual stress profiles are taken into consideration, the critical buckling loads of welded Panel A and Panel B will decrease 14.2% and 12.4% respectively.
Key words:    friction stir welding    stiffened panel    multi-welded    residual stress    stability    bearing capacity   
收稿日期: 2020-09-14     修回日期:
DOI: 10.1051/jnwpu/20213930586
基金项目: 国家自然科学基金(11572250,91860128)资助
通讯作者: 马玉娥(1975-),女,西北工业大学教授,主要从事结构力学和结构强度研究。e-mail:ma.yu.e@nwpu.edu.cn     Email:ma.yu.e@nwpu.edu.cn
作者简介: 郭妍宁(1990-),女,西北工业大学博士研究生,主要从事焊接残余应力研究。
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参考文献:
[1] 白承正, 宋欣, 盛宏威, 等.飞机焊接加筋壁板拉伸强度预估方法研究[J].机械强度, 2019, 41(1):157-162 BAI Chengzheng, SONG Xin, SHENG Hongwei, et al. Study on estimation method of tensile strength of aircraft stiffened-welded plate[J]. Journal of Mechanical Strength, 2019, 41(1):157-162(in Chinese)
[2] 刘建光, 胡忠民, 吴为. 铝合金加筋壁板搅拌摩擦焊接残余应力及变形分析[J], 精密成形工程, 2017, 9(4):101-106 LIU Jianguang, HU Zhongmin, WU Wei. Residual stress and deformation in friction stir welding of aluminium stiffened panel[J]. Journal of Netshape Forming Engineering, 2017, 9(4):101-106(in Chinese)
[3] 付瑞东, 李艺君. 我国搅拌摩擦焊技术的发展及展望[J]. 金属加工(热加工), 2020, 6:14-18 FU Ruidong, LI Yijun. Development and prospect of friction stir welding technology in China[J]. Metal Processing (Hot-working), 2020, 6:14-18(in Chinese)
[4] 荆慧强, 贾延奎, 刘国英, 等. 大型多焊缝结构焊接残余应力计算方法研究[J]. 焊接技术, 2017, 46(2):23-26 JING Huiqiang, JIA Yankui, LIU Guoying, et al. Research on welding residual stress calculation of large and multi-weld structure[J]. Welding Technology, 2017, 46(2):23-26(in Chinese)
[5] 栾国红, North T H, 郭德伦, 等. 铝合金搅拌摩擦焊接头行为分析[J]. 焊接学报, 2002, 23(6):62-66 LUAN Guohong, NORTH T H, GUO Delun, et al. Characterizations of friction stir welding on aluminum alloy[J]. Trans of the China Welding Institution, 2002, 23(6):62-66(in Chinese)
[6] 成中山, 林清宇, 王宽福. 球形容器"十"字焊缝的残余应力分析及缺陷修复[J]. 石油工程建设, 1994, 4:38-41 CHENG Zhongshan, LIN Qingyu, WANG Kuanfu. To analuse the residual stress of cruciform welding seams on spherical vessels and repair the defects thereof[J]. Petroleum Engineering Construction, 1994, 4:38-41(in Chinese)
[7] 张天弛, 张明, 李博, 等. 基于电子散斑干涉的载人航天器密封舱焊缝残余应力测试方法[J]. 载人航天, 2018, 24(5):674-678 ZHANG Tianchi, ZHANG Ming, LI Bo, et al. Testing method for residual stress in welds of manned spacecraft cabin based on electronic speckle pattern interferometry[J]. Manned Spaceflight, 2018, 24(5):674-678(in Chinese)
[8] LEE Jaeho, JANG Beomseon, KIM Hyeonjin, et al. The effect of weld residual stress on fracture toughness at the intersection of two welding lines of offshore tubular structure[J]. Marine Structures, 2020, 7:102708
[9] JUN S M, HONG C S. Buckling behavior of laminated composite cylindrical panels under axial compression[J]. Computers & Structures, 1988, 29(3):479-490
[10] 李振远. 机身新型焊接加筋壁板压缩失稳载荷预估方法研究[D]. 哈尔滨:哈尔滨理工大学, 2016 LI Zhenyuan. The study of compression instability load estimated methods of new stiffened-welded aircraft plate[D]. Harbin:Harbin University of Science and Technology, 2016(in Chinese)
[11] 郭敏. 加筋薄板单边焊接屈曲变形及其影响因素研究[D]. 上海:上海交通大学, 2017 GUO Min. Study of welding buckling distortion and its influence factors of a multiply stiffened thin-plate structure under single-side welds[D]. Shanghai:Shanghai Jiaotong University, 2017(in Chinese)
[12] 周亮. 考虑初始残余应力的薄板焊接屈曲变形分析[D]. 重庆:重庆交通大学, 2018 ZHOU Liang. Numerical simulation of welding buckling deformation in thin plates with considering initial residual stress influences[D]. Chongqing:Chongqing Jiaotong University, 2018(in Chinese)
[13] 于健. 考虑连接性能的搅拌摩擦点焊加筋壁板力学性能分析[D]. 南京:南京航空航天大学, 2015 YU Jian. On mechanical properties of friction stir welded stiffened panel considering the effect of connection[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2018(in Chinese)
[14] YOON J W, BRAY G H, VALENTE R A F, et al. Buckling analysis for an integrally stiffened panel structure with a friction stir weld[J]. Thin-Walled Structures, 2009, 47(12):1608-1622
[15] MURPHY A, EKMEKYAPAR T, ZAKCA M, et al. Buckling/post-buckling strength of friction stir welded aircraft stiffened panels[J]. Journal of Aerospace Engineering, 2014, 228(2):178-192
[16] MURPHY A, MCCUNE W, QUINN D, et al. The characterisation of friction stir welding process effects on stiffened panel buckling performance[J]. Thin-Walled Structures, 2007, 45(3):339-351
[17] MURPHY A, LYNCH F, PRICE M, et al. Modified stiffened panel analysis methods for laser beam and friction stir welded aircraft panels[J]. Proceedings of the Institution of Mechanical Engineers, 2006, 220(4):267-278
[18] CHEN C M, KOVACEVIC R. Finite element modeling of friction stir welding-thermal and thermo mechanical analysis[J]. International Journal of Machine Tools & Manufacture, 2003, 43:1319-1326
[19] SONNE M R, TUTUM C C, HATTEL J H, et al. The effect of hardening laws and thermal softening on modeling residual stresses in FSW of aluminum alloy 2024-T3[J]. Journal of Materials Processing Technology, 2013, 213:477-486
[20] HE Xiaocong, GU Fengshou, BALL Andrew. A review of numerical analysis of friction stir welding[J]. Progress in Materials Science, 2014, 65:1-66
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