复合材料加筋板筋条修理后的压缩性能

赵闯; 聂恒昌; 郭霞; 关志东

doi:10.13700/j.bh.1001-5965.2013.0431

复合材料加筋板筋条修理后的压缩性能

doi: 10.13700/j.bh.1001-5965.2013.0431

北京航空航天大学航空科学与工程学院, 北京 100191

详细信息

作者简介:
赵闯（1989- ），男，天津人，硕士生，zcmacaron@sina.cn.

中图分类号: V214.8
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- 被引次数: 0
出版历程
- 收稿日期: 2013-07-29
- 网络出版日期: 2014-06-20

Compression performance of composite stiffened panel after stiffener repair

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 承受压缩载荷时，筋条损伤往往造成复合材料加筋板结构的严重失效.针对筋条壁板脱黏、腹板分层、上缘条损伤3种情况分别设计了相应的修理方案并制作了试验件.为保证压缩载荷的均匀施加，设计制作了加筋板试验专用夹具，含有固定试验件的卡槽和保证加载方向沿竖直方向的导轨.筋条修理后的复合材料加筋板的轴向压缩试验表明不同修理部位、不同修理方法对加筋板的力学性能影响不同.有限元分析表明加筋板的屈曲模态、整体破坏模式以及板-筋胶层的破坏情况都受到修理方案的影响.
- 复合材料 /
- 加筋板 /
- 脱黏 /
- 筋条修理 /
- 压缩试验 /
- 有限元法
Abstract: Subjected to compressive load, stiffener injury often causes serious failure of stiffened composite panels. In consideration of stiffener-skin debonding, delamination in web and damage to upper flange, corresponding repair programs were designed and necessary specimens were manufactured. In order to ensure a uniform compressive load during experiment, test fixture for composite stiffened panel was designed and fabricated, containing two slots to fix the stiffened panel and four guides to ensure the vertical loading direction. All the experiments that were taken using that fixture show the influences of different repair parts, different repair methods to the mechanical properties of stiffened panels are different. Finite element analysis shows that buckling mode, failure mode of stiffened panel and skin-stiffener glue injury are both influenced by repair programs.
- composite materials /
- stiffened panel /
- debonding /
- repaired stiffener /
- compression testing /
- finite element method

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参考文献(11)

[1]	Hart-Smith L J. Adhesive bonded double lap joints[R].NASA CR-112235,1973
[2]	Hart-Smith L J. Adhesive bonded single lap joints[R].NASA CR-112236,1973
[3]	Hart-Smith L J. Adhesive bonded scarf and stepped-lap joint[R].NASACR-112237,1973
[4]	Hassan N K, Mohamedien M A,Rizkalla S H.Finite element a- nalysis of bolted connections for PFRP composites[J].Composites Part B:Engineering,1996,27(3/4):339-349
[5]	Kassapoglou C. Stress determination at skin-stiffener interfaces of composite stiffened panels under generalized loading[J].Journal of Reinforced Plastics and Composites,1994,13(6):555-571
[6]	Zhang H, Motipalli J,Lam Y C,et al.Experimental and finite element analyses on the post-buckling behaviour of repaired composite panels[J].Composites Part A:Applied Science and Manufacturing,1998,29(11):1463-1471
[7]	Mahdi S, Kinloch A J,Crisfield M A,et al.The mechanical performance of repaired stiffened panels.part II:finite element modelling[J].Composites Part B:Engineering,2002,33(5):355-366
[8]	李航,矫桂琼, 赵龙,等.含切口复合材料加筋板的压缩剩余强度研究[J].工程力学,2011,176(8):133-137 Li Hang,Jiao Guiqiong,Zhao Long,et al.Progressive failure analysis of stiffened composite plate with notch[J].Engineering Mechanics,2011,176(8):133-137(in Chinese)
[9]	孙立,许希武, 徐焜.含脱粘损伤的复合材料加筋板压缩破坏渐进损伤数值分析[J].材料科学与工程学报,2009,27(5):740-744 Sun Li,Xu Xiwu,Xu Kun.Progressive damage analysis of stiffened composite panels with debonding damage under compressive load[J].Journal of Materials Science and Engineering,2009,27(5):740-744(in Chinese)
[10]	刘从玉,许希武, 陈康.考虑脱粘的复合材料加筋板屈曲后屈曲及承载能力数值分析[J].复合材料学报,2010, 27(6): 158-166 Liu Congyu,Xu Xiwu,Chen Kang.Buckling,post-buckling and collapse analysis of stiffened composite panels with debonding damage[J].Acta Materiae Compositae Sinica,2010,27(6):158-166(in Chinese)
[11]	常园园,许希武, 郭树祥.压缩载荷下复合材料整体加筋板渐进损伤非线性数值分析[J].复合材料学报,2011, 28(4): 202-211 Chang Yuanyuan,Xu Xiwu,Guo Shuxiang.Nonlinear progressive damage analysis of integral stif fened composite panels under compressive load[J].Acta Materiae Compositae Sinica,2011,28(4):202-211(in Chinese)