欢迎登录材料期刊网

材料期刊网

高级检索

研究各向同性材料内胆外对称均衡缠绕纤维的厚壁圆柱形容器在内外压力作用下的应力和强度特性.采用正交各向异性本构关系和轴对称厚壁筒理论,获得纤维层和内胆的应力,以及纤维方向三向应力的解析公式.利用Hoffman和Tsai-Wu失效准则研究薄壁筒理论和三维应力对应的强度随壁厚和缠绕角的分布规律.计算比较了有、无内胆的纤维缠绕容器的强度随缠绕角的变化情况.利用ANSYS软件的层合单元SOLID191建立的模型给出的纤维向应力和强度比与本文理论结果吻合很好.研究发现:基于层合板理论的二维纤维向应力公式给出了不准确的纤维向应力,不准确的横向应力造成容器纤维层的强度值偏低;不同的纤维类型和缠绕角,厚度-半径比对强度比的影响不同;基于二维应力分析的薄壁筒理论给出的纤维层强度比小于三维分析的结果;缠绕角对无内胆的缠绕容器强度比的影响比有内胆的更敏感.

参考文献

[1] 周海成,阮海东.纤维缠绕复合材料气瓶的发展及其标准情况[J].压力容器,2004,21(9):32-36.Zhou Haicheng,Ruan Haidong.Development of filament wound composite gas cylinder and its standard condition[J].Pressure Vessel Technology,2004,21(9):32-36.
[2] 陈汝训.纤维缠绕圆筒压力容器结构分析[J].固体火箭技术,2004,27(2),105-107.Chen Ruxun.Structure analysis for filament wound cylinder pressure[J].Journal of Solid Rocket Technology,2004,27(2):105-107.
[3] 陈汝训.纤维缠绕壳体设计的网格分析方法[J].固体火箭技术,2003,26(1):30-32.Chen Ruxun.Netting analysis method for the filament-wound case design[J].Journal of Solid Rocket Technology,2003,26(1):30-32.
[4] Xia M,Takayanagi H,Kemmochi K.Analysis of multi-layered filament-wound composite pipes under internal pressure[J].Composite Structures,2001,53(4):483-491.
[5] Bakaiyan H,Hosseini H,Ameri E.Analysis of multi-layered filament-wound composite pipes under combined internal pressure and thermomechanical loading with thermal variations[J].Composite Structures,2009,88(4):532-541.
[6] Takayanagi H,Xia M,Kerrunochi K.Stiffness and strength of filament wound fiber reinforced composite pipes under internal pressure[J].Advanced Composite Materials,2002,11(2):137-149.
[7] Zheng C X,Yang F,Zhu A S.Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel[J].Journal of Zhejiang University,Science A,2009,10(3):384-391.
[8] 倪爱清,朱以文,王继辉.缠绕角对复合材料内压管强度的影响[J].武汉理工大学学报,2006,28(3):10-13.Ni Aiqing,Zhu Yiwen,Wang Jihui.The effects of winding angle on the strength of composite pipe under internal pressure[J].Journal of Wuhan University of Technology,2006,28(3):10-13.
[9] 邢静忠,陈利,孙颖.纤维缠绕厚壁柱形容器的应力和变形[J].固体火箭技术,2009,32(6):680-685.Xing Jingzhong,Chen Li,Sun Ying.Stress and deformation of filament-wound thick cylinder vessel under internal and external pressure[J].Journal of Solid Rocket Technology,2009.32(6):680-685.
[10] Ellyin F,Carroll M,Kujawski D,Chiu A S.The behavior of multidirectional filament wound fibre glass epoxy tubulars[J].Composites Part A,1997,28(9/10):781-790.
[11] Chang R R.Experimental and theoretical analyses of first-ply failure of laminated composite pressure vessels[J].Composite Structures,2000,49(2):237-243.
[12] Mertiny P,Gold A.Quantification of leakage damage in highpressure fibre-reinforced polymer composite tubular vessels[J].Polymer Testing,2007,26(2):172-179.
[13] Antoniou A E,Kensche C,Philippidis T P.Mechanical behavior of glasse/poxy tubes under combined static loadingⅠ:Experimental[J].Composites Science and Technology,2009,69(13):2241-2247.
[14] 张志民.复合材料结构力学[M].北京:北京航空航天大学出版社,1993:123-142.
[15] 蔡为仑.复合材料设计[M].北京:科学出版社,1989:380-382.
[16] Liu K S,Tsai S W.A progressive quadratic failure erierion for a laminate[J].Composite Science and Technology,1998,58(7):1023-1032.
[17] Goetschel D B,Radford D W.Analytical development of through-thickness properties of composite laminates[J].Journal of Advanced Materials,1997,29(7):37-46.
[18] Soden P D,Hinton M J,Kaddour A S.Lamina properties,lay-up configurations and loading conditions for a range of fibrereinforced composite laminates[J].Composite Science and Technology,1998,58(7):1011-1022.
[19] 沃丁柱.复合材料大全[M].北京:化学工业出版社,2000:599-600.
[20] Tabakov P Y,Summers E B.Lay-up optimization of multilayered anisotropic cylinders based on a 3D elasticity solution[J].Computers and Structures,2006,84(5/6):374-384.
[21] Mertiny P,Ellyin F,Hothan A.An experimental investigation on the effect of multi-angle filament winding on the strength of tubular composite structures[J].Composite Science and Technology,2004,64(1):1-9.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%