Load sharing ability of the liner in type III composite pressure vessels under internal pressure

被引:38
作者
Almeida, Jose Humberto S., Jr. [1 ,3 ]
Faria, Hugo [2 ]
Marques, Antonio T. [3 ]
Amico, Sandro C. [1 ]
机构
[1] UFRGS Fed Univ Rio Grande do Sul, PPGE3M, BR-91501970 Porto Alegre, RS, Brazil
[2] INEGI Inst Mech Engn & Ind Management, Oporto, Portugal
[3] Univ Porto, FEUP Fac Engn, P-4100 Oporto, Portugal
关键词
Composite overwrapped pressure vessel; finite element analysis; liner load share; thickness ratio; filament winding; THICKNESS; STORAGE; DESIGN;
D O I
10.1177/0731684414560221
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this work, the load sharing ability of metallic liners in type III composite overwrapped pressure vessel was investigated by means of accurate numerical models based on finite element method in order to realistically represent the hybrid metal-composite structure. The varying thickness of the composite layers throughout the dome, as well as their angles, were accounted for in the model. The study focused on the influence of material properties and liner-to-composite thickness ratio on the stress and strain distribution between liner and composite at the cylindrical, dome, and polar boss regions. Two novel concepts for the evaluation of the structural response of a composite overwrapped pressure vessel were introduced, namely: (i) the liner stress and strain fractions, and (ii) the correlation with liner-to-composite thickness ratio. The results show complex overall behavior close to the onset of plasticity of the liner, which is critically investigated. A decrease in liner stress fraction was found for higher internal pressure loads since the stress field is increasingly dominated by the composite overwrap. Also, the von Mises equivalent stress along the longitudinal profile of the structure showed a peak at the dome of the liner, whereas for the composite, the peak was at the shoulder region. This was justified considering that, at low pressure, the liner operates elastically in compression-tension mode and the composite in tension-tension mode.
引用
收藏
页码:2274 / 2286
页数:13
相关论文
共 17 条
  • [1] Akula VMK, 2013, AM SOC COMP 28 TECHN, P1
  • [2] Progressive failure analysis for filament wound pressure vessel
    Doh, YD
    Hong, CS
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1995, 14 (12) : 1278 - 1306
  • [3] Faria H, 2009, 1 INT C COMP MAT STR, P1
  • [4] Finite element analysis of composite pressure vessels with a load sharing metallic liner
    Kabir, MZ
    [J]. COMPOSITE STRUCTURES, 2000, 49 (03) : 247 - 255
  • [5] Kaw A.K., 2005, MECH COMPOS MATER
  • [6] Kim C, 2001, J REINF PLAST COMP, V20, P166
  • [7] Multi-sequence dome lay-up simulations for hydrogen hyper-bar composite pressure vessels
    Leh, D.
    Saffre, P.
    Francescato, P.
    Arrieux, R.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2013, 52 : 106 - 117
  • [8] Optimal design of a composite laminate hydrogen storage vessel
    Lin, David T. W.
    Hsieh, Jui-Ching
    Chindakham, Nachaya
    Hai, Pham Duy
    [J]. INTERNATIONAL JOURNAL OF ENERGY RESEARCH, 2013, 37 (07) : 761 - 768
  • [9] Park JS, 2002, J COMPOS MATER, V36, P2373, DOI [10.1177/0021998302036020870, 10.1106/002199802027870]
  • [10] Analysis of filament wound composite structures considering the change of winding angles through the thickness direction
    Park, JS
    Hong, CS
    Kim, CG
    Kim, CU
    [J]. COMPOSITE STRUCTURES, 2002, 55 (01) : 63 - 71