Influence of Manufacturing Variances on the Strength of Pressure Vessels: Analytical Study

被引：0
作者：
Chaitanya, Ch Sri [1 ]
Rao, R. Narasimha [1 ]
机构：
[1] Natl Inst Technol Warangal, Dept Mech Engn, Warangal 506004, Andhra Pradesh, India
来源：
ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING | 2020年 / 45卷 / 11期
关键词：
Pressure vessels; Classical laminate theory; Winding angle; Laminate thickness; Fibre content; Tsai-Hill failure criteria; DESIGN;
D O I：
10.1007/s13369-020-04744-8
中图分类号：
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号：
07 ; 0710 ; 09 ;
摘要：
The strength of composite structure is sensitive to the manufacturing variances like fibre orientation angle, thickness of the laminate and the volume fraction of fibre. In the present study, the effect of these parameters on the strength of the composite laminate and the optimum parameters for higher strength were observed using classical laminate theory. The optimum fibre orientation angle was found to be 55 degrees/- 55 degrees. The ideal thickness of the laminate is 0.2 mm and the volume fraction of the fibre in the composite is 0.53. The results of the effect of the fibre orientation angle on the strength obtained were validated using Autodesk Helius composite.
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收藏
页码：9413 / 9421
页数：9
相关论文
共 23 条
[1]   Simulation procedure of high pressure vessels using the wire winding technique [J].
Alegre, J. M. ;
Bravo, P. ;
Preciado, M. ;
Solaguren-Beascoa, M. .
ENGINEERING FAILURE ANALYSIS, 2010, 17 (01) :61-69
[2]   Influence of variable scattering on the optimum winding angle of cylindrical laminated composites [J].
Béakou, A ;
Mohamed, A .
COMPOSITE STRUCTURES, 2001, 53 (03) :287-293
[3]   Structural Integrity Assessment of Filament Wound Composite Pressure Vessel Using Through Transmission Technique [J].
Behera, Sameerkant ;
Sahoo, S. K. ;
Srivastava, Lokesh ;
Gopal, A. S. Srinivasa .
2ND INTERNATIONAL CONFERENCE ON STRUCTURAL INTEGRITY AND EXHIBITION 2018 (SICE 2018), 2019, 14 :112-118
[4]   Optimal design of filament wound truncated cones under axial compression [J].
Cagdas, Izzet U. .
COMPOSITE STRUCTURES, 2017, 170 :250-260
[5]   Orthotropic mechanical properties of fused deposition modelling parts described by classical laminate theory [J].
Casavola, Caterina ;
Cazzato, Alberto ;
Moramarco, Vincenzo ;
Pappalettere, Carmine .
MATERIALS & DESIGN, 2016, 90 :453-458
[6]   Classical laminate theory model for twill weave fabric composites [J].
Chaphalkar, P ;
Kelkar, AD .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2001, 32 (09) :1281-1289
[7]   The effect of fiber volume fraction on filament wound composite pressure vessel strength [J].
Cohen, D ;
Mantell, SC ;
Zhao, LY .
COMPOSITES PART B-ENGINEERING, 2001, 32 (05) :411-427
[8]   The influence of manufacturing variances on the progressive failure of filament wound cylindrical pressure vessels [J].
Ellul, Brian ;
Camilleri, Duncan .
COMPOSITE STRUCTURES, 2015, 133 :853-862
[9]  
Glenn CG, 1992, COMPOSITE MAT TESTIN
[10]   Structural design and experimental investigation on filament wound toroidal pressure vessels [J].
Hu, Haixiao ;
Li, Shuxin ;
Wang, Jihui ;
Zu, Lei .
COMPOSITE STRUCTURES, 2015, 121 :114-120
123