Intrinsic Safety Factors for Glass & Carbon Fibre Composite Filament Wound Structures

被引:0
|
作者
A. R. Bunsell
A. Thionnet
H. Y. Chou
机构
[1] Mines ParisTech,
[2] Université de Bourgogne,undefined
来源
关键词
Reliability; Modelling; Fibre failure; Intrinsic limiting properties;
D O I
暂无
中图分类号
学科分类号
摘要
The determination of intrinsic safety factors for glass and carbon fibre unidirectional composites and filament wound internally pressurised structures, is described. In such structures the fibres are placed on geodesic paths and the pressure induces tensile forces in them. The fibres ensure the strength of the composite and must break for it to fail. Failure is seen in such structures, to depend mainly on the accumulation of fibre breaks. These are initially randomly distributed but become critical when clusters of breaks develop. Long term behaviour of carbon fibre composites is controlled by the viscoelastic relaxation of the matrix around breaks, which can lead to further delayed fibre breaks. Failure in glass fibre structures can additionally be induced by stress corrosion of the glass fibres. This process does not seem to occur with carbon fibres and as the latter are increasingly used in critical structures emphasis is given to them. Until the development of clusters of fibre breaks, in a filament wound structure, no macroscopic changes in the composite behaviour are evident so that failure occurs in a sudden death manner. Multi-scale simulation, taking into account the characteristics of the composite components and scaling up their behaviour under load, accurately describes the overall behaviour of the composite structure. This approach not only allows the behaviour to be described, as a function of time, but also calculates the scatter which will occur in the behaviour of the structure. This allows the intrinsic safety factors of the composite structure to be quantified.
引用
收藏
页码:107 / 121
页数:14
相关论文
共 50 条
  • [31] EFFECTS OF BAND WEAVING ON FIBER STRENGTH IN FILAMENT-WOUND COMPOSITE STRUCTURES
    GRAMOLL, K
    RAMAPRASAD, S
    COMPOSITES ENGINEERING, 1995, 5 (04): : 363 - 373
  • [32] Structural integrity of filament wound composite structures with embedded fiber optic sensors
    Foedinger, R
    Sirkis, J
    Chang, CC
    Vandiver, TL
    EVOLVING TECHNOLOGIES FOR THE COMPETITIVE EDGE, BOOKS 1 AND 2, 1997, 42 : 368 - 379
  • [33] Effect of carbon black nanoparticle intrinsic properties on the self-monitoring performance of glass fibre reinforced composite rods
    Nanni, Francesca
    Ruscito, Giovanni
    Puglia, Debora
    Terenzi, Andrea
    Kenny, J. M.
    Gusmano, Gualtiero
    COMPOSITES SCIENCE AND TECHNOLOGY, 2011, 71 (01) : 1 - 8
  • [34] Inhalation and deposition of carbon and glass composite fibre in the respiratory airway
    Inthavong, Kiao
    Mouritz, Adrian P.
    Dong, Jingliang
    Tu, Ji Yuan
    JOURNAL OF AEROSOL SCIENCE, 2013, 65 : 58 - 68
  • [35] Inhalation and deposition of carbon and glass composite fibre in the respiratory airway
    Tu, J.Y. (jiyuan.tu@rmit.edu.au), 1600, Elsevier Ltd (65):
  • [36] Moisture-induced degradation of glass/epoxy filament-wound composite tubes
    Chiou, PL
    Bradley, WL
    JOURNAL OF THERMOPLASTIC COMPOSITE MATERIALS, 1996, 9 (02) : 118 - 128
  • [37] Hoop tensile strength testing of glass/jute hybrid filament wound composite tubes
    Shrigandhi, Ganesh D.
    Kothavale, Basavaraj S.
    INTERNATIONAL JOURNAL OF INTERACTIVE DESIGN AND MANUFACTURING - IJIDEM, 2025, 19 (04): : 2659 - 2669
  • [38] Carbon/epoxy filament wound composite drive shafts under torsion and compression
    Filho, Paulo Stedile
    Almeida, Jose Humberto S., Jr.
    Amico, Sandro C.
    JOURNAL OF COMPOSITE MATERIALS, 2018, 52 (08) : 1103 - 1111
  • [39] Evaluating the effectiveness of nanofillers in filament wound carbon/epoxy multiscale composite pipes
    Ustun, Tugay
    Ulus, Hasan
    Karabulut, Salim Egemen
    Eskizeybek, Volkan
    Sahin, Omer Sinan
    Avci, Ahmet
    Demir, Okan
    COMPOSITES PART B-ENGINEERING, 2016, 96 : 1 - 6
  • [40] Experimental Evaluation of Strength Degradation Temperature for Carbon Epoxy Filament Wound Composite
    Mishra, Jai Krishna
    Rao, Surya Prakash
    Bose, Subhash Chandra
    Nath, Kishore N.
    Golla, Rama Rao
    INTERNATIONAL JOURNAL OF AVIATION AERONAUTICS AND AEROSPACE, 2020, 7 (04): : 1 - 18