Study of the Fatigue Behavior of the Unidirectional Zylon/epoxy Composite Used in Pulsed Magnets

被引:6
|
作者
Peng, Tao [1 ]
Wang, Shuang [1 ]
Huang, Y. D. [1 ]
Jiang, Fan [1 ]
Sun, Quqin [1 ]
Li, Liang [1 ]
Xiao, Houxiu [1 ]
机构
[1] Wuhan Natl High Magnet Field Ctr, State Key Lab Adv Electromagnet Engn & Technol, Wuhan 430074, Peoples R China
基金
中国国家自然科学基金;
关键词
Damage evolution; fatigue; mechanical properties; zylon/epoxy; MECHANICAL-PROPERTIES; RESIDUAL STIFFNESS; LIFE PREDICTION; FIBER; STRENGTH; DAMAGE; PERFORMANCE; FLAX/EPOXY; CONDUCTORS; MODEL;
D O I
10.1109/TASC.2020.2976946
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The fatigue behavior of the Zylon/epoxy composite has been tested under quasi-static tensile and tensile fatigue loads. The distribution of the fatigue life at different stress was determined. The results show that the statistical characteristic of the static strength and the fatigue life can be satisfactorily described by the normal, lognormal or Weibull distribution model. The measured S-N curve exhibits a pronounced nonlinear behavior. Strains of the unidirectional specimens were monitored with a mechanical extensometer during the test. Three distinct stages of the strain evolutionary process were observed. The evolution curves show a sharp increase in the first stage, an approximately linear slow increasing in the middle stage and an unstable acceleration in the third stage before failure. Similar to the strain evolution, the three-stage stiffness of degradation was also observed. The maximal cycle strain is chosen as the indicator of damage evaluation. The experimental data of the damage parameters are fitted with the existing analytical model. The presented models have a good agreement with the tested results.
引用
收藏
页数:5
相关论文
共 50 条
  • [11] Tension-tension fatigue behavior of unidirectional single-walled carbon nanotube reinforced epoxy composite
    Ren, Y
    Li, F
    Cheng, HM
    Liao, K
    CARBON, 2003, 41 (11) : 2177 - 2179
  • [12] An Experimental Study of the Routing of a Unidirectional Carbon/Epoxy Composite
    Turki, Yosra
    Habak, Malek
    Velasco, RaphaeL
    Vantomme, Pascal
    Khellil, Kamel
    14TH INTERNATIONAL CONFERENCE ON MATERIAL FORMING ESAFORM, 2011 PROCEEDINGS, 2011, 1353 : 1013 - 1018
  • [13] Delamination Growth In Unidirectional Glass/Epoxy Composite Under Static And Fatigue Loads
    Kenane, M.
    PROCEEDINGS OF THE JMSM 2008 CONFERENCE, 2009, 2 (03): : 1195 - 1203
  • [14] Fatigue Properties of Cu-Nb Conductor Used for Pulsed Magnets at the WHMFC
    Sun, Q. Q.
    Liang, L.
    Jiang, F.
    Xiao, H. X.
    Peng, T.
    IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 2014, 24 (03)
  • [15] VISCOELASTIC STUDY OF CARBON EPOXY UNIDIRECTIONAL COMPOSITE-MATERIALS
    PERRET, P
    GERARD, JF
    CHABERT, B
    MAKROMOLEKULARE CHEMIE-MACROMOLECULAR SYMPOSIA, 1989, 23 : 139 - 147
  • [16] Study of translaminar fracture toughness of unidirectional flax/epoxy composite
    Saadati, Yousef
    Lebrun, Gilbert
    Bouvet, Christophe
    Chatelain, Jean-Francois
    Beauchamp, Yves
    COMPOSITES PART C: OPEN ACCESS, 2020, 1
  • [17] EFFECT OF STRESS RATIO ON THE FATIGUE OF UNIDIRECTIONAL GLASS-FIBER EPOXY COMPOSITE LAMINAE
    ELKADI, H
    ELLYIN, F
    COMPOSITES, 1994, 25 (10): : 917 - 924
  • [18] Multiaxial failure behavior and fatigue life prediction of unidirectional composite laminates
    Lian, Yuhao
    Wu, Fuqiang
    Zhao, Qijun
    Han, Yalin
    Wang, Bin
    COMPOSITES SCIENCE AND TECHNOLOGY, 2024, 247
  • [19] Evaluation of the fill yarns effect on the out-of-plane compressive fatigue behavior for an unidirectional glass fiber reinforced epoxy composite
    Juan, Victor San
    Fernandez, Eduardo
    Pincheira, Gonzalo
    Melendrez, Manuel
    Flores, Paulo
    COMPOSITE STRUCTURES, 2016, 138 : 237 - 242
  • [20] Comparative Study on the Fatigue Behavior of Jute-Wool Felt/Epoxy Hybrid and Glass Fiber/Epoxy Composite
    Thilakan, Sanjay
    Mathivanan, N. Rajesh
    SAE INTERNATIONAL JOURNAL OF MATERIALS AND MANUFACTURING, 2023, 16 (04) : 343 - 353