COMPOSITES SCIENCE AND ENGINEERING ›› 2015, Vol. 0 ›› Issue (5): 47-53.

• BASIC STUDY • Previous Articles     Next Articles

INVESTIGATION ON IMPACT PROPERTIES OF 2-D TRIAXIAL HYBRID-BRAID LAMINATED COMPOSITES

WANG Wen-sha1,2, YAN Jian-hua3*, GU Hai-lin4   

  1. 1. Key Lab of Textile Science & Technology, Ministry of Education, Donghua University, Shang 201620, China;
    2. College of Textiles, Donghua University, Shanghai 201620, China;
    3. Research Institute of Donghua University, Donghua University, Shanghai 201620, China;
    4. SAIC Motor Corporation Limited, Shanghai 201600, China
  • Online:2015-05-28 Published:2021-09-13

Abstract: Three types of 2D triaxial carbon/glass hybrid-braid laminated composites with same laminating layers were designed to study the influences of hybrid-braid patterns on low velocity impact properties, providing basis for design and theory for applied reseach in aerospace and other fields. Through comparisons and analysis of low-velocity impact and three point bending experiments, we can conclude that: The composites of glass fiber as braiding yarn and carbon fiber as axial yarn, after low velocity impact, had the least cracks on the surface, the lowest absorbed energy per unit thickness, the minimum damage range in thickness direction, the minimum damage after bending experiment, thus the impact performance of this kind of composite was the best. Through suitable hybrid braiding patterns of carbon fiber/glass fiber combination, the impact properties can be effectively improved to achieve positive hybrid effect, and can enhance the impact performance of hybrid-braid laminated composites.

Key words: 2D triaxial hybrid-braid laminated composites, absorbed energy per unit thickness, low velocity impact properties, bending properties after impact

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