Mechanical properties and failure mechanisms of 3D layer-to-layer interlock woven composites

被引:0
|
作者
Wei, Jiahui [1 ,2 ]
Zhang, Yifan [1 ,2 ]
Feng, Jiading [1 ,2 ]
Guo, Qiwei [3 ]
Zou, Qi [4 ]
Shi, Dongjie [5 ]
Zhang, Daijun [4 ]
Wu, Xiaojia [1 ,2 ]
Sun, Zheng [6 ]
Guo, Junhua [7 ]
Jiao, Yanan [1 ,2 ]
Chen, Li [1 ,2 ]
机构
[1] Tiangong Univ, Minist Educ, Key Lab Adv Text Composite Mat, Tianjin 300387, Peoples R China
[2] Tiangong Univ, Sch Text Sci & Engn, Tianjin, Peoples R China
[3] Tianjin Normal Univ, Coll Fine Arts & Design, Tianjin, Peoples R China
[4] AECC Beijing Inst Aeronaut Mat, Beijing, Peoples R China
[5] Natl SuperComp Ctr Tianjin, Tianjin, Peoples R China
[6] Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing, Peoples R China
[7] Jiangsu Univ Sci & Technol, Sch Energy & Power, Zhenjiang, Peoples R China
关键词
fabric structure; failure mechanisms; layer-to-layer interlock; mechanical properties; woven composite; TENSILE PROPERTIES; ORTHOGONAL WEAVE; BEHAVIOR; DAMAGE; PREFORMS;
D O I
10.1002/pc.29312
中图分类号
TB33 [复合材料];
学科分类号
摘要
Three-dimensional layer-to-layer interlock woven composites (3D LTLIWCs) have been widely used in various aero-engine blade models because of their excellent near-net forming capabilities for complex components, as well as significant advantages in structural design flexibility and high damage tolerance. In this paper, a typical and two new 3D LTLIWCs, specifically including 1/3 twill (S-I), modified satin (S-II), and stuffer twill (S-III), were manufactured by two design methods: varying interweaving frequency and introducing stuffer yarns. Three-point bending and uniaxial tensile tests were conducted along the 0 degrees (warp) and 90 degrees (weft) directions. The damage morphology and failure mechanism of the specimens were revealed by nondestructive testing technology and topological structure analysis. The results showed that the fabric structure significantly influenced the mechanical properties and failure mechanisms of the 3D LTLIWCs. Compared with S-I and S-II, S-III demonstrated a 17.9%-80.2% increase in bending strength and a 35.3%-162.8% increase in tensile strength in the 0 degrees direction, while the bending strength and tensile strength in the 90 degrees direction increased by 1.1%-73.3% and 9.3%-50.4%, respectively. Notably, S-III exhibited lower bending and tensile damage in the 0 degrees direction than S-I and S-II, with a smaller propagation range of resin and interface cracks and less severe shear fracture of the load-bearing yarns. This study can provide a useful reference for the optimal design of fabric structure for 3D woven composite blades.Highlights Two design schemes for optimizing 3D LTLI fabric structure were compared. Introducing stuffer yarns improved the mechanical properties of 3D LTLIWCs. S-III composites exhibited the highest failure strength in all test directions. Full-field strain distribution was closely related to the interlocking patterns. Fabric structures had a great influence on the failure modes of 3D LTLIWCs.
引用
收藏
页数:19
相关论文
共 50 条
  • [1] Design strategy for 3D layer-to-layer angle interlock woven composites
    Sitnikova, Elena
    Xu, Mingming
    Kong, Weiyi
    Hu, Shoufeng
    Li, Shuguang
    MATERIALS & DESIGN, 2024, 247
  • [2] Thermo-mechanical responses of notched layer-to-layer 3D angle-interlock woven composites
    Song, Jian
    Liu, Lu
    Li, Lixiao
    Zhou, Haijun
    Zhou, Wenzhao
    Li, Xiang
    Wen, Weidong
    COMPOSITES PART B-ENGINEERING, 2019, 176
  • [3] 3D layer-to-layer orthogonal interlock woven composites under monotonic loading: Multiscale modeling
    Muthukumar, M.
    Prasath, J.
    Sathish, S.
    Ravikumar, G.
    Desai, Y. M.
    Naik, N. K.
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2017, 36 (17) : 1263 - 1285
  • [4] Experimental Investigation of Damage Process in Layer-to-layer Interlock 3D Woven Composites under Uniaxial Tension
    Yu, Tianhong
    Li, Shuguang
    PROCEEDINGS OF THE SECOND INTERNATIONAL CONFERENCE ON MECHANICS, MATERIALS AND STRUCTURAL ENGINEERING (ICMMSE 2017), 2017, 102 : 319 - 324
  • [5] Layer-to-Layer Angle Interlock 3D Woven Bandstop Frequency Selective Surface
    Alonso-Gonzalez, Leticia
    Ver-Hoeye, Samuel
    Fernandez-Garcia, Miguel
    Las-Heras, Fernando
    PROGRESS IN ELECTROMAGNETICS RESEARCH-PIER, 2018, 162 : 81 - 94
  • [6] Understanding the damage mechanisms in 3D layer-to-layer woven composites from thermal and acoustic measurements
    Navratil, Libor
    Le Saux, Vincent
    Marco, Yann
    Aboura, Zoheir
    Harizi, Walid
    Cuniberti, Clement
    Carrere, Nicolas
    Leclercq, Sylvain
    JOURNAL OF COMPOSITE MATERIALS, 2022, 56 (10) : 1559 - 1575
  • [7] Geometrical model of 3D layer-to-layer angle-interlock woven preforms with oblique structure
    Huang, Zhaohua
    Ma, Wensuo
    Jia, Chenhui
    Lei, Xianqing
    Zhang, Zhuangya
    MATERIALS RESEARCH EXPRESS, 2022, 9 (09)
  • [8] Structural and laminar damage mechanisms in layer-to-layer orthogonal angle-interlock woven fabrics and composites
    Jia X.
    Zhuang Y.
    Tang Y.
    Li S.
    Shi W.
    Zhang L.
    Liu M.
    Zhou J.
    Fangzhi Xuebao/Journal of Textile Research, 2022, 43 (07): : 81 - 89
  • [9] Infrared Image Processing to Guide the Identification of Damage and Dissipative Mechanisms in 3D Layer-to-Layer Woven Composites
    Libor Navrátil
    Vincent Le Saux
    Sylvain Leclercq
    Nicolas Carrere
    Yann Marco
    Applied Composite Materials, 2022, 29 : 1449 - 1477
  • [10] Tension-tension fatigue behavior of layer-to-layer 3-D angle-interlock woven composites
    Jin, Limin
    Jin, Bo Cheng
    Kar, Nikhil
    Nutt, Steven
    Sun, Baozhong
    Gu, Bohong
    MATERIALS CHEMISTRY AND PHYSICS, 2013, 140 (01) : 183 - 190