首页|三维角联锁机织复合材料的制备及其弯曲压缩失效机制

三维角联锁机织复合材料的制备及其弯曲压缩失效机制

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为掌握三维纺织结构复合材料在准静态下的失效机制,以碳纤维角联锁预制体为增强体,环氧树脂为基体,采用树脂传递模塑成型工艺制备三维角联锁机织复合材料,并对试样进行匀速载荷下的三点弯曲和压缩试验.采用X射线计算机断层扫描技术观测材料内部结构的损伤情况,并分析材料的失效机制.结果表明:三维角联锁机织复合材料的弯曲强度达到136.43 MPa,弹性模量接近20 GPa,材料的抗弯曲性能优异;基体开裂、下表面纤维断裂和分层是材料的主要弯曲失效模式;材料沿厚度方向的压缩应力达到266.17 MPa,具有良好的抗压缩性能;当承受压缩载荷时,材料在厚度方向上的主要破坏机制表现为剪切破坏.
Preparation and bending compression failure mechanism of three-dimensional angle interlock woven composites
Objective Three-dimensional(3-D)woven fabric is an fabric structure wherein the upper and lower layers of fabric are interconnected using warp or weft yarns to form an angle interlock structure.Due to their exceptional mechanical properties,3-D woven composites have gained increasingly popularity in aerospace and military applications.While most research has focused on the failure mechanism of angle interlock woven composite(AIWC)under dynamic load,it is crucial to also consider the various loads that AIWCs endure in practical engineering applications,partications in quasi-static environments.Although the quasi-static load is implicit,the damage and failure resulting from such load cansignificantly impact materials safety,underscoring the importance of studying the mechanical properties of AIWCs in quasi-static environments.Method In this study,3-D woven composites were prepared using the vacuum assisted resin transfer molding(VARTM)technique.Subsequently,their bending and compression properties were investigated through three-point bending and compression experiments.X-ray computed tomography(XR-CT)technology was employed to observe microstructural damage profiles and analyze the failure mechanism of the material.Results In the three-point bending test,the maximum load on the 3-D woven composites reached 1 108.3 N,the bending strength reached 136.43 MPa,and the bending modulus was close to 20 GPa.The primary failure modes of the material included resin compression fracture on the upper and lower surfaces,fiber layer delamination,and warp yarn tension fracture on the lower surface.In terms of compression resistance in the thickness direction,the 3-D woven composites exhibited favorable pefformance.Under compression load,the material experienced significant shear failure along the 45° direction in the thickness,accompanied by resin fragmentation and wavy delamination in both longitudinal and latitudinal directions.Additionally,compression expansion was observed in the latitudinal section.These phenomena were attributed to the appearance of the shear band,resulting in relative slippage of the resin near the shear band and higher shear loads on the straight weft yarns.The bending sections of the warp and straight weft yarns experienced compression against each other.Ultimately,when the yarns reached their extreme limits,the warp and weft yarn fractured,leading to material failure.Conclusion In conclusion,this study successfully prepared 3-D woven composites using the VARTM technique.The three-point bending test demonstrated that the bending strength of 3-D angle interlocking woven composites reached 136.43 MPa,with a bending modulus close to 20 GPa,indicating excellent bending performance.The main failure modes of the material were matrix cracking,fiber fracture on the lower surfaces,and delamination.The material exhibited good compression resistance in the thickness direction,with a compressive stress reaching 266.17 MPa.The primary failure mechanism in the thickness direction under compression loads was shear failure.In the investigation of the mechanical properties of 3-D woven composites,several aspects require further observation.Firstly,since the material is composed of different warp and weft yarns,it is crucial to study its mechanical properties in different directions.Additionally,apart from the experimental process,the accuracy of the experiments can be verified through finite element simulations and comparison with experimental results.

angle interlock structurecompositeangle interlock woven compositecarbon fiberbending propertycompression propertyfailure mechanism

李天宇、沈伟、陈立峰、竺铝涛

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浙江理工大学纺织科学与工程学院(国际丝绸学院),浙江杭州 310018

绍兴宝旌复合材料有限公司,浙江绍兴 312000

浙江理工大学桐乡研究院有限公司,浙江嘉兴 314599

角联锁结构 复合材料 角联锁机织复合材料 碳纤维 弯曲性能 压缩性能 失效机制

浙江省基础公益研究计划项目浙江省"尖兵"研发攻关计划项目浙江理工大学桐乡研究院有限公司开放基金类项目

LGG21E0500252023C01097TYY202302

2024

纺织学报
中国纺织工程学会

纺织学报

CSTPCD北大核心
影响因子:0.699
ISSN:0253-9721
年,卷(期):2024.45(8)