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碳纤维复合材料编织-针刺预制体成形质量研究

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编织-针刺复合成形技术可实现大厚度回转形复合材料预制体一体化成形.为研究编织-针刺复合材料预制体成形质量,试制了不同K数纱线、编织角度的编织-针刺预制体以及作为对照组的机织-针刺预制体.考虑背面针刺纤维束形貌以及基布损伤提出通过用预制体纤维束细长率χf 定量表征针刺纤维束形貌.结合实际针刺预制体剥离曲线的变化特点,采用有效剥离曲线内所有波峰和波谷的平均值来对层间剥离强力进行描述.结果表明,试样纱线K数为6K时,编织-针刺预制体平均细长率相较机织-针刺预制体提升7.2%,编织-针刺预制体纤维束形貌更理想.当纱线K数由 6 增加至 12 时,机织-针刺预制体背面纤维束平均细长率提升了78.9%,编织-针刺预制体却减少了 30.6%,其原因在于编织-针刺预制体刺针作用位置处纱线被挤开,增大了纤维束投影面积.编织-针刺预制体在层间剥离强力指标方面优势显著,各试样相较机织-针刺预制体提升 38.0%以上,12K纱线编织-针刺预制体层间剥离强力比 6K纱线大78.3%,且随着编织角由30°增加至60°,编织-针刺预制体平均剥离强力减少46.6%.
Study on the Forming Quality of Carbon Fiber Composite Braided-punched Preforms
The braided-punched composite forming technology can achieve the integrated forming of large thickness rotary-shaped composite preforms.To investigate the forming quality of braided-punched composite mate-rial preforms with different yarn K-numbers and braiding angles,as well as woven-punched performs as a control group,were experimentally produced.The morphology of the backside punched fiber bundles and the damage to the base fabric were considered,and the preform fiber bundles elongation χf was proposed to quantitatively charac-terize the punched fiber bundle morphology.By combining the actual changes in the peeling curve of the punched preforms,the average values of all peaks and troughs within the effective peeling curve were used to describe the interlaminar peeling force.The results show that when the yarn K-number is 6K,the average elongation of the brai-ded-punched preforms is increased by 7.2%compared to the woven-punched preforms,making the fiber bun-dle morphology of the braided-punched preforms more ideal.When the yarn K-number increases from 6 to 12,the average elongation of the fiber bundles on the back of the woven-punched preforms increases by 78.9%.In com-parison,that of the braided-punched preforms decreases by 30.6%due to the yarn being displaced at the punching site,increasing the fiber bundle's projected area.The braided-punched preforms show significant ad-vantages in interlaminar peeling force,with each sample showing an increase of over 38.0%compared to the wov-en-punched preforms.The interlaminar peeling strength of the 12K yarn braided-punched preforms is 78.3%greater than that of the 6K yarn.As the braiding angle increases from 30° to 60°,the average peeling strength of the braided-punched preforms decreases by 46.6%.

compositesbraided-punched preformsforming qualitypreform characterization

周征西、单忠德、孙正、郭子桐、杨天政

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南京航空航天大学 机电学院,南京 210016

南京航空航天大学 航空航天结构力学及控制全国重点实验室,南京 210016

复合材料 编织-针刺预制体 成形质量 预制体性能表征

江苏省前沿引领技术基础研究专项项目中国国家自然青年科学基金中国博士后面上基金中国博士后特助基金

BK2021200752305376YBA23044YBA23031

2024

高科技纤维与应用
北京华腾东光科技发展有限公司 全国特种合成纤维信息中心

高科技纤维与应用

CSTPCD
影响因子:0.571
ISSN:1007-9815
年,卷(期):2024.49(3)