1. 西北工业大学,西安,710072
2. 中国航发贵阳发动机设计研究所,贵阳,550081
3. 西安理工大学,西安,710048
纸质出版:2021
移动端阅览
严斌,陈汉元,周举,代悦,刘维伟 . 半厚度Z–pin植入对层合板弯曲性能的影响研究[J]. 航空制造技术, 2021, 64(22): 97-. YAN Bin, CHEN Hanyuan, ZHOU Ju, DAI Yue, LIU Weiwei . Effect of Half Thickness Z–pin Implantation on Flexural Properties of Laminates. 航空制造技术, 2021, 64(22): 97-.
YAN Bin, CHEN Hanyuan, ZHOU Ju, et al. Effect of Half Thickness Z–pin Implantation on Flexural Properties of Laminates[J]. Aeronautical Manufacturing Technology, 2021, 64(22).
严斌,陈汉元,周举,代悦,刘维伟 . 半厚度Z–pin植入对层合板弯曲性能的影响研究[J]. 航空制造技术, 2021, 64(22): 97-. YAN Bin, CHEN Hanyuan, ZHOU Ju, DAI Yue, LIU Weiwei . Effect of Half Thickness Z–pin Implantation on Flexural Properties of Laminates. 航空制造技术, 2021, 64(22): 97-. DOI: 10.16080/j.issn1671-833x.2021.22.097.
YAN Bin, CHEN Hanyuan, ZHOU Ju, et al. Effect of Half Thickness Z–pin Implantation on Flexural Properties of Laminates[J]. Aeronautical Manufacturing Technology, 2021, 64(22). DOI: 10.16080/j.issn1671-833x.2021.22.097.
通过三点弯曲试验研究了 Z–pin 在半厚度植入条件下其材质、直径和加捻状态对 Z–pin 增强复合材料层合板弯曲性能的影响。结果表明,采用 Z–pin 半厚度植入工艺相比于未增强对照组试件,增强组试件的弯曲强度、弯曲模量及弯曲应变能都有所提升。Z–pin 材质、直径和加捻状态对试件弯曲强度、模量和弯曲应变能的影响甚微,究其原因为增强组试件界面 X、Y 处潜在的分层缺陷扩展严重,分层损伤主导了弯曲过程中试件的破坏。但 Z–pin 直径对层合板的失效模式有着重要影响,表现为小直径 Z–pin 增强试件分层裂纹扩展较为严重,但萌生裂纹数量较少,试件损伤多表现为受单一裂纹控制;大直径 Z–pin 增强试件裂纹扩展相对一般,但萌生裂纹数量较多,试件多表现为多重裂纹的损伤。
The effects of material
diameter and twisting state of Z–pin on the bending properties of Z–pin reinforced composite laminates were studied by three-point bending test. The results show that the flexural strength
flexural modulus and flexural strain energy of the reinforced laminates with Z–pin half thickness implantation process are significantly improved compared with the control group. The material
diameter and twisting state of Z–pin have little effect on the flexural strength
modulus and strain energy of the specimens. The reason is that the potential delamination defects at the interface X and Y of the reinforcement group expand seriously
and the delamination damage dominates the failure of the specimen in the bending process. However
the Z–pin diameter has an important influence on the failure mode of laminates. The results show that the delamination crack propagation of small diameter Z–pin reinforced specimens is serious
but the number of initiation cracks is small. The damage of specimens is mostly controlled by a single crack. The crack growth of large-diameter Z–pin reinforced specimens is relatively common
but the number of initiation cracks is more
and the specimens are mostly multi crack damaged.
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