Study on voids of epoxy matrix composites sandwich structure parts

17th IUMRS International Conference in Asia

He, Simin^1 ; Wen, Youyi^1 ; Yu, Wenjun^1 ; Liu, Hong^1 ; Yue, Cheng^1 ; Bao, Jing^1

AVIC Chengdu Aircraft Industry (Group) Co. Ltd., Chengdu

610091, China^1

关键词: Carbon fiber reinforced epoxy resin;    Compaction pressure;    Composites laminates;    Epoxy-matrix composite;    Manufacturing process;    Manufacturing process parameters;    Non-destructive measurement;    Ultrasonic measurement methods;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/182/1/012031/pdf
DOI  :  10.1088/1757-899X/182/1/012031

来源: IOP

【 摘 要 】

Void is the most common tiny defect of composite materials. Porosity is closely related to composite structure property. The voids forming behaviour in the composites sandwich structural parts with the carbon fiber reinforced epoxy resin skins was researched by adjusting the manufacturing process parameters. The composites laminate with different porosities were prepared with the different process parameter. The ultrasonic non-destructive measurement method for the porosity was developed and verified through microscopic examination. The analysis results show that compaction pressure during the manufacturing process had influence on the porosity in the laminate area. Increasing the compaction pressure and compaction time will reduce the porosity of the laminates. The bond-line between honeycomb core and carbon fiber reinforced epoxy resin skins were also analyzed through microscopic examination. The mechanical properties of sandwich structure composites were studied. The optimization process parameters and porosity ultrasonic measurement method for composites sandwich structure have been applied to the production of the composite parts.