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紫外辅助缠绕玻璃纤维增强树脂基复合材料的制备和力学性能研究

陈晓东 李勇 还大军 王武强 刘丽

南京航空航天大学学报(英文版)2020,Vol.37Issue(3):467-480,14.
南京航空航天大学学报(英文版)2020,Vol.37Issue(3):467-480,14.

紫外辅助缠绕玻璃纤维增强树脂基复合材料的制备和力学性能研究

Preparation and Mechanical Properties of UV-Assisted Filament Winding Glass Fiber Reinforced Polymer-Matrix Composite

陈晓东 1李勇 2还大军 1王武强 1刘丽1

作者信息

  • 1. 南京航空航天大学材料科学与技术学院,南京 211106,中国
  • 2. 南京航空航天大学直升机传动技术重点实验室,南京 210016,中国
  • 折叠

摘要

Abstract

This paper studied the preparation and mechanical properties of glass fiber reinforced polymer-matrix composite rings prepared by filament winding assisted by ultraviolet(UV)curing. A ray-tracing method was used to calculate the penetration ability of UV light in the resin casting,and then a typical composite ring with dual-curing characteristics was prepared by UV-assisted curing. The effects of winding speed and thermal initiator concentration on the distribution of fiber fraction and mechanical properties were studied. Microscopic morphology was used for the observation of the differences in fiber volume fraction. Mechanical properties tests and scanning electron micrographs were performed to investigate the failure and damage mechanisms of the composite ring samples. The ray tracing results indicate that the UV light can pass through a single yarn thickness and the energy transmitted is sufficient to cure the back side quickly. The experimental results show that the mechanical properties of the composite ring prepared in this paper are comparable to those of the heat-cured samples,which is sufficient to meet the requirements of the flywheel.

关键词

玻璃纤维增强复合材料/紫外固化/双重固化树脂/力学性能/纤维体积分数

Key words

glass fiber reinforced polymer (GFRP)/ultraviolet (UV) curing/dual-curable resin/mechanical properties/fiber volume fraction

分类

通用工业技术

引用本文复制引用

陈晓东,李勇,还大军,王武强,刘丽..紫外辅助缠绕玻璃纤维增强树脂基复合材料的制备和力学性能研究[J].南京航空航天大学学报(英文版),2020,37(3):467-480,14.

基金项目

This work was supported by the National Key Laboratory of Science and Technology on Helicopter Transmission(Nanjing University of Aeronautics and Astronautics)(No.HTL-A-20K01),the Pretension and Relaxation Mechanism of Thermoplastic Prepreg Tape Winding with Tension Used to Hi-Speed Permanent Magnet Machine Sleeve(No.51903249),and the Priority Academic Program Development of Jiangsu Higher Education Institutions and the Fundamental Research Funds for the Central Universities. The authors would like to acknowledge the following people for their assistance: CHU Qiyi, ZHANG Xiangyang,LIU Hongquan,LI Lisha,and LUO Rui,all with the National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics. (Nanjing University of Aeronautics and Astronautics)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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