复合材料科学与工程 ›› 2023, Vol. 0 ›› Issue (9): 80-84.DOI: 10.19936/j.cnki.2096-8000.20230928.012

• 应用研究 • 上一篇    下一篇

热处理对CF/PEEK热塑性复合材料变形的影响

王维泽, 刘榕, 于航   

  1. 南京航空航天大学 材料科学与技术学院,南京210006
  • 收稿日期:2022-08-05 出版日期:2023-09-28 发布日期:2023-10-20
  • 作者简介:王维泽(2001—),男,本科,2019级材料科学与工程专业,wswwzws23@nuaa.edu.cn。
  • 基金资助:
    国家级大学生创新创业训练支持项目(202010287060Z)

Effect of heat treatment on deformation of CF/PEEK thermoplastic composites

WANG Weize, LIU Rong, YU Hang   

  1. College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210006, China
  • Received:2022-08-05 Online:2023-09-28 Published:2023-10-20

摘要: 碳纤维增强聚醚醚酮(CF/PEEK)是一种性能优异的热塑性复合材料。CF/PEEK在成型过程中对温度和压力等条件敏感,不同的热处理条件都可能会对零件的变形产生影响。在带弧度的复合材料固化时,层合板间的内应力在脱模时被释放,会造成材料的变形,影响成型件的精度与后期使用。基于热处理工艺对CF/PEEK力学性能的提升,本文聚焦热处理工艺对CF/PEEK变形的影响,设计用于制造曲面零件的原位膜加热设备,利用圆柱形模具加工C形件,探究不同熔融温度以及不同退火温度对材料变形的影响,找出最优工艺曲线,讨论不同退火温度下可能影响变形的因素。研究发现不同熔融温度下零件回弹角在0.325 7~0.473 7之间,退火温度在250 ℃下时零件的变形最小。此研究旨在利用更高效的制造方法,提升复合材料固化后成型件的质量,助力其在航空航天领域中得到更好的应用。

关键词: 热塑性复合材料, 原位膜, 热处理, 变形, C形件

Abstract: Carbon fiber reinforced polyetheretherketone (CF/PEEK) is a thermoplastic composite material with excellent properties. CF/PEEK is sensitive to conditions such as temperature and pressure during the molding process, and different heat treatment conditions can have an impact on the deformation of the part. During the curing of composites with curvature, internal stresses between the laminates are released during demolding, which can cause deformation of the material and affect the accuracy and later use of the molded part. Based on the enhancement of the mechanical properties of CF/PEEK by the heat treatment process, this paper focuses on the effect of the heat treatment process on the deformation of CF/PEEK, designs in-situ film heating equipment for the manufacture of curved parts, uses cylindrical molds to process C-shaped parts, explores the effect of different melting temperatures as well as different annealing temperatures on the deformation of the material, finds the optimal process curve and discusses the factors that may affect the deformation at different annealing temperatures. It was found that the spring-back angle of the parts at different melting temperatures ranged from 0.325 7 to 0.473 7, and the deformation of the parts at an annealing temperature of 250 ℃ was the smallest. This study aims toutilize more efficient manufacturing methods, to improve the quality of the molded parts after curing composite materials and help them to be better used in the aerospace field.

Key words: thermoplastic composite, in-situ membrane, heat treatment, deformation, C-shaped

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