复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (10): 123-132.DOI: 10.19936/j.cnki.2096-8000.20251028.018

• 航空复合材料 • 上一篇    

航空复合材料机身Z形隔框辊压预成型缺陷的影响因素研究

孙道萍1,2, 岳广全2, 刘卫平2,3*, 李哲夫3, 宋清华3, 卢鑫4   

  1. 1.东华大学 先进纤维材料全国重点实验室 材料科学与工程学院,上海 201620;
    2.东华大学 民用航空复合材料协同创新中心,上海 201620;
    3.上海飞机制造有限公司,上海 201324;
    4.常州市新创智能科技有限公司,常州 213001
  • 收稿日期:2024-12-23 出版日期:2025-10-28 发布日期:2025-12-02
  • 通讯作者: 刘卫平(1963—),男,博士,研究员,博士生导师,研究方向为先进航空复合材料制造,liuweiping@comac.cc。
  • 作者简介:孙道萍(1998—),女,硕士研究生,研究方向为复合材料成型加工。

Study on the influencing factors of Z-shaped partition frame roll forming defects in aviation composite fuselage

SUN Daoping1,2, YUE Guangquan2, LIU Weiping2,3*, LI Zhefu3, SONG Qinghua3, LU Xin4   

  1. 1. College of Materials Science and Engineering, State Key Laboratory of Advanced Fiber Materials, Donghua University, Shanghai 201620, China;
    2. Center for Civil Aviation Composites, Donghua University, Shanghai 201620, China;
    3. Shanghai Aircraft Manufacturing Co., Ltd., Shanghai 201324, China;
    4. Changzhou Newtry Aviation Technology Co., Ltd., Changzhou 213001, China
  • Received:2024-12-23 Online:2025-10-28 Published:2025-12-02

摘要: 本文采用复合材料辊压自动化成型技术制备了含有曲率且结构复杂的机身Z形隔框零件,但在辊压成型过程中预浸料受到复杂的热/力作用,导致隔框出现面内屈曲或面外褶皱等缺陷。针对此类缺陷,本文对不同工艺参数和结构参数进行理论分析及工艺试验研究,通过缺陷观察与表征讨论了温度、速度和铺层结构对缺陷形成的影响。温度影响预浸料中树脂的状态,从而影响滑移机制的变化,导致缺陷产生;速度决定了预浸料发生结构响应的充分性;铺层的变化使得层间剪切、层间滑移和摩擦等作用随之发生改变,进而影响褶皱等缺陷的产生。结果表明:在温度为50 ℃、速度为50 mm/min时,隔框辊压预成型效果最好,本文的研究成果可为辊压预成型过程的参数优化提供理论指导。

关键词: Z形隔框, 辊压, 预成型, 褶皱, 工艺参数, 结构参数, 复合材料

Abstract: In this paper, Z-shaped frame parts with curvature and complex structure were prepared by the automatic roll forming technology of composite materials. However, during the roll forming process, the prepreg is subjected to complex thermal/mechanical effects, resulting in defects such as in-plane buckling or out of plane wrinkles in the frame. In this paper, different process parameters and structure parameters were analyzed theoretically and studied experimentally. The effects of temperature, speed and lay-up structure on the formation of defects were discussed through defect observation and characterization. The temperature affects the state of the resin in the prepreg, which affects the change of the slip mechanism and leads to the defects. The velocity determines the sufficiency of structural response of prepreg. The change of layering changes the interlayer shear, interlayer slip and friction, and then affects the generation of defects such as wrinkles. The results show that the best roller preforming effect is achieved at the temperature of 50 ℃ and the speed of 50 mm/min. The research results in this paper can provide theoretical guidance for parameter optimization of roller preforming process.

Key words: Z-shaped frame, roll forming, preforming, wrinkles, process parameters, structural parameter, composites

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