玻璃钢/复合材料 ›› 2018, Vol. 0 ›› Issue (9): 98-101.

• 应用研究 • 上一篇    下一篇

预浸料变形性能参数的测量方法研究

李妍, 原崇新, 李永行, 蔡志强   

  1. 中国商飞北京民用飞机技术研究中心,北京102211
  • 收稿日期:2018-02-11 出版日期:2018-09-28 发布日期:2018-09-28
  • 作者简介:李妍(1984-),女,硕士,工程师,主要从事树脂基复合材料方面的研究,liyan1@comac.cc。

A MEASUREMENT METHOD RESEARCH ON DEFORMATION PROPERTY OF PREPREG

LI Yan, YUAN Chong-xin, LI Yong-hang, CAI Zhi-qiang   

  1. Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, China
  • Received:2018-02-11 Online:2018-09-28 Published:2018-09-28

摘要: 复合材料设计软件中预浸料等材料的性能参数大部分可从供应商处获得,但缺少影响制造可行性模拟的材料变形性能参数——预警角度(warning angle)和极限角度(limit angle)。预警角度和极限角度的大小将直接影响软件中纤维变形模拟结果的真实性,并影响无褶皱铺放的制造要求。对预浸料的预警角度和极限角度测量原理进行研究,分析并验证了预警角度和极限角度测量方法的可行性,将测量结果输入FiberSIM中,对吊挂前缘模具的预浸料铺放变形性进行模拟仿真,并将模拟结果同实际铺贴效果进行比较,结果一致,褶皱变形位置及变形尺寸准确无误。结果表明,本文提出的预浸料变形性能的测量及验证方法对复合材料制备过程的铺放模拟和铺层设计具有重要的指导意义。

关键词: 复合材料, 预警角度, 极限角度, 制造可行性模拟

Abstract: Software is very popular in composite design and manufacturing field, which could increase efficiency and reduce costs. During design and layup process, software needs a lot of material property parameters. Most of them can be obtained from suppliers, but warning angle and limit angle are not provided by suppliers. They are usually set according to engineering experience, which are not accurate. The two values are important to predict producibility with software during the design and manufacturing process. This paper is aimed to find an approach to measure the values of warning angle and limit angle of composite lamina. A novel approach of flat model was developed to measure the warning angle and limit angle as the initial values, and then the values were corrected by spare model. After several iterations, warning angle is 9.8° and limit angle is 19.6°, which are the best results for the material. A practical layup on pylon model was conducted to verify the warning angle and limit angle values. The results show that the practical deformation is close to the simulation, which indicates that the measurement method of the warning angle and the limit angle is reliable. In conclusion, the method could solve the layup problems during composite processing, and can be a guidance for layup simulation and laminate design.

Key words: composite, limit angle, warning angle, producibility

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