玻璃钢/复合材料 ›› 2018, Vol. 0 ›› Issue (3): 5-12.

• 基础研究 •    下一篇

大张力缠绕碳纤维复合材料高速飞轮转子研究

惠鹏,祖磊*,李书欣,汪洋   

  1. 武汉理工大学材料科学与工程学院,武汉430070
  • 收稿日期:2017-08-23 出版日期:2018-03-20 发布日期:2018-03-20
  • 通讯作者: 祖磊(1983-),男,博士,教授,主要从事复合材料方面的研究,zulei@whut.edu.cn。
  • 作者简介:惠鹏(1993-),男,硕士研究生,主要从事复合材料方面的研究。
  • 基金资助:
    国家自然科学基金(11302168);湖北省自然科学基金(2014CFB140);中央高校基本科研业务费专项资金资助项目(143101001)

RESEARCH ON CARBON FIBER COMPOSITE HIGH SPEED FLYWHEEL ROTOR IN LARGE TENSION WINDING

HUI Peng, ZU Lei*, LI Shu-xin, WANG Yang   

  1. School of Materials Science and Engineering, Wuhan University of Technology, Wuhan 430070, China
  • Received:2017-08-23 Online:2018-03-20 Published:2018-03-20

摘要: 碳纤维复合材料由于其较高的比强度、比刚度以及不产生高频涡流损耗等特点,日益广泛地被用来制造高速飞轮转子护套。另外,大张力缠绕相比压装等工艺更适用于施加碳纤维复合材料层与金属轮毂间的过盈配合。研究了大张力缠绕复合材料飞轮转子护套的设计与成型工艺,建立了复合材料护套的三维有限元模型,采用温差法模拟纤维缠绕张力,采用单元生死法模拟逐层缠绕及固化过程。在30000 RPM的转速及不同工作温度下,分析了缠绕张力及轮毂和转轴间过盈量对转子各材料界面处压应力的影响规律。此外,采用大张力缠绕工艺制备了高速飞轮转子碳纤维护套样件,测试了样件护套对金属轮毂的径向压应力以及轮毂径向应变。结果表明,基于仿真模型的计算值与样件测试值吻合良好,获得了飞轮转子的最佳几何外形和制备工艺参数,使转子的最大工作外缘线速度达697 m/s,最大储能密度为44.5 Wh/kg。研究成果对复合材料高速飞轮转子护套的设计与制造具有重要的意义。

关键词: 复合材料, 纤维缠绕, 飞轮转子, 大张力, 高速旋转

Abstract: The carbon fiber composite has been widely applied to manufacture high speed flywheel rotor sheath for its high specific strength, specific stiffness, and absence of high frequency eddy current power loss. Moreover, compared with the press-fitted process, the large tension winding process is more suitable for applying the interference fit between the carbon fiber composite sheath and the metal hub. In this paper, the design and forming process of the large tension winding composite sheath of the flywheel rotor was discussed. A three-dimensional finite element model of composite flywheel rotor has been built. The filament winding tension was applied by using temperature difference method. And the winding and curing processes were simulated by the element deletion method. The influence of the winding tension and the interference between the hub and the shaft on the compressive stress at the interface of the rotor was analyzed at the speed of 30000 RPM and the different operating temperature. In addition, the specimens of composite sheath of high speed flywheel rotor were prepared by the large tension winding technology. The radial compressive stress of the sheath on hub and the radial strain of the hub were tested. The results show that the calculated values were in agreement with the measured values of specimens. The optimum geometry and technological parameters of the composite flywheel rotor were obtained. The maximum energy storage density was 44.5 Wh/kg, while the peripheral speed was 697 m/s. The results of this paper are of important significance to the design and manufacture of composite high speed flywheel rotor sheath.

Key words: composite materials, filament winding, flywheel rotor, large tension, high-speed rotation

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