Durability of filament-wound composite flywheel rotors

被引:0
|
作者
Jun Koyanagi
机构
[1] Japan Aerospace Exploration Agency,Institute of Space and Astronautical Science
来源
Mechanics of Time-Dependent Materials | 2012年 / 16卷
关键词
Polymer matrix composites; Durability; Strength; Flywheel; Rotational stress;
D O I
暂无
中图分类号
学科分类号
摘要
This paper predicts the durability of two types of flywheels, one assumes to fail in the radial direction and the other assumes to fail in the circumferential direction. The flywheel failing in the radial direction is a conventional filament-wound composite flywheel and the one failing in the circumferential direction is a tailor-made type. The durability of the former is predicted by Micromechanics of Failure (MMF) (Ha et al. in J. Compos. Mater. 42:1873–1875, 2008), employing time-dependent matrix strength, and that of the latter is predicted by Simultaneous Fiber Failure (SFF) (Koyanagi et al. in J. Compos. Mater. 43:1901–1914, 2009), employing identical time-dependent matrix strength. The predicted durability of the latter is much greater than that of the former, depending on the interface strength. This study suggests that a relatively weak interface is necessary for high-durability composite flywheel fabrication.
引用
收藏
页码:71 / 83
页数:12
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