设计具有特定要求的复合材料飞轮

Saad Jabbr Nazal
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引用次数: 0

摘要

为了满足储能系统对高能量密度和长寿命日益增长的需求,复合材料飞轮的设计方法不断得到改进。这项研究的目标是设计一个能够存储10 m -焦耳的飞轮,质量为10 Kg,最大直径为750 mm,最大长度为300 mm,同时以70000 RPM的标称速度旋转。复合材料技术是实现飞轮最大性能所需的超高强度重量比的方法之一。本报告介绍了一种复合Stodola飞轮设计,能够产生10 m -焦耳,质量为10 Kg。该研究旨在获得用于储能运行的高质量飞轮。在飞轮的设计和性能预测中进行了弹性、粘弹性和疲劳分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
DESIGN OF A COMPOSITE FLYWHEEL WITH SPECIFIC REQUIRMENTS
In order to meet the increasing demand of high energy density and long life of energy storage systems, improvement of composite flywheel design approaches have been under development. The goal of this research is to design a flywheel capable of storing 10M-Joules with a mass of 10 Kg, a maximum diameter of 750 mm, and a maximum length of 300 mm, while spinning at a nominal speed of 70,000 RPM. Composite technology is one of the ways to attain extraordinarily high strength-to-weight ratios required for maximum flywheel performance. This report presents a Composite Stodola flywheel design capable of producing 10 M-Joules, with a mass of 10 Kg. The research was conducted to obtain a high quality flywheel for energy storage operations. Elastic, viscoelastic, and fatigue analysis were developed in the design as well as the prediction of the behavior of flywheel.
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