高温强磁场下飞机用圆柱形磁流变液制动器剪切应力的研究

Kazuki Nagashima, Hiroki Shiga, Y. Kikuchi, H. Wakiwaka, M. Sonehara, Toshiro Sato
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摘要

作者一直在研究一种结合涡流制动器和磁流变液制动器的非接触式混合制动器作为下一代飞机制动器的使用。本文研究了旋转棒周围温度为300度,磁通密度为1.26特斯拉时的剪切应力。实验结果表明,即使在高温高磁场条件下,剪切应力也不会因温度变化而迅速增大或减小,因此V-Co-Fe磁流变液适用于飞机。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Considerations on Shear Stress in Cylindrical Magneto-rheological fluid Brake for Aircraft under High Temperature and High Magnetic Field
The authors have been studying the use of a noncontact hybrid brake that combines an eddy current brake and a magneto-rheological fluid brake as the next generation brake for aircraft. In this paper, we investigated shear stress when the temperature around the rotating rod was changed to 300 degree and the magnetic flux density was changed to 1.26 Tesla. As a result of the experiment, it was found that a V-Co-Fe magneto-rheological fluid was suitable for aircraft because shear stress did not increase or decrease rapidly due to temperature change even under high temperature and high magnetic field conditions.
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