直线电机在人造卫星燃油泵系统中的应用

Conference Record of the 1992 IEEE Industry Applications Society Annual Meeting Pub Date : 1992-10-04 DOI:10.1109/IAS.1992.244450

J. Oyama, T. Higuchi, H. Akashi, E. Yamada, N. Nagatomo, I. Yoshinaga

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引用次数: 3

摘要

本文提出了一种新型的直线电机推进燃油泵系统，在直线电机两侧安装两个泵，并组织一个带弹簧的谐振系统来减小额定推力。假设泵的排出压力为21.0 kgf/cm/sup 2/，排出流量为21.25 cm/sup 3/ s。设计、制造并测试了一种线性脉冲电机样机。利用等效磁路对推力特性进行了估计，计算结果与实验结果吻合较好

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Application of linear motor on artificial satellite fuel pump system

The authors propose a new type of fuel pump system with linear motor propulsion, in which two pumps are equipped on both sides of the linear motor and a resonant system with springs is organized to decrease the rated thrust. A pump where the discharge pressure is 21.0 kgf/cm/sup 2/ and the discharge flow rate is 21.25 cm/sup 3//s is assumed. A prototype linear pulse motor was designed, built, and tested. The thrust characteristics are estimated using an equivalent magnetic circuit, and it is confirmed that the calculated results agree well with the experimental results.<>

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Conference Record of the 1992 IEEE Industry Applications Society Annual Meeting

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