摘要
Magnetically suspended flywheel (MSFW) with gimballing capability fulfills requirements of precision and maneuvers for space applications. A novel reluctance force-type hybrid magnetic bearing (RFHMB) is presented based on analysis of demerits of Lorentz force-type magnetic bearing and common RFHMB. It features that radial and axial magnetic bearing units are integrated into a compact assembly with four separate biased permanent magnets and two conical stators; four radial poles with shoes and rotor made of iron-based amorphousness can reduce eddy loss. Equivalent magnetic circuits of permanent magnets and their control currents are presented. Simulation results indicate flux density fluctuates from 0.272 T to 0.41 T; rotor tilting does not affect the suspension force when rotor only tilts around X -axis or Y -axis. When rotor drifts in X, Y, or Z direction and tilts around X -axis or Y -axis simultaneously, force in corresponding directions slightly increases with tilting angle's enlargement, but the maximum change does not exceed 14%. Additional tilting torque mainly determined by uniformity of flux density in conical air gaps is 0.05 Nm which is far smaller than 11 Nm in common RFHMB; magnetic suspension force is effectively decoupled among X, Y, and Z directions; results prove that MSFW with gimballing capability theoretically meets maneuvering requirement of spacecraft.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 836058 |
| 期刊 | Mathematical Problems in Engineering |
| 卷 | 2013 |
| DOI | |
| 出版状态 | 已出版 - 2013 |
指纹
探究 'Design and mathematical analysis of a novel reluctance force-type hybrid magnetic bearing for flywheel with gimballing capability' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver