Abstract
A tubular moving-magnet linear oscillating motor (TMMLOM) has merits of high efficiency and excellent dynamic capability. To enhance the thrust performance, quasi-Halbach permanent magnet (PM) arrays are arranged on its mover in the application of a linear electro-hydrostatic actuator in more electric aircraft. The arrays are assembled by several individual segments, which lead to gaps between them inevitably. To investigate the effects of the gaps on the radial magnetic flux density and the machine thrust in this paper, an analytical model is built considering both axial and radial gaps. The model is validated by finite element simulations and experimental results. Distributions of the magnetic flux are described in condition of different sizes of radial and axial gaps. Besides, the output force is also discussed in normal and end windings. Finally, the model has demonstrated that both kinds of gaps have a negative effect on the thrust, and the linear motor is more sensitive to radial ones.
| Original language | English |
|---|---|
| Pages (from-to) | 927-940 |
| Number of pages | 14 |
| Journal | Chinese Journal of Aeronautics |
| Volume | 31 |
| Issue number | 5 |
| DOIs | |
| State | Published - May 2018 |
Keywords
- Air-gap flux density
- Linear motor
- Mover gaps
- Quasi-Halbach array
- Thrust output
- Tubular moving-magnet linear oscillating motor (TMMLOM)
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