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A reciprocating single-phase tubular switched reluctance linear launcher (TSRLL) with a short stroke is presented in this paper. The parametric design of this launcher is achieved based on finite-element method (FEM). By using the finite-element (FE) software FLUX, the 2-D and 3-D electromagnetic analyses of this launcher are carried out, respectively. The characteristic curves of position-current-flux linkage are analyzed by the 2-D and 3-D FEM. The prototype tests are conducted to verify the FE analyses. The static tests results show that the 3-D FE calculated results are more precise than the 2-D FE calculated results, and they coincide well with prototype static test results. The effectiveness of the FE model for the TSRLL is further testified by the results of prototype dynamic tests. Finally, some analyses on sensitivity parameters are conducted to further improve the performance of the TSRLL. [ABSTRACT FROM PUBLISHER]

In this paper, a magnetic analysis of large linear motors with long primary and short interior permanent magnet (PM) secondary is presented. The calculations are carried out using a finite-element method, taking into account the secondary motion and saturation in iron parts. Reluctance force could be increased using interior PM secondary. The thrust force oscillations are evaluated to obtain minimum force ripple. Furthermore, a magnet demagnetization analysis is presented to evaluate the magnet demagnetization risk under loading. Reduction in the magnet volume is considered for cheaper and simpler secondary structure. [ABSTRACT FROM AUTHOR]

As the exploitation of astrospace deepens, many new types of space-based electromagnetic launchers (EMLs) have aroused wide attention and discussions. Compared with traditional slotted electromagnetic linear launchers, a slotless-plate permanent-magnet linear synchronous motor can easily meet demands such as flexible structure, light weight, and high control precision for space use. This paper analyzes the magnetic field of the slotless inverted- U structure based on the equivalent-magnetizing-current method. The validity of this technique for integral-slot configuration is confirmed with finite-element analysis. Then, the influence of the main design parameters is investigated, and design optimization guides are established for the selection of the key design parameters. To reach the suitable air-gap flux density here, some new constructional optimization details are discussed. Design optimization is also performed to fulfill enough thrust for the EML system. [ABSTRACT FROM AUTHOR]