The invention provides a superconducting electric suspension propulsion integrated system which comprises a first superconducting mover coil assembly, a second superconducting mover coil assembly, a first propulsion coil assembly, a second propulsion coil assembly, a first 8-shaped zero-flux coil assembly, a second 8-shaped zero-flux coil assembly, a first suspension induction plate assembly and a second suspension induction plate assembly. The first propulsion coil assembly and the first superconducting rotor coil assembly interact to generate electromagnetic driving force for driving the train to advance, and the second propulsion coil assembly and the second superconducting rotor coil assembly interact to generate electromagnetic driving force for driving the train to advance. The first and second 8-shaped zero-flux coil groups respectively interact with the first and second superconducting rotor coil groups to generate a suspension force and a guide force; and the first and second suspension induction plate groups respectively interact with the first and second superconducting rotor coil groups to generate a suspension force and a guide force. By means of the technical scheme, the technical problems that in the prior art, a Holloman high-speed test track test line is complex in structure topology, low in magnetic field utilization rate, low in floating resistance ratio and low in economical efficiency are solved.

    本发明提供了一种超导电动悬浮推进一体化系统,包括第一、第二超导动子线圈组、第一、第二推进线圈组、第一、第二8字零磁通线圈组以及第一、第二悬浮感应板组,第一推进线圈组与第一超导动子线圈组相互作用以产生驱动列车前进的电磁驱动力,第二推进线圈组与第二超导动子线圈组相互作用以产生驱动列车前进的电磁驱动力,第一、第二8字零磁通线圈组分别与第一、第二超导动子线圈组相互作用以产生悬浮力和导向力,第一、第二悬浮感应板组分别与第一、第二超导动子线圈组相互作用以产生悬浮力和导向力。应用本发明的技术方案,以解决现有技术中Holloman高速测试轨道试验线存在结构拓扑复杂,磁场利用率低、浮阻比低且经济性低的技术问题。


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    Titel :

    Superconducting electric suspension propulsion integrated system


    Weitere Titelangaben:

    超导电动悬浮推进一体化系统


    Beteiligte:
    MAO KAI (Autor:in) / ZHANG YANQING (Autor:in) / ZHANG ZHIHUA (Autor:in) / DU XIUFANG (Autor:in) / HU DAOYU (Autor:in) / CAO ZHAOBIN (Autor:in)

    Erscheinungsdatum :

    09.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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