This paper means to provide an innovative design of aero-engine after investigating existing aero-engines. It is a late model power plant design which is based on the watercraft electromagnetic propulsion technology and the theory that in electromagnetic field magnetic field generates Ampere force to current flow and in combination with specific structures of aero-engines. The design principle of this engine is that when the air working medium with high conductivity goes through an arc generator, it will ionize and produce plasma, which actions in the magnetic field that produced by built-in superconducting magnetic and generates forward push. This design will provide a theoretical reserve for future development of aero-engines and has potential market prospects.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Electromagnetic Propulsion Aero-Engine Design Based on Ampere Theorem


    Beteiligte:
    Bi, Shu-Sheng (Autor:in) / Fang, Shi-Xing (Autor:in) / Wang, Shi-Hao (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    6 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Integrated Thermal Aero Propulsion (ITAP) Engine

    Fagan, John R. / Morris, Scott / Cameron, Joshua | AIAA | 2022



    Aero Engine Design

    Ford, Terry | Emerald Group Publishing | 1992


    Aero engine design

    Wilkinson, G.S. | Engineering Index Backfile | 1934