The invention discloses a carrier aircraft electromagnetic catapult. The carrier aircraft electromagnetic catapult drags an aircraft though electromagnetic coupling depending on power of an engine, and is advantaged in that the catapult is simple in structure and high in reliability, and can recover next launch in a short time, and is without energy storage units. The carrier aircraft electromagnetic catapult comprises an engine 1, a power transmission system 2, a first rotor 3, a second rotor 4, a current regulator 5, a current load 6 and a cable 7. The engine 1 transmits power to the first rotor 3 through the power transmission system 2, the second rotor 4 is driven by the first rotor 3 through electromagnetism, the cable 7 is attached to the second rotor 4, and is dragged by the second rotor 4, the cable 7 is used for dragging the aircraft, the current regulator 5 is used for regulating the current output by the first rotor 3 or the second rotor 4, and the current load 6 is used for absorbing electric energy output by the current regulator 5.


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    Titel :

    Carrier aircraft electromagnetic catapult


    Beteiligte:
    SUN HONGBIN (Autor:in)

    Erscheinungsdatum :

    24.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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