The invention discloses an aircraft carrier ejector. The aircraft ejector comprises a diesel engine set and a magnetic vehicle. The diesel engine set is connected with an input shaft of an acceleration wheel through a belt, one end of a haulage rope is connected with the magnetic vehicle, and the other end penetrates a fixed pulley and is winded on the acceleration wheel. The magnetic vehicle comprises a vehicle A and a vehicle B, the vehicle A is arranged on a deck, the vehicle B is arranged under the deck, both the lower surface of the vehicle A and the upper surface of the vehicle B are provided with strong magnets, a rail groove is disposed between the vehicle B and the deck, the end of the vehicle A is provided with a thrust sleeve, the end of the vehicle B is provided with a haulage rope fixing apparatus, the lower portion, close to the fixed pulley, of the deck is provided with a detection contact, the detection contact is connected with a controller to control a switch of an diesel engine, and a buffer is disposed between the detection contact and the fixed pulley. The aircraft carrier ejector can effectively shortened the launch time of an airplane so as to raise the combat efficiency; the airplane can launch on a short runway, the space of the deck can be saved; and a heavyweight airplane can launch on an aircraft carrier, the energy can be saved, and the deck of the aircraft carrier does not need refitting a lot.


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    Titel :

    Aircraft carrier ejector


    Beteiligte:
    LI YUXIANG (Autor:in) / QIAO ZHONGHUI (Autor:in) / LI JUNYI (Autor:in)

    Erscheinungsdatum :

    2015-10-21


    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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