The invention discloses an aircraft carrier air injection catapult solving the problem of takeoff of an airplane on an aircraft carrier. A jet engine serves as power and an airplane takes off in an acceleration manner. The aircraft carrier air injection catapult comprises a guide rail (1), a tackle (2), a jet engine set (3), a wireless receiving and transmitting control system (4), a traction cable (5), a steering wheel 1 (6), a steering wheel 2 (7), a shuttle (8) and an arresting cable (9). The shuttle is connected with the airplane. The wireless receiving and transmitting control system (4) can be connected with the airplane and controlled by the airplane. The jet engine set (3) is installed on the tackle (2), and the airplane takes off in the acceleration manner through pushing force of the jet engine set (3) via the tackle (2), the steering wheel 1 (6), the steering wheel 2(7) and the traction cable (5). The arresting cable (9) prevents the jet engine set (3) from continuing to move after the airplane takes off. At the takeoff point, the control system detects the speed of the airplane, and whether the airplane is in the fault processing procedure or not is judged. The aircraft carrier air injection catapult is adjustable in pushing force, constant in launching push force, small in weight and convenient to install and maintain, and has the beneficial effects of being simple in structure and high in energy utilization rate.


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    Titel :

    Aircraft carrier air injection catapult


    Beteiligte:
    CHEN PEIHONG (Autor:in)

    Erscheinungsdatum :

    2015-11-25


    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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