The invention discloses a carrier-based aircraft take-off structure, and especially relates to a carrier-based aircraft take-off structure of a vertical takeoff and landing fixed wing airplane disclosed in the patent with an application number of 2015203521439. Besides, the carrier-based aircraft take-off structure is composed of a driving motor, a motor deceleration driving device, an airplane rotation driving output shaft and an airplane hook. The driving motor and the motor deceleration driving device are installed and fixed below a naval flight deck, the airplane rotation driving output shaft is driven and controlled by the driving motor and the motor deceleration driving device and penetrates the flight deck, the upper end of the airplane rotation driving output shaft is connected with the lower half segment of the airplane hook and the two rotate synchronously, the upper half segment of the airplane hook and an airplane main beam form one body and can synchronously rotate, the airplane hook is divided into the upper half segment and the lower half segment and has functions of close connection, firm locking and controllable instant disengagement, and the upper half segment and the lower half segment synchronously rotate.


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    Title :

    Carrier-based aircraft take-off structure


    Contributors:
    ZHANG BIN (author)

    Publication date :

    2016-01-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 / B64C AEROPLANES , Flugzeuge



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