The invention discloses a hydraulic and electromagnetic composite aircraft catapult, in particular to an aircraft catapult for an aircraft carrier. An electromagnetic catapult is improved, and mainly, the capacity of a forced energy storage device is reduced. According to the technical scheme, through a hydraulic cylinder and an acceleration mechanism, an electromagnetic catapult unit is turned on after an initial speed of 45 m/s or higher is provided for an aircraft, acceleration does not need to be started from zero during electromagnetic catapulting, and therefore the capacity of the forced energy storage device is reduced. The hydraulic and electromagnetic composite aircraft catapult can be used as an aircraft catapult without runways on land or a vehicle-mounted mobile aircraft catapult.


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    Title :

    Hydraulic and electromagnetic composite aircraft catapult


    Contributors:

    Publication date :

    2015-11-04


    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



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