The invention provides a catapult excitation safety device of a fixed-wing aircraft catapult. The catapult excitation safety device mainly and structurally comprises a slide supporting frame, a fixing shaft, a gear rod, a gear rod lock and other portions. The fixing shaft is vertically installed on one side of the slide supporting frame, and a gear rod capable of being opened and closed is fixed to the fixing shaft. The other end of the gear rod stretches across the supporting frame and is locked by the gear rod lock.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Catapult excitation safety device of fixed-wing aircraft catapult


    Erscheinungsdatum :

    29.04.2015


    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




    Fixed-wing unmanned aerial vehicle catapult-assisted take-off device and catapult-assisted take-

    WANG LIANGXIU / LIU YUNXIAO / LI HAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft carrier catapult

    XU YANMING | Europäisches Patentamt | 2015

    Freier Zugriff

    Vacuum-energy-storage-type launching catapult for fixed-wing aircraft

    WANG ZHENCHUAN | Europäisches Patentamt | 2016

    Freier Zugriff

    INCENDIARY WARHEAD LAUNCH CATAPULT, COMBUSTION EXPANSION FORCE CATAPULT, NUCLEAR CATAPULT

    SHIRAKAWA TOSHIHISA | Europäisches Patentamt | 2024

    Freier Zugriff