A cargo system (100, 520) is provided. The cargo system may comprise a floor panel (112), a cargo sled configured to move across the floor panel (112), and a cargo restraint (200, 202, 500, 722) configured to translate relative to the floor panel (112). The cargo restraint may comprise a longitudinal restraint rod (302, 503) configured to protrude from the floor panel (112) in a deployed position. The cargo restraint may also comprise a restraint surface (300A, 501) disposed on the longitudinal restraint rod. The cargo restraint may enable the cargo sled to pass over the restraint surface in a stowed position. An electromechanical actuator (702) may be mechanically coupled to the longitudinal restraint rod and configured to deploy and stow the cargo restraint.


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    Title :

    CONFORMAL ACTUATOR OPERATED AIRCRAFT CARGO RESTRAINT MECHANISM


    Additional title:

    KONFORMER AKTUATORBETÄTIGTER LUFTFRACHTZURÜCKHALTUNGSMECHANISMUS
    MÉCANISME DE RETENUE DE CHARGEMENT D'AÉRONEF MANOEUVRÉ PAR ACTIONNEUR CONFORME


    Contributors:

    Publication date :

    2019-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60P Fahrzeuge zum Transport von Lasten oder zum Befördern, Tragen oder Aufnehmen besonderer Lasten oder Gegenstände , VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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