An aircraft payload retention system includes a cable, a brake assembly, a hollow crushable member and a hollow structural member. The hollow structural member is fixed adjacent an aircraft internal cargo bay. In response to a high-G condition, the payload may break free from a tie-down system and move forward. The brake assembly engages the hollow crushable member within the hollow structural member and begins to crush the hollow crushable member as the cable is pulled therethrough to dissipate energy of the payload into the structure of the aircraft to arrest forward movement of the payload toward the cockpit.


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    Titel :

    AIRCRAFT PAYLOAD RETENTION SYSTEM FOR INTERIOR LOADS


    Weitere Titelangaben:

    SYSTEM ZUR RÜCKHALTUNG VON FLUGZEUGNUTZDATEN FÜR INNENLASTEN
    SYSTÈME DE RÉTENTION DE CHARGE UTILE D'AÉRONEF POUR CHARGES INTÉRIEURES


    Beteiligte:

    Erscheinungsdatum :

    11.10.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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



    Payload retention device

    Monford, Leo G., Jr. | NTRS | 1992


    STS payload retention system concept

    Clark, K. H. | NTRS | 1982


    STS Payload Retention System Concept

    K. H. Clark | NTIS | 1982


    AIRCRAFT PAYLOAD LAUNCH SYSTEM

    WHITE ANDREW CHARLES | Europäisches Patentamt | 2016

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    AIRCRAFT PAYLOAD LAUNCH SYSTEM

    Europäisches Patentamt | 2016

    Freier Zugriff