An inlet cover mechanism for an air launched vehicle includes a quick release pin, a chassis, a collar, and a piston pin. The inlet cover mechanism facilitates attachment and deployment of an inlet cover with the air launched vehicle. The quick release pin is connected to the inlet cover. The chassis is connected to the air launched vehicle. The collar is connected to the chassis and is releasably engageable with the quick release pin. The piston pin is slidably engaged within the chassis and is configured to contact the quick release pin.


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    Titel :

    Inlet Cover Mechanism


    Beteiligte:

    Erscheinungsdatum :

    19.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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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