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.


    Access

    Download


    Export, share and cite



    Title :

    Inlet cover mechanism



    Publication date :

    2025-01-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    Inlet Cover Mechanism

    HOLLEN KEITH RYAN / LORIS BRYAN MICHAEL / KNIBB NATHAN MATTHEW et al. | European Patent Office | 2024

    Free access

    Seawater inlet cover

    YANG HWAN SEOK / KWON HEEKYU / KIM BONGSEOK | European Patent Office | 2021

    Free access

    Sliding charging inlet cover

    GARY EDWARDS | European Patent Office | 2024

    Free access

    SLIDING CHARGING INLET COVER

    EDWARDS GARY | European Patent Office | 2022

    Free access

    ENGINE INLET COVER DETECTION SYSTEM

    HAUSMANN JEFFREY / KNIGHT MICHAEL | European Patent Office | 2022

    Free access