A fastener assembly (102) may comprise a housing (104) defining a first cavity (106) and a second cavity (108). A first threaded member (110a) and a second threaded member (110b) may be located within the housing (104). A first biasing member (112) may be coupled to the first threaded member (110a). A second biasing member (112) may be coupled to the second threaded member (110b).


    Access

    Download


    Export, share and cite



    Title :

    FASTENER ASSEMBLY FOR NACELLE PRESSURE-RELIEF DOORS


    Additional title:

    BEFESTIGUNGSANORDNUNG FÜR GONDELDRUCKENTLASTUNGSTÜREN
    ENSEMBLE DE FIXATION POUR PORTES DE DÉTENTE DE PRESSION DE NACELLE


    Contributors:

    Publication date :

    2023-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05B LOCKS , Schlösser



    Fastener assembly for nacelle pressure-relief doors

    DELANEY MAC PATRICK | European Patent Office | 2021

    Free access

    FIRE SEAL ASSEMBLY FOR NACELLE DOORS

    RAMLAOUI JIHAD / SLATTERY TIMOTHY | European Patent Office | 2021

    Free access

    Fire seal assembly for nacelle doors

    RAMLAOUI JIHAD / SLATTERY TIMOTHY | European Patent Office | 2021

    Free access

    FIRE SEAL ASSEMBLY FOR NACELLE DOORS

    RAMLAOUI JIHAD / SLATTERY TIMOTHY | European Patent Office | 2022

    Free access

    Aircraft nacelle comprising a cowl with two articulated doors

    GELIOT JEAN / LABARTHE CHRISTOPHE | European Patent Office | 2022

    Free access