An assembly with an aircraft fuel tank is disclosed having a captive nut with an internal thread, a secondary structure, and a fastener which secures the secondary structure to the fuel tank. The fastener has a shaft which passes through the secondary structure and has an external thread coupled to the internal thread of the captive nut. The fuel tank has a fuel tank element with a hole, and the captive nut has a sleeve which is located in the hole with an interference fit between an outer surface of the sleeve and an inner surface of the wall of the hole.


    Access

    Download


    Export, share and cite



    Title :

    Assembly with captive nut


    Contributors:

    Publication date :

    2022-03-29


    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



    ASSEMBLY WITH CAPTIVE NUT

    TULLOCH WILLIAM / BROOMFIELD PAT | European Patent Office | 2023

    Free access

    ASSEMBLY WITH CAPTIVE NUT

    TULLOCH WILLIAM / BROOMFIELD PAT | European Patent Office | 2022

    Free access

    Assembly with captive nut

    European Patent Office | 2018

    Free access

    ASSEMBLY WITH CAPTIVE NUT

    TULLOCH WILLIAM / BROOMFIELD PAT | European Patent Office | 2023

    Free access

    Assembly with captive nut

    TULLOCH WILLIAM / BROOMFIELD PAT | European Patent Office | 2024

    Free access