CIRCUMFERENCE SPLICE FOR JOINING SHELL STRUCTURES The disclosed shell structure splice (10) and method may include a first panel (1 10a) having a first edge, a second panel (1 10b) having a second edge, the second edge being positioned in edgewise alignment with the first edge to form a splice joint (106), a strap (12) bridging the splice joint (106) and attached to the first panel (1 10a) and the second panel (1 10b), the strap (12) having a first tapered region (22a)and a second tapered region (22b), a first fitting (34) having a tapered section (34) and a flat section (36), the tapered section (34) being attached to the first tapered region (22a) of the strap (12), and a second fitting (24) having a tapered section (34) and a flat section (36), the tapered section (34) being attached to the second tapered region (22b) of the strap (12).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Circumference splice for joining shell structures


    Beteiligte:
    DIEP PAUL (Autor:in) / DOPKER BERNHARD (Autor:in)

    Erscheinungsdatum :

    2016-12-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    CIRCUMFERENCE SPLICE FOR JOINING SHELL STRUCTURES

    DIEP PAUL / DOPKER BERNHARD | Europäisches Patentamt | 2016

    Freier Zugriff

    Circumference splice for joining shell structures

    Europäisches Patentamt | 2018

    Freier Zugriff

    Circumference splice for joining shell structures

    DIEP PAUL / DOPKER BERNHARD | Europäisches Patentamt | 2017

    Freier Zugriff

    Splice Assembly For Joining Structural Components

    REEVES ANDREW C | Europäisches Patentamt | 2016

    Freier Zugriff

    SPLICE ASSEMBLY FOR JOINING STRUCTURAL COMPONENTS

    REEVES ANDREW C | Europäisches Patentamt | 2021

    Freier Zugriff