An aircraft casing structure including a shroud surrounding the engine and made up of a plurality of sectors; a plurality of radial arms, each mounted between two adjacent shroud sectors and each having a base; and a plurality of fasteners for fastening the shroud sectors on the bases of the radial arms; the fasteners including a plurality of plates each mounted flush in a respective groove of corresponding shape in a shroud sector, and a set of headed bolts held captive in the plate by a difference of diameter between their shanks and their threads, a set of captive nuts being fastened to the bases to provide a secure connection between the shroud sectors and the radial arms by each nut receiving the thread of a respective captive bolt of the set of headed bolts.


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    Titel :

    STRUCTURE DE CARTER INTERPOSEE ENTRE LE MOTEUR ET LA NACELLE A PLATINE A VIS


    Weitere Titelangaben:

    CASING STRUCTURE ARRANGED BETWEEN AN ENGINE AND A NACELLE, THE CASING STRUCTURE COMPRISING A FIXATION PLATE CARRYING ATTACHMENT BOLTS
    STRUKTURGEHÄUSE, ANGEORDNET ZWISCHEN TRIEBWERK UND TRIEBWERKSGONDEL, MIT EINER DIE BEFESTIGUNGSBOLZEN TRAGENDE BEFESTIGUNGSPLATTE


    Beteiligte:
    BELJAMBE CEDDRIC (Autor:in) / ROBIN NOËL (Autor:in)

    Erscheinungsdatum :

    03.10.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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