A casing structure interposed between the engine and the nacelle of an aircraft, the structure including a shroud surrounding the engine having an engine axis and including a stationary portion and a plurality of sectors; a radial arm providing the connection to the nacelle; fasteners for securing the plurality of shroud sectors to one another or to the radial arm; and the fasteners include two series of holes formed in two parallel side walls of the shroud sectors for the purpose of receiving two respective series of bolts, each passing through a corresponding set of orifices of an adjacent shroud sector or of an adjacent radial arm, a hinge arranged between each of the shroud sectors and the stationary portion of the shroud to enable the shroud sectors to be pivoted in individual manner about a common pivot axis perpendicular to the side walls arranged along the engine axis.


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    Titel :

    STRUCTURE DE CARTER INTERPOSEE ENTRE LE MOTEUR ET LA NACELLE A SECTEURS DE VIROLE PIVOTANTS


    Weitere Titelangaben:

    ENGINE CASING HAVING PIVOTABLE ACCESS DOORS
    TRIEBWERKSGEHÄUSE MIT SCHWENKBAREN WARTUNGSKLAPPEN


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

    Erscheinungsdatum :

    2019-01-09


    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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