Internal shield (41) in the rear fuselage (11) of an aircraft having a propulsion system formed by two engines (13) mounted on each side of it; the rear fuselage (11) having at least a vertical symmetry plane (A-A); the rear fuselage (11) being made of a composite material; the internal shield (41) being located in said vertical symmetry plane (A-A) and extended in an area that covers the possible trajectories of a set of pre-defined fragments detached from one of said engines (13) in a failure event that would impact on critical elements of the opposite engine; the internal shield (41) having a flat shape and an energy absorption capability that allows stopping said fragments. The invention also refers to a method for determining the area of an internal shield (41) and to an aircraft having said internal shield (41)


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    Titel :

    Rear fuselage with a shield for an aircraft with fuselage-mounted engines and method for determining the area of the shield


    Weitere Titelangaben:

    Rumpfheck mit einem Schild für ein Flugzeug mit rumpfmontierten Motoren und Verfahren zur Bestimmung der Fläche des Schildes
    Partie arrière de fuselage avec un bouclier pour aéronef avec moteurs montés sur le fuselage et procedé pour déterminer la surface du bouclier



    Erscheinungsdatum :

    28.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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