Improved impact-resistant and damage-tolerant aircraft fuselage. The invention relates to a section (32) of the fuselage of an aircraft suffering impacts from external bodies, the fuselage of the aircraft having a curved form with at least one vertical plane of symmetry (A - A) and central longitudinal axis, and comprising a skin (35) and a plurality of ring frames ( 37) arranged perpendiculary to said longitudinal axis, said section (32) of the fuselage also comprising at least one reticular internal structure ( 51, 53) mounted on a support structure ( 41, 43), wich includes longitudinal beams (39) connected to the skin (35) and interconnected with said ring frames (37), said reticular internal structure ( 51, 53) being arranged in order to create at least one closed cell (75) with the skin (45) in order to improve the strength thereof and the tolerance to damage from said impacts.


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    Titel :

    IMPROVED IMPACT RESISTANT AND DAMAGE TOLERANT AIRCRAFT FUSELAGE


    Weitere Titelangaben:

    VERBESSERTER SCHLAGZÄHER UND BESCHÄDIGUNGSBESTÄNDIGER FLUGZEUGRUMPF
    FUSELAGE D'AÉRONEF RÉSISTANT AUX IMPACTS ET TOLÉRANT AUX DOMMAGES AMÉLIORÉ



    Erscheinungsdatum :

    15.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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