The present invention regards an aircraft structure comprising an aerodynamic composite shell (7), the interior face (9) of which in whole or in part is bonded with at least one two- or three-dimensional structural composite part (11) by means of a bonding material (15). It also regards a method of manufacture of the aircraft structure. The bonding material (15) comprises a non-structural fiber reinforced resin system, wherein at least one portion of the bonding material, which portion spatially corresponds with an interior face filling volume (21), is thicker than other portions of the bonding material (15), due to settlement of resin of the non-structural fiber reinforced resin system in said interior face filling volume (21) during the viscous phase of the curing of the non-structural fiber reinforced resin system.


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    Titel :

    AN AIRCRAFT STRUCTURE WITH STRUCTURAL NON-FIBER REINFORCING BONDING RESIN LAYER


    Weitere Titelangaben:

    FLUGZEUGSTRUKTUR MIT STRUKTURELLER FASERFREIER VERSTÄRKENDER BINDEHARZSCHICHT
    STRUCTURE D'AÉRONEF POSSÉDANT UNE COUCHE DE RÉSINE DE LIAISON DE RENFORCEMENT À FIBRES NON STRUCTURELLES


    Beteiligte:
    GRANKÄLL TOMMY (Autor:in) / HALLANDER PER (Autor:in) / PETERSSON MIKAEL (Autor:in) / WEIDMANN BJÖRN (Autor:in)

    Erscheinungsdatum :

    06.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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