Reinforcement structure (1) for an opening (10) in the primary structure of an aircraft, said structure comprising a skin (2), frame members (3) which are transverse with respect to the flying direction of the aircraft, and stringers (4) which are longitudinal with respect to the flying direction of the aircraft, said reinforcing structure (1) comprising: - a perimetral reinforcing element (5) situated along the edge of the opening (10) and reproducing the geometrical form thereof; - at least one pair of transverse reinforcing elements (6) arranged on both transverse sides of the opening (10); - at least one pair of longitudinal reinforcing elements (7) arranged on both longitudinal sides of the opening (10).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    INTERNAL STRUCTURE OF AIRCRAFT MADE OF COMPOSITE MATERIAL


    Weitere Titelangaben:

    INNERE FLUGZEUGSTRUKTUR AUS VERBUNDWERKSTOFF
    STRUCTURE INTERNE D'AÉRONEF EN MATÉRIAU COMPOSITE



    Erscheinungsdatum :

    25.01.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    INTERNAL STRUCTURE OF AIRCRAFT MADE OF COMPOSITE MATERIAL

    AREVALO RODRIGUEZ ELENA / CRUZ DOMINGUEZ FRANCISCO JOSE | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft structure made of composite material

    AREVALO RODRIGUEZ ELENA | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft structure made of composite material

    AREVALO RODRIGUEZ M ELENA | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft structure made of composite material

    AREVALO RODRIGUEZ ELENA | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft structure made of composite material

    ARÉVALO RODRÍGUEZ M ELENA | Europäisches Patentamt | 2018

    Freier Zugriff