An aircraft is provided and includes an airframe, a blade disk, which is rotatable relative to the airframe, including a plurality of rotor blades, a rotor shaft disposed to drive rotation of the blade disk relative to the airframe and a pitching of each of the rotor blades about corresponding pitch axes and a rotor assembly configured to form couplings by which each of the rotor blades is coupled to the rotor shaft. The rotor assembly includes a composite laminate arranged to resolve loading associated with the couplings in-plane of the composite laminate.


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    Titel :

    AIRCRAFT ROTOR ASSEMBLY WITH COMPOSITE LAMINATE


    Weitere Titelangaben:

    FLUGZEUGROTORBAUGRUPPE MIT VERBUNDLAMINAT
    ENSEMBLE ROTOR D'AÉRONEF DOTÉ DE STRATIFIÉ COMPOSITE


    Beteiligte:

    Erscheinungsdatum :

    2017-04-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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