A flexbeam unit comprising a plurality of flexbeam elements, each defining a load passing member that is attachable to a rotor hub associated with a rotor shaft of said multi-blade rotor, said plurality of flexbeam elements defining a predetermined number of torsion elements that are connectable with associated rotor blades of said multi-blade rotor, wherein at least one of the predetermined number of torsion elements comprises at least one first flexbeam element defining a first longitudinal direction and at least one second flexbeam element defining a second longitudinal direction, wherein said at least one first and second flexbeam elements are interconnected by a beam connector in a direction transverse to said first and/or second longitudinal directions.


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    Titel :

    FLEXBEAM UNIT FOR A BEARINGLESS OR A HINGE AND BEARINGLESS MULTI-BLADE ROTOR OF A ROTARY WING AIRCRAFT


    Beteiligte:
    PFALLER RUPERT (Autor:in)

    Erscheinungsdatum :

    16.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flexbeam unit for a bearingless or a hinge- and bearingless multi-blade rotor of a rotary wing aircraft

    PFALLER RUPERT / SCHULZ MARTIN / BODEMANN TOBIAS | Europäisches Patentamt | 2018

    Freier Zugriff


    Flexbeam unit for a bearingless or a hinge- and bearingless multi-blade rotor of a rotary wing aircraft

    PFALLER RUPERT / SCHULZ MARTIN / BODEMANN TOBIAS | Europäisches Patentamt | 2015

    Freier Zugriff

    FLEXBEAM UNIT FOR A BEARINGLESS OR A HINGE- AND BEARINGLESS MULTI-BLADE ROTOR OF A ROTARY WING AIRCRAFT

    PFALLER RUPERT / SCHULZ MARTIN / BODEMANN TOBIAS | Europäisches Patentamt | 2015

    Freier Zugriff