A flexbeam unit for a multi-blade rotor of a rotary wing aircraft, the flexbeam unit comprising a plurality of flexbeam elements defining a predetermined number of torsion elements that are connectable with associated rotor blades of the multi-blade rotor, at least one of the predetermined number of torsion elements comprising at least one flexbeam element having an associated longitudinal direction, the at least one flexbeam element comprising at least one twisted area in which the at least one flexbeam element is twisted in the associated longitudinal direction.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FLEXBEAM UNIT WITH AT LEAST ONE TWISTED FLEXBEAM ELEMENT


    Beteiligte:
    BUESING MORITZ (Autor:in)

    Erscheinungsdatum :

    2015-12-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flexbeam unit with at least one twisted flexbeam element

    BUESING MORITZ | Europäisches Patentamt | 2018

    Freier Zugriff

    Flexbeam unit with at least one twisted flexbeam element

    BÜSING MORITZ | Europäisches Patentamt | 2018

    Freier Zugriff

    Partly cruciform flexbeam and method of manufacturing such a flexbeam

    KUNTZE-FECHNER GERALD / ORTNER MARTIN | Europäisches Patentamt | 2016

    Freier Zugriff

    Flexbeam rotor

    HUNTER DAVID H / CASEY RYAN THOMAS / BYRNES FRANCIS EDWARD | Europäisches Patentamt | 2017

    Freier Zugriff

    Partly cruciform flexbeam and method of manufacturing such a flexbeam

    KUNTZE-FECHNER GERALD / ORTNER MARTIN | Europäisches Patentamt | 2017

    Freier Zugriff