A flexbeam for a rotor blade is provided and includes a first end coupled to a body of the rotor blade and a second end coupled to a flap disposed along a trailing edge of the body to pitch about a pitching axis defined along a span of the body and a flexbeam body extending from the first end to the second end and being configured to retain the flap under a first loading and being flexible about the pitching axis.


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    Titel :

    Flexbeam hinge for helicopter blade active trailing edge flap


    Beteiligte:
    KOPANSKI KRIS (Autor:in) / COWLES DEVON (Autor:in) / BRUNO DAVID E (Autor:in) / MINER FREDERICK J (Autor:in) / HEIN BENJAMIN REED (Autor:in)

    Erscheinungsdatum :

    2016-08-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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