A blade pitch actuation mechanism comprising a rotating race member in which is formed a race configured to receive a trunnion pin attached to a blade, whereby the race defines a cam profile such that rotation of the race member causes the trunnion pin received in the race to rotate as it slides over the cam profile.


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    Titel :

    BLADE PITCH ACTUATION MECHANISM


    Beteiligte:
    PRUNET LUDOVIC (Autor:in) / MOLES PATRICK (Autor:in) / LE MEUR KEVIN (Autor:in)

    Erscheinungsdatum :

    2021-09-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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