A bladed rotor comprises a rotor body 2 carrying blades 6, whose pitch can be varied by means of a pitch input shaft 10. The pitch input shaft 10 drives the respective blade 6 about a spanwise axis X of the blade through a harmonic drive reduction gear 14. The harmonic drive reduction gear 14 comprises a wave generator 16 which is fixed for rotation on the pitch input shaft 10 and a flex spline which meshes with a circular spline 20 and is secured to the blade 6.


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    Titel :

    A variable pitch propeller rotor


    Weitere Titelangaben:

    Verstellbarer Propellerrotor
    Rotor d'hélice à pas variable


    Beteiligte:
    THORNTON STEWART (Autor:in) / SIMMS PAUL (Autor:in) / MCFARLANE COLIN (Autor:in)

    Erscheinungsdatum :

    19.12.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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