A rotor includes a rotatable hub, blades, and two coupling members, namely, a first coupling member and a second coupling member that couple each blade and the hub. The longitudinal directions of the first coupling member and the second coupling member lie along a tangential direction of a rotation trajectory of the hub, and the first coupling member and the second coupling member are spaced apart from each other in a radial direction of the rotation trajectory.


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    Titel :

    ROTOR AND AIRCRAFT


    Beteiligte:
    ISO TOMOYUKI (Autor:in) / ISHITSUKA YUJI (Autor:in)

    Erscheinungsdatum :

    15.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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