A propeller blade is provided including a leading edge and a trailing edge. The trailing edge is arranged opposite the leading edge to form an airfoil there between. At least one of the leading edge and the trailing edge include at least one facet.

    Cette invention concerne une pale d'hélice, comprenant un bord d'attaque et un bord de fuite. Le bord de fuite est agencé à l'opposé du bord d'attaque, de façon à former un plan porteur entre ceux-ci. Au moins un élément parmi le bord d'attaque et le bord de fuite comprend au moins une facette.


    Access

    Download


    Export, share and cite



    Title :

    PROPELLER ROTOR FOR A VERTICAL TAKE OFF AND LANDING AIRCRAFT


    Additional title:

    ROTOR D'HÉLICE POUR UN AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX


    Contributors:

    Publication date :

    2015-10-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Propeller rotor for a vertical take off and landing aircraft

    ALBER MARK R | European Patent Office | 2020

    Free access

    PROPELLER ROTOR FOR A VERTICAL TAKE OFF AND LANDING AIRCRAFT

    ALBER MARK R | European Patent Office | 2017

    Free access

    VERTICAL TAKE-OFF AND LANDING AIRCRAFT PROPELLER ROTATION SYSTEM

    OSININ ALEKSANDR TROFIMOVICH | European Patent Office | 2022

    Free access

    Propeller for an aircraft for vertical take-off and landing

    JOHANNES REITER | European Patent Office | 2016

    Free access