Providing improved yaw maneuverability to an aerial vehicle of the multi-blade type, that enables modifying the pitch angle (α) of its rotors blades, and a method of implementation for this purpose, wherein the axis of movement of at least two pairs of the aerial vehicle's rotors are tilted in a symmetrical configuration in relation to the aerial vehicle's yaw plane, so that each pair converges towards another point on the same level along a longitudinal axis plane of the aerial vehicle while creating an angle (Υ) between the rotation planes of the rotors of each pair, which is less than 180° and greater than 140°.


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    Titel :

    IMPROVED MANEUVERABILITY AERIAL VEHICLE AND A METHOD IMPLEMENTED FOR THIS PURPOSE


    Weitere Titelangaben:

    LUFTFAHRZEUG MIT VERBESSERTER MANÖVRIERFÄHIGKEIT UND IMPLEMENTIERUNGSVERFAHREN FÜR DIESEN ZWECK
    VÉHICULE AÉRIEN À MANOEUVRABILITÉ AMÉLIORÉE ET PROCÉDÉ MIS EN OEUVRE À CET EFFET


    Beteiligte:
    AGRONOV AHARON (Autor:in)

    Erscheinungsdatum :

    04.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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