A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS


    Weitere Titelangaben:

    VTOL-FAHRZEUG MIT KOAXIAL GENEIGTEN ODER NEIGBAREN ROTOREN
    VÉHICULE VTOL À ROTORS COAXIALEMENT BASCULÉS OU BASCULANTS


    Beteiligte:
    YOELI RAPHAEL (Autor:in)

    Erscheinungsdatum :

    06.09.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    VTOL AIRCRAFT WITH TILTABLE PROPELLERS

    MILANI KAZEM | Europäisches Patentamt | 2016

    Freier Zugriff

    VTOL aircraft with tiltable propellers

    MILANI KAZEM | Europäisches Patentamt | 2019

    Freier Zugriff

    VTOL AIRCRAFT WITH TILTABLE PROPELLERS

    MILANI KAZEM | Europäisches Patentamt | 2018

    Freier Zugriff

    Amphibious unmanned aerial vehicle with tiltable rotors

    ZHANG LI / AI JIANLIANG | Europäisches Patentamt | 2021

    Freier Zugriff

    Quadrotor with tiltable rotors for manned applications

    Elfeky, Mahmoud / Elshafei, Moustafa / Saif, Abdul-Wahid A. et al. | IEEE | 2014