An aircraft is provided which includes a fuselage having a first wing with curved wingtips positioned above a second wing having curved wingtips. Rotor assemblies located in between the curved wingtips of the first and second wing, are employable to both provide vertical thrust for vertical take off of the aircraft and auto rotation to generate electric energy to recharge an onboard electric power supply. The first wing may be formed in a V-shape, and additional rotor assemblies to provide forward and vertical thrust to the airplane can be included on rotatable canards.


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    Title :

    Aircraft with Wingtip Positioned Propellers


    Contributors:

    Publication date :

    2023-12-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft with wingtip positioned propellers

    RUSS JONATHAN CHRISTIAN | European Patent Office | 2022

    Free access

    AIRCRAFT WITH WINGTIP POSITIONED PROPELLERS

    RUSS JONATHAN CHRISTIAN | European Patent Office | 2021

    Free access

    Aircraft with Wingtip Positioned Propellers

    RUSS JONATHAN CHRISTIAN | European Patent Office | 2022

    Free access

    AIRCRAFT WITH WINGTIP POSITIONED PROPELLERS

    RUSS JONATHAN CHRISTIAN | European Patent Office | 2021

    Free access

    Aircraft with wingtip positioned propellers

    RUSS JONATHAN CHRISTIAN | European Patent Office | 2023

    Free access