A flight vehicle includes a frame, a propulsion system coupled to the frame, a first source of power coupled to the frame and configured to power the propulsion system, a traction wheel coupled to the frame and configured for tractional engagement with a ground surface during low-speed ground operation of the flight vehicle, and a second source of power coupled to the frame and configured to power to the traction wheel.


    Access

    Download


    Export, share and cite



    Title :

    SYSTEMS AND METHODS FOR ELECTRIC-POWERED FLIGHT VEHICLES


    Additional title:

    SYSTEME UND VERFAHREN FÜR ELEKTRISCH ANGETRIEBENE LUFTFAHRZEUGE
    SYSTÈMES ET PROCÉDÉS POUR VÉHICULES AÉRIENS À ALIMENTATION ÉLECTRIQUE


    Contributors:
    LOVE ROBERT (author)

    Publication date :

    2025-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen / B62K Fahrräder , CYCLES



    SYSTEMS AND METHODS FOR ELECTRIC-POWERED FLIGHT VEHICLES

    LOVE ROBERT | European Patent Office | 2024

    Free access

    SYSTEMS AND METHODS FOR ELECTRIC-POWERED FLIGHT VEHICLES

    LOVE ROBERT | European Patent Office | 2025

    Free access


    Electrically powered aerial vehicles and flight control methods

    LENG MARKUS | European Patent Office | 2016

    Free access

    Electrically powered aerial vehicles and flight control methods

    LENG MARCUS | European Patent Office | 2017

    Free access