Vertical takeoff and landing (VTOL) aircraft, especially electric VTOL (e-VTOL) aircraft include a fuselage (which may include a pair of ground-engaging skids) defining a longitudinal axis of the aircraft, forward and aft pairs of port and starboard aerodynamic wings extending laterally outwardly from the fuselage and forward and aft pairs of port and starboard rotor pods each being in substantial alignment with the longitudinal axis of the fuselage. In specific embodiments, each of the forward and aft pairs of port and starboard rotor pods comprises a forward and aft pair of rotor assemblies.


    Access

    Download


    Export, share and cite



    Title :

    Vertical take-off and landing (VTOL) aircraft



    Publication date :

    2023-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

    MOORE ANDREW DUDLEY / WILSON JOHN | European Patent Office | 2025

    Free access

    Vertical take-off and landing (VTOL) aircraft

    MOORE ANDREW DUDLEY / WILSON JOHN | European Patent Office | 2024

    Free access

    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

    MELO ADILSON / CASTELLI ALBERTO DEI / ZARONI FABIO et al. | European Patent Office | 2020

    Free access

    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

    MOORE ANDREW DUDLEY / WILSON JOHN | European Patent Office | 2020

    Free access

    VERTICAL TAKE-OFF AND LANDING AIRCRAFT (VTOL)

    YAKOVLEV VLADIMIR VASILEVICH | European Patent Office | 2018

    Free access