A vertical or short takeoff and landing (V/STOL) aerial vehicle comprising: a wing having a leading edge and a trailing edge; a thrust rotor operatively coupled with the wing; and a lift rotor operatively coupled with the wing. The thrust rotor may comprise a first propeller having a first fixed axis of rotation that is substantially horizontal. The first propeller may be positioned forward of the leading edge. The lift rotor may comprise a second propeller having a second fixed axis of rotation that is substantially perpendicular to said first fixed axis of rotation. The wing may be operatively coupled with a fuselage.


    Access

    Download


    Export, share and cite



    Title :

    Double-Blown Wing Vertical Takeoff and Landing Aircraft


    Contributors:

    Publication date :

    2018-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    DOUBLE-BLOWN WING VERTICAL TAKEOFF AND LANDING AIRCRAFT

    ST CLAIR RAN D / PARKS ROBERT W / ORMISTON ROBERT | European Patent Office | 2021

    Free access

    Double-blown wing vertical takeoff and landing aircraft

    ST CLAIR RAN D / PARKS ROBERT W / ORMISTON ROBERT | European Patent Office | 2023

    Free access

    Quad-wing vertical takeoff and landing aircraft

    VILLA IAN ANDREAS / MOORE MARK / MCDONALD ROBERT ALAN et al. | European Patent Office | 2022

    Free access

    QUAD-WING VERTICAL TAKEOFF AND LANDING AIRCRAFT

    VILLA IAN ANDREAS / MOORE MARK / MCDONALD ROBERT ALAN et al. | European Patent Office | 2019

    Free access

    QUAD-WING VERTICAL TAKEOFF AND LANDING AIRCRAFT

    VILLA IAN ANDREAS / MOORE MARK / MCDONALD ROBERT ALAN et al. | European Patent Office | 2019

    Free access