An aircraft airfoil or wing or fuselage MODULE is fitted with a gas turbine engine driving a fan or propeller, in combination with a gaseous pressure accumulator, wherein said fan or propeller and said gaseous pressure accumulator both provide thrust, said fan thrust being provided from a rear of the MODULE via a drop-down thrust vectoring panel and said gaseous pressure accumulator thrust being provided from a fore of said MODULE, wherein the gaseous pressure accumulator is supplied with exhaust from said gas turbine engine and said exhaust is delivered downwardly at a variable angle, and said thrust vectoring panel is a panel with multiple minor panels which vector fan thrust at more than one angle. The gas turbine engine exhaust is delivered forwardly of said fan or propeller exhaust.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vertical takeoff and landing aircraft and gas turbine engine with fan thrust and exhaust thrust delivered downwardly


    Beteiligte:

    Erscheinungsdatum :

    08.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vertical takeoff and landing aircraft having a forward thrust propulsor

    MURROW KURT DAVID / ZATORSKI DAREK TOMASZ / BREEZE-STRINGFELLOW ANDREW et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    THRUST VECTORING APPARATUS FOR JET PROPULSION VERTICAL TAKEOFF AND LANDING AIRCRAFT

    KIM HYUNG OH / KIM KI BEOM | Europäisches Patentamt | 2020

    Freier Zugriff



    GAS TURBINE ENGINE FOR VERTICAL TAKEOFF AND LANDING AIRCRAFT

    TAKADA TAKEYUKI | Europäisches Patentamt | 2025

    Freier Zugriff