An aircraft and a hybrid aircraft propulsion system for the aircraft is disclosed. The aircraft has propellers and a jet engine. The propellers convert energy generated by the generator into a mechanical energy for rotating the blades and vice versa. The aircraft preferably has a configuration with left and right wing mounted propellers with electrical engines which may also function as electrical generators, a tail mounted jet engine with a coupled electrical generator, and optionally left and right wing mounted jet engines. The tail mounted jet engine is provided with air for combustion via an air intake of an S-duct type, whereby the rotor of the generator is positioned in line with the turbine shaft, therefore not disturbing airflow. A method is provided to calculate a safe flight of the aircraft, even when exclusively flying on electrical energy.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID AIRCRAFT PROPULSION


    Beteiligte:

    Erscheinungsdatum :

    06.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    HYBRID AIRCRAFT PROPULSION

    TEN HOUTEN MERIEN | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID AIRCRAFT PROPULSION

    TEN HOUTEN MERIEN | Europäisches Patentamt | 2024

    Freier Zugriff

    Hybrid Aircraft Propulsion System

    SCOTHERN DAVID P | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT HAVING HYBRID PROPULSION

    GIANNINI FRANCESCO | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT HYBRID PROPULSION SYSTEM

    VENTER GIDEON DANIEL / HARVEY GILES E | Europäisches Patentamt | 2021

    Freier Zugriff