The invention relates to an electrical energy generator system (20) for an aircraft (10), the system comprising a streamlined fairing (21) containing at least one turbine (22) housed in the front portion (21a) of the fairing (21), and an electrical energy generator (23) connected to said turbine. The front portion (21a) of the fairing (21) is fitted with air admission means (26) that are movable between an open position in which the turbine (22) is exposed to the stream of air outside the fairing (21) and a closed position in which the turbine (22) is masked inside the fairing (21). The invention serves to reduce the aerodynamic drag usually caused by turbulence present at a wing tip for a conventional wing having sharp edges during stages of takeoff, climbing, and cruising; and during stages of descent it makes it possible to recover the kinetic and potential energy that has been accumulated by the aircraft during its stages of climbing and cruising.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    A SYSTEM FOR RECOVERING AND CONVERTING KINETIC ENERGY AND POTENTIAL ENERGY AS ELECTRICAL ENERGY FOR AN AIRCRAFT


    Beteiligte:
    ROQUES SERGE (Autor:in)

    Erscheinungsdatum :

    04.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F03D Windkraftmaschinen , WIND MOTORS





    Device for converting kinetic energy into electrical energy

    EICHHORN KARL | Europäisches Patentamt | 2015

    Freier Zugriff

    ENERGY HARVESTER AND METHOD FOR CONVERTING KINETIC ENERGY TO ELECTRICAL ENERGY

    PAGET CHRISTOPHE / REHMAN MUHAMMAD ABDUL | Europäisches Patentamt | 2019

    Freier Zugriff

    Trolley capable of converting gravitational potential energy into kinetic energy

    JIA LIGANG / XIN JIANXIN / YU SHUAI et al. | Europäisches Patentamt | 2025

    Freier Zugriff