An aircraft (10) with improved aerodynamic performances is adapted to keep the directional stability and a very good aerodynamic behavior at medium-high incidence. The aircraft (10) includes a fuselage (12) to which shaped wings (18, 20) are associated, and a nose (52). The aircraft (10) also includes a vortex control device (72) of the extension of the leading edge of the wing at the root (LERX), shaped in order to symmetrize the bursting of the vortices generated by such LERX with a medium-high incidence. Said aircraft comprises removable equipment with at least one dissipation device of incident radar waves, on at least one hot portion of the aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT WITH IMPROVED AERODYNAMIC PERFORMANCE.


    Weitere Titelangaben:

    FLUGZEUG MIT VERBESSERTER AERODYNAMISCHER LEISTUNG
    AVION AVEC PERFORMANCES AÉRODYNAMIQUES AMÉLIORÉES


    Beteiligte:

    Erscheinungsdatum :

    04.07.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft with improved aerodynamic performance

    LUCCHESINI MASSIMO / MERLO EMANUELE | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT WITH IMPROVED AERODYNAMIC PERFORMANCE

    Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft air inlet diverter assemblies with improved aerodynamic characteristics

    DA SILVA CARLOS ROBERTO ILÁRIO / RONCATTO ANDRÉ LUIS / BELÉM ANTÔNIO NUNES et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    AERODYNAMIC AIRCRAFT

    GRIGORCHUK VLADIMIR STEPANOVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    Aerodynamic performance improvement of WIG aircraft

    Tahani, Mojtaba / Masdari, Mehran / Bargestan, Ali | Emerald Group Publishing | 2017