A longitudinal control augmentation surface of aircraft, particularly turboprop/propfan aircraft with engines mounted on the rear portion of the fuselage. This longitudinal control augmentation surface is positioned in the connecting structure of the engine with the fuselage. A longitudinal control augmentation system for aircraft with engines arranged in a rear portion of the fuselage close to a vertical tail, this system comprising means of controlling the longitudinal control augmentation surfaces of the aircraft to distribute a longitudinal offset of the aircraft between these surfaces by means of functions, and an aircraft comprising the longitudinal control augmentation surface and the longitudinal control augmentation system.


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    Titel :

    AIRCRAFT LONGITUDINAL CONTROL SURFACE, LONGITUDINAL CONTROL AUGMENTATION SYSTEM FOR AIRCRAFT, AND AIRCRAFT



    Erscheinungsdatum :

    11.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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