An aerodynamic device includes a main aerodynamic body having a leading edge and a trailing edge, a flight control surface coupled to the main aerodynamic body near the trailing edge of the main aerodynamic body, and a rotating body coupled to the flight control surface. The rotating body is rotatable relative to the flight control surface between a stowed position and a deployed position to define a gap. The rotating body is rotated toward the main aerodynamic body while in the stowed position to close the gap. The rotating body is rotated away from the main aerodynamic body while in the deployed position to widen the gap. The gap adjusts an airflow flowing between the main aerodynamic body and the flight control surface.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotating flight control surface for aircraft


    Beteiligte:

    Erscheinungsdatum :

    09.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotating flight control surface for aircraft

    HUBBARD ANDREW J / POTTER RICHARD C | Europäisches Patentamt | 2023

    Freier Zugriff

    Actuator device for flight control surface, flight control surface of aircraft, and aircraft

    ISHIHARA KENYA | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT FLIGHT CONTROL SURFACE ACTUATOR

    VIENNOT SEVERIN / CARTRY THIERRY / LEBRUN MARC | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft flight control surface actuator

    VIENNOT SEVERIN / CARTRY THIERRY / LEBRUN MARC | Europäisches Patentamt | 2019

    Freier Zugriff

    Translating flight control surface for aircraft

    HUBBARD ANDREW J / POTTER RICHARD C | Europäisches Patentamt | 2023

    Freier Zugriff