A leading edge structure for an aerodynamic surface of an aircraft with an outer wall part curved in a streamlined manner around an interior compartment and having an inner surface pointing toward the interior compartment and an outer surface provided for contact with the external surrounding flow. The outer wall part has a first outer wall section extending from a leading edge point in an incident flow direction in a convexly curved manner in the direction of a first side. The outer wall part has a second outer wall section which extends from the leading edge point in the incident flow direction in a convexly curved in the direction of a second side. An inner wall part is arranged in the interior compartment opposite the inner surface of the outer wall part and extends from the first outer wall section to the second outer wall section.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Leading edge structure for an aerodynamic surface of an aircraft


    Beteiligte:
    KUHLMANN GUIDO (Autor:in) / TEMMEN HUBERT (Autor:in) / SCHRÖDER RENÉ (Autor:in) / ROMBS WILHELM (Autor:in)

    Erscheinungsdatum :

    07.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LEADING EDGE STRUCTURE FOR AN AERODYNAMIC SURFACE OF AN AIRCRAFT

    KUHLMANN GUIDO / TEMMEN HUBERT / SCHRÖDER RENÉ et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft Aerodynamic Surface With A Detachable Leading Edge

    CEBOLLA GARROFE PABLO / VÉLEZ DE MENDIZABAL ALONSO IKER / CRESPO PEÑA SOLEDAD et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT AERODYNAMIC SURFACE WITH A DETACHABLE LEADING EDGE

    CEBOLLA GARROFE PABLO / VÉLEZ DE MENDIZÁBAL ALONSO IKER / CRESPO PEÑA SOLEDAD et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft leading edge structure

    LIU CHUANJUN / JIA JIALE / FANG ZHIYANG et al. | Europäisches Patentamt | 2024

    Freier Zugriff