Noise-abatement for a leading edge wing slat is provided by a noise-abatement airflow shield integral with the lower trailing edge of the slat, wherein the shield is reciprocally autonomously curveable from a substantially planar configuration when the slat is in a retracted position thereof and into a convexly curved configuration when the slat is in a deployed position thereof.


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    Titel :

    RETRACTABLE LEADING EDGE WING SLATS HAVING AUTONOMOUSLY CURVABLE AIRFLOW SHIELD FOR NOISE-ABATEMENT


    Weitere Titelangaben:

    EINZIEHBARE VORFLÜGEL MIT EINEM AUTONOM KRÜMMBAREN LUFTSTROMSCHIRM ZUR LÄRMMINDERUNG
    BECS DE BORD D'ATTAQUE RÉTRACTABLES AYANT UN DISPOSITIF D'ARRÊT DE L'ÉCOULEMENT D'AIR POUVANT ÊTRE INCURVÉ DE MANIÈRE AUTONOME POUR RÉDUIRE LE BRUIT



    Erscheinungsdatum :

    11.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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