A system for an aircraft (20) includes a vane (54) and an air system (32). The air system (32) includes a first air circuit (86A) and a first door assembly (88A). The first air circuit (86A) extends in the vane (54) to a first circuit outlet (92A) at a first side (70A) of the vane (54). The first door assembly (88A) is arranged at the first circuit outlet (92A). The air system (32) is configured to exhaust a flow of air out of the first air circuit (86A) through the first circuit outlet (92A) during a first mode and a second mode. The first door assembly (88A) is configured to direct the flow of air exhausted from the first circuit outlet (92A) longitudinally towards a leading edge (66) of the vane (54) during the first mode. The first door assembly (88A) is configured to direct the flow of air exhausted from the first circuit outlet (92A) longitudinally towards a trailing edge (68) of the vane (54) during the second mode.


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    Title :

    AIRCRAFT AIRFRAME COMPONENT WITH AIR SYSTEM


    Additional title:

    FLUGZEUGFLUGWERKKOMPONENTE MIT LUFTSYSTEM
    COMPOSANT DE CELLULE D'AÉRONEF AVEC SYSTÈME D'AIR


    Contributors:

    Publication date :

    2025-07-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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