A galley insert (100, 200, 300) for an aircraft galley is proposed. The galley insert (100, 200, 300) comprises heating equipment (120) and an exhaust arrangement (10, 20, 30) configured to pass an exhaust air stream out of the galley insert (100, 200, 300), wherein the exhaust arrangement (10, 20, 30) comprises a plurality of deflection lamellas (11, 11a, 11b) configured to adjust a direction of the exhaust air stream. It is proposed to configure at least some of the deflection lamellas (11, 11a, 11b) such as to be angularly adjusted on the basis of a temperature of the exhaust air stream using one or more temperature-dependent actors. A corresponding method in which such a galley insert is used is also disclosed.


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    Title :

    AIRCRAFT GALLEY INSERT


    Additional title:

    FLUGZEUGBORDKÜCHENEINSATZ
    INSERT DE CUISINE D'AVION


    Contributors:

    Publication date :

    2024-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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