The present application relates to a vortex generator (20). The present application also relates to an aircraft assembly with a hot air exhaust outlet (15). The aircraft assembly has an assembly surface over which a hot-air exhaust flow from the hot-air exhaust outlet (15) is exhausted. The aircraft assembly also has a vortex generator (20) with a flow surface (27, 28). The flow surface (27, 28) lies in an air flow over the vortex generator (20). The flow surface (27, 28) is arranged to interrupt the hot-air exhaust flow and generates a flow vortex to cool the air flow over the assembly surface.


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    Title :

    AIRCRAFT ASSEMBLY WITH A HOT-AIR EXHAUST OUTLET


    Additional title:

    FLUGZEUGANORDNUNG MIT EINEM HEISSLUFT-ABGASAUSLASS
    ENSEMBLE D'AÉRONEF COMPORTANT UNE SORTIE D'ÉCHAPPEMENT D'AIR CHAUD


    Contributors:

    Publication date :

    2022-09-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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