The invention relates to an exhaust assembly (30) for a turbine engine, turbine engine and method of exhausting combustion gas. The exhaust assembly (30) comprising an exhaust conduit comprising a reverse flow portion, said reverse flow portion (44) defining a turn (46) with an interior (48), wherein the reverse flow portion (44) comprises an exhaust stub (32,132) extending from an exhaust collector (38,138) to an exhaust outlet (36,136) defining the exhaust conduit (47) and forming the turn (46,146), characterized in that it further comprises snorkels (168) being small pipes, placed into the exhaust stubs (132) downstream of where the exhaust stub (132) couples to the exhaust collector (138), the snorkel (168) connecting an anti-ice scoop (160) to a conduit (166) of the anti-ice system (164).


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    Titel :

    EXHAUST ASSEMBLY WITH VORTEX GENERATOR


    Weitere Titelangaben:

    ABGASANLAGE MIT WIRBELERZEUGER
    ENSEMBLE D'ÉCHAPPEMENT AVEC GÉNÉRATEUR DE VORTEX


    Beteiligte:

    Erscheinungsdatum :

    30.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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