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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    Title :

    EXHAUST ASSEMBLY WITH VORTEX GENERATOR


    Additional title:

    ABGASANLAGE MIT WIRBELERZEUGER
    ENSEMBLE D'ÉCHAPPEMENT AVEC GÉNÉRATEUR DE VORTEX


    Contributors:

    Publication date :

    2025-07-30


    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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