An assembly for an aircraft turbojet engine is described. The assembly includes a central gas-exhaust element and a connecting flange interposed between, upstream, a metallic outlet of a turbojet engine and, downstream, the central element. The connecting flange consists of an annular part and flexible lugs having axially: a first end where the lug is connected to the annular part, and a second free end, projecting radially outwards from the first end and towards which the lug is fixed with the central element.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    EXHAUST CONE WITH FLEXIBLE ATTACHMENT


    Beteiligte:
    CONETE ERIC (Autor:in) / CARRERE BENOIT (Autor:in)

    Erscheinungsdatum :

    2021-09-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Exhaust cone with flexible fitting

    CONETE ERIC / CARRERE BENOIT | Europäisches Patentamt | 2022

    Freier Zugriff

    EXHAUST FINISHER ATTACHMENT STRUCTURE

    KORNBLATT ANDREW S / BURNS TYLER | Europäisches Patentamt | 2019

    Freier Zugriff

    Exhaust cone heat exchanger (HEX)

    HENRIK STRÖMBERG / SONNY ANDERSSON / ANDERS LUNDBLADH | Europäisches Patentamt | 2024

    Freier Zugriff

    Exhaust finisher attachment structure

    KORNBLATT ANDREW S / BURNS TYLER | Europäisches Patentamt | 2020

    Freier Zugriff

    NOSE CONE ATTACHMENT FOR TURBOFAN ENGINE

    HALL CHRISTOPHER | Europäisches Patentamt | 2023

    Freier Zugriff