A containment assembly is provided for an aircraft engine having a rotor with a set of blades. The containment assembly comprises a containment casing annularly surrounding the rotor radially outward of the set of blades. The containment casing is made of a material having a density less than that of steel. A layer of thermal insulation is disposed radially inward of the containment casing. The layer of thermal insulation is radially disposed between the containment casing and the set of blades.


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    Titel :

    CONTAINMENT ASSEMBLY FOR AN AIRCRAFT ENGINE


    Weitere Titelangaben:

    ENSEMBLE DE CONFINEMENT POUR MOTEUR D'AERONEF


    Beteiligte:

    Erscheinungsdatum :

    2023-12-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    CONTAINMENT ASSEMBLY FOR AN AIRCRAFT ENGINE

    GOVER CHRISTOPHER | Europäisches Patentamt | 2023

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