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    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    Neue Suche nach: MCCAFFREY MICHAEL G

    Disclosed is a gas turbine engine component, and a method for forming the component. The component includes a first portion, a second portion formed separately from the first portion, and an intermediate layer provided between the first portion and the second portion.

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    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    Neue Suche nach: MCCAFFREY MICHAEL G

    Disclosed is a gas turbine engine component, and a method for forming the component. The component includes a first portion, a second portion formed separately from the first portion, and an intermediate layer provided between the first portion and the second portion.

    Zugriff

    Download

    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    Neue Suche nach: MCCAFFREY MICHAEL G

    Disclosed is a gas turbine engine component, and a method for forming the component. The component includes a first portion, a second portion formed separately from the first portion, and an intermediate layer provided between the first portion and the second portion.

    Zugriff

    Download

    Zugriff

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    Seitennavigation

    Dokumentinformationen
    Ähnliche Titel

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    Titel:

    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    Weitere Titelangaben:

    MOTORKOMPONENTE MIT EINEM TRÄGER MIT EINER ZWISCHENSCHICHT
    COMPOSANT DE MOTEUR AYANT UN SUPPORT AVEC UNE COUCHE INTERMÉDIAIRE

    Beteiligte:

    MCCAFFREY MICHAEL G (Autor:in)

    Erscheinungsdatum:

    07.12.2016

    Medientyp:

    Patent

    Format:

    Elektronische Ressource

    Sprache:

    Englisch

    Klassifikation:

    IPC:  F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / C04B Kalk , LIME

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