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    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    New search for: 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

    New search for: 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.

    Access

    Download

    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    New search for: 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.

    Access

    Download

    Access

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    Document information
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    Document information
    Title:

    ENGINE COMPONENT HAVING SUPPORT WITH INTERMEDIATE LAYER

    Additional title:

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

    Contributors:

    MCCAFFREY MICHAEL G (author)

    Publication date:

    2016-12-07

    Type of media:

    Patent

    Type of material:

    Electronic Resource

    Language:

    English

    Classification:

    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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