One embodiment of the present disclosure is a unique system. Another embodiment is a unique fastener system. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines, fastener systems and other systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.


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    Titel :

    THERMALLY TUNABLE SYSTEMS


    Weitere Titelangaben:

    THERMISCH ABSTIMMBARE SYSTEME
    SYSTÈMES THERMIQUEMENT ACCORDABLES


    Beteiligte:
    PETERS JOSHUA M (Autor:in) / MUSKAT JAMES C (Autor:in)

    Erscheinungsdatum :

    21.11.2018


    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 / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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