The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT WITH RAM AIR TURBINE DISK WITH GENERATOR HAVING BLADE SHROUD RING INTEGRATED MAGNETS


    Beteiligte:

    Erscheinungsdatum :

    2023-11-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    Aircraft with ram air turbine disk with generator having blade shroud ring integrated magnets

    SCHENK PETER M / RODRIGUEZ RIGOBERTO / LOCASCIO DAVID | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT WITH RAM AIR TURBINE DISK WITH GENERATOR HAVING BLADE TIP INTEGRATED MAGNETS

    SCHENK PETER M / RODRIGUEZ RIGOBERTO / LOCASCIO DAVID | Europäisches Patentamt | 2023

    Freier Zugriff

    Turbine Blade Platform, Blade Tip and Shroud Heat Transfer

    Dunn, M. G. / Kim, J. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995



    Turbine blade platform, blade tip and shroud heat transfer

    Dunn, M.G. / Kim, J. | Tema Archiv | 1995