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.


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    Title :

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


    Contributors:

    Publication date :

    2023-08-08


    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 | European Patent Office | 2023

    Free access

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

    SCHENK PETER M / RODRIGUEZ RIGOBERTO / LOCASCIO DAVID | European Patent Office | 2023

    Free access

    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 Archive | 1995