A ram air turbine movable between a stowed position and a deployed position is provided including a rotatable hub assembly. A hub face is arranged at a first end of the rotatable hub assembly. The hub face has a non-planar configuration such that a limited portion of a surface area of the hub face is arranged within a plane oriented perpendicular to a direction of travel of an airflow upstream from the hub face when the ram air turbine is in a deployed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Ice-shedding spinner for ram air turbine



    Erscheinungsdatum :

    2018-10-16


    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 / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    ICE-SHEDDING SPINNER FOR RAM AIR TURBINE

    BORTOLI STEPHEN MICHAEL / FENELON GEOFFREY D / SEIDEL WILLIAM E et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Novel Cohesive/Adhesive Ice Shedding Model for Spinner Cone

    Chen, Y. / Fu, L. / Dong, W. | AIAA | 2017


    Gas turbine engine spinner

    KLING COLIN J / BUGAJ SHARI L / ROACH JAMES T | Europäisches Patentamt | 2019

    Freier Zugriff

    Gas Turbine Engine Spinner

    KLING COLIN J / BUGAJ SHARI L / ROACH JAMES T | Europäisches Patentamt | 2016

    Freier Zugriff

    Gas turbine engine with reinforced spinner

    ROACH JAMES T / COOK III GRANT O / KLING COLIN J et al. | Europäisches Patentamt | 2019

    Freier Zugriff