An exemplary gas turbine engine includes a turbine section and a fan mechanically connected to the turbine section such that rotation of the turbine drives rotation of the fan. The fan includes a hub, a plurality of blade bodies extending radially outward from the hub to a first partial shroud, and a plurality of blade tips extending radially outward from the partial shroud.


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    Titel :

    Partially shrouded gas turbine engine fan


    Beteiligte:

    Erscheinungsdatum :

    14.04.2020


    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 / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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    FARB DANIEL | Europäisches Patentamt | 2020

    Freier Zugriff

    AIAA-2007-1299 AERO-THERMAL ANALYSIS OF A PARTIALLY SHROUDED AXIAL TURBINE

    Kalfas, A.I. / Porreca, L. / Abhari, R.S. et al. | British Library Conference Proceedings | 2007


    Computational Analysis of Shrouded Wind Turbine Configurations

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