A turbofan engine defining a circumferential direction is provided. The turbofan engine includes a turbomachine; an unducted rotor assembly drivingly coupled to the turbomachine, the unducted rotor assembly including a plurality of unducted rotor blades; and a plurality of outlet guide vanes positioned downstream of the plurality of unducted rotor blades, the plurality of outlet guide vanes each defining a span, the spans of the plurality of outlet guide vanes being nonuniform along the circumferential direction.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE


    Beteiligte:

    Erscheinungsdatum :

    27.06.2024


    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Outlet guide vane assembly for turbofan engine

    RAMAKRISHNAN KISHORE / KARVI RAVISH / CARR SARAH ELIZABETH et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Outlet guide vane assembly for a turbofan engine

    RAMAKRISHNAN KISHORE / KARVE RAVISH / CARLE SARA ELIZABETH et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    The Use of Cyclic Outlet Guide Vane in Turbofan

    Joo, W.-G. / International Society for Air Breathing Engines | British Library Conference Proceedings | 1999


    Gas turbine engine outlet guide vane assembly

    BREEZE-STRINGFELLOW ANDREW / KHALID SYED ARIF | Europäisches Patentamt | 2022

    Freier Zugriff

    Turbofan with motorized rotating inlet guide vane

    KUPRATIS DANIEL BERNARD / SIDELKOVSKIY DMITRIY B / TERWILLIGER NEIL et al. | Europäisches Patentamt | 2020

    Freier Zugriff