A fan section for a gas turbine engine includes a fan hub having blade slots for receiving a root of a fan blade. A lock ring is configured to move rotatably from an unlocked position to a locked position for securing the blade root in the blade slot. A nose cone is secured to the lock ring, and thereby secured to the fan section.


    Access

    Download


    Export, share and cite



    Title :

    GAS TURBINE ENGINE NOSE CONE ATTACHMENT


    Additional title:

    NASENHAUBENBEFESTIGUNG FÜR GASTURBINENMOTOR
    FIXATION DE CÔNE DE NEZ DE TURBINE À GAZ


    Contributors:

    Publication date :

    2021-06-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    NOSE CONE ATTACHMENT FOR TURBOFAN ENGINE

    HALL CHRISTOPHER | European Patent Office | 2020

    Free access

    NOSE CONE ATTACHMENT FOR TURBOFAN ENGINE

    HALL CHRISTOPHER | European Patent Office | 2018

    Free access

    Nose cone attachment for turbofan engine

    HALL CHRISTOPHER | European Patent Office | 2020

    Free access

    GAS TURBINE ENGINE NOSE CONE ASSEMBLY

    HARNER JOHN / MCPHAIL JAMES J | European Patent Office | 2020

    Free access

    Gas turbine engine nose cone assembly

    HARNER JOHN / MCPHAIL JAMES J | European Patent Office | 2021

    Free access