A fan section to be incorporated into a gas turbine engine has a rotor and a plurality of fan blades. The fan blades deliver air into a bypass duct defined inwardly of the nacelle and into a core engine. There are static vanes inward of the nacelle. A surface of the fan section is provided with a removable film material. A gas turbine engine and a method of refurbishing a surface are also disclosed.


    Access

    Download


    Export, share and cite



    Title :

    Removable film for airfoil surfaces


    Contributors:

    Publication date :

    2019-10-29


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    AIRFOIL PROFILE FOR AN AIRCRAFT AND AERODYNAMIC SURFACES USING SAID AIRFOIL PROFILE

    ZECHERU MIHAI IOAN | European Patent Office | 2024

    Free access

    LOW DRAG REMOVABLE JOINT FOR AERODYNAMIC SURFACES

    CRUZ PALACIOS DAVID / MARTIN DE LA ESCALERA FEDERICO / CASTILLO ACERO MIGUEL ANGEL et al. | European Patent Office | 2022

    Free access

    AN AIRFOIL PROFILE FOR AN AIRCRAFT AND AERODYNAMIC SURFACES USING SAID AIRFOIL PROFILE

    ZECHERU MIHAI IOAN | European Patent Office | 2024

    Free access

    Removable transparent electrically conductive thin film

    SMITH CHARLES R | European Patent Office | 2020

    Free access

    REMOVABLE VIHICLE AIR FILM FORMATION APPARATUS

    SHIN JI HYOUN | European Patent Office | 2020

    Free access