Methods are provided forming a metallic nacelle inlet structure for a turbine engine aircraft propulsion system with an axis. The nacelle inlet structure includes an inlet lip portion and an outer barrel portion. One of the method may include steps of: forming the inlet lip portion; forming the outer barrel portion; arranging the inlet lip portion axially adjacent the outer barrel portion; and friction stir welding the inlet lip portion to the outer barrel portion to provide a circumferentially extending weld joint between the inlet lip portion and the outer barrel portion.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FORMING A NACELLE INLET FOR A TURBINE ENGINE PROPULSION SYSTEM


    Beteiligte:
    BROWN KEITH T (Autor:in) / PUJAR VIJAY V (Autor:in) / HAYES RUSTY (Autor:in) / ROSE DAVID L (Autor:in)

    Erscheinungsdatum :

    2017-04-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B23K Löten , SOLDERING OR UNSOLDERING / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    FORMING A NACELLE INLET FOR A TURBINE ENGINE PROPULSION SYSTEM

    BROWN KEITH T / PUJAR VIJAY V / HAYES RUSTY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Forming a nacelle inlet for a turbine engine propulsion system

    BROWN KEITH T / PUJAR VIJAY V / HAYES RUSSELL B et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Inlet part of aero-engine nacelle and aero-engine nacelle

    BAI JIE / YU TIANHONG / HE YUJUN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Air inlet channel of aero-engine nacelle and aero-engine nacelle

    DA YUBAO / ZHOU SONGPING / SUN LIBING | Europäisches Patentamt | 2022

    Freier Zugriff

    NACELLE WITH A TRANSLATABLE INLET FOR AN AIRCRAFT PROPULSION SYSTEM

    COCHRAN MICHAEL | Europäisches Patentamt | 2022

    Freier Zugriff