An air intake for a nacelle of an aircraft propulsion assembly includes an upstream section that defines an air intake flow path, a central section surrounding a fan of an engine, and a downstream section surrounding a combustion chamber of the engine. The air intake includes a disassembly mechanism which has a panel able to move between a flush closed position in which the panel provides aerodynamic continuity of the air intake in the air intake flow path, and an open maintenance position in which the panel is radially and outwardly retracted in relation to its flush closed position in order to free up a space which allows removal of a blade of the fan at its distal end.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT NACELLE AND ASSOCIATED AIR INTAKE


    Beteiligte:

    Erscheinungsdatum :

    05.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE

    PORTE ALAIN / LALANE JACQUES / OUNDJIAN FRANCK | Europäisches Patentamt | 2018

    Freier Zugriff

    Air intake structure for an aircraft nacelle

    PORTE ALAIN / HARAMBURU ERIC / OBERLE PATRICK et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT NACELLE COMPRISING AN IMPROVED AIR INTAKE

    ROUYRE FRANCOIS | Europäisches Patentamt | 2015

    Freier Zugriff

    Intake duct for aircraft turbine engine nacelle

    LANCLERC ALEXIS YVES MARIE / VALLEROY LAURENT GEORGES | Europäisches Patentamt | 2022

    Freier Zugriff

    NACELLE INTAKE

    QIN NING / SHAHPAR SHAHROKH / SMITH ANGUS et al. | Europäisches Patentamt | 2020

    Freier Zugriff