An aircraft nacelle comprising an air intake configured to channel an air flow in the direction of an engine assembly which comprises a fan with an axis of rotation, said air intake comprising, according to a flow direction of the air flow, a lip with a leading edge and an internal conduit which extends said lip towards the fan, wherein the air intake comprises a plurality of protrusions distributed over the circumference of the air intake and following each protrusion, a concave form configured in order to achieve compression of the air flow.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft nacelle comprising an improved air intake


    Beteiligte:

    Erscheinungsdatum :

    18.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT NACELLE COMPRISING AN IMPROVED AIR INTAKE

    ROUYRE FRANCOIS | Europäisches Patentamt | 2015

    Freier Zugriff

    NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE

    FERRIER GINA / BOILEAU PATRICK | Europäisches Patentamt | 2021

    Freier Zugriff

    Nacelle air intake and nacelle comprising such an air intake

    FERRIER GINA / BOILEAU PATRICK / CARUEL PIERRE | Europäisches Patentamt | 2023

    Freier Zugriff

    NACELLE AIR INTAKE AND NACELLE COMPRISING SUCH AN AIR INTAKE

    FERRIER GINA / BOILEAU PATRICK / CARUEL PIERRE | Europäisches Patentamt | 2022

    Freier Zugriff

    Nacelle air intake and nacelle comprising such an air intake

    FERRIER GINA / BOILEAU PATRICK | Europäisches Patentamt | 2024

    Freier Zugriff