An aircraft nacelle air intake structure including an air intake lip with a U-shaped section to ensure air is shared between an inner face and an outer face. An acoustic panel is on the intake lip rear on the side of the inner face level with a first assembly point. An outer panel is on the intake lip rear on the side of the outer face level with a second assembly point. A front reinforcing frame on the intake lip inside is fixed to the air intake lip on the side of the inner face level with a first fixing point and on the side of the outer face level with a second fixing point. The length of the chord between the stop point and each fixing point is between ⅓ and ⅙ of the total chord between the stop point and the assembly point.


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    Titel :

    AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE


    Beteiligte:
    PORTE ALAIN (Autor:in) / HARAMBURU ERIC (Autor:in) / OBERLE PATRICK (Autor:in) / ALBET GRÉGORY (Autor:in) / BILLEROT VINCENT (Autor:in) / PIARD FRÉDÉRIC (Autor:in) / OUNDJIAN FRANCK (Autor:in)

    Erscheinungsdatum :

    19.07.2018


    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



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