A method for manufacturing an air-intake structure for a turbojet-engine nacelle includes two component parts, i.e. one air-intake lip structure and one outer cowl for the air-intake structure. In particular, the method includes the following steps: separately manufacturing the component parts such that each integrates one overlapping portion with a part to which is to be attached. The overlapping portion is configured such that an outer surface of the outer overlapping portion provides continuity with an outer surface of the outer cowl associated with the inner overlapping portion. To secure the overlapping portions, glue or a fastener may be used.


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    Title :

    PROCÉDÉ DE FABRICATION D'UNE STRUCTURE D'ENTRÉE D'AIR DE NACELLE DE TURBORÉACTEUR


    Additional title:

    METHOD FOR MANUFACTURING AN AIR-INTAKE STRUCTURE FOR A TURBOJET-ENGINE NACELLE
    VERFAHREN ZUR HERSTELLUNG EINER LUFTEINLASSSTRUKTUR FÜR EINE TURBODÜSENMOTORGONDEL


    Contributors:

    Publication date :

    2018-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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