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.
PROCÉDÉ DE FABRICATION D'UNE STRUCTURE D'ENTRÉE D'AIR DE NACELLE DE TURBORÉACTEUR
METHOD FOR MANUFACTURING AN AIR-INTAKE STRUCTURE FOR A TURBOJET-ENGINE NACELLE
VERFAHREN ZUR HERSTELLUNG EINER LUFTEINLASSSTRUKTUR FÜR EINE TURBODÜSENMOTORGONDEL
2018-03-28
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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