A method for assembling a primary structure of an aircraft pylon, includes a step of fixing an angle bracket to each of the first and second lateral panels such as to obtain an L form for each of the first and second lateral panels prior to a placement of said L forms each placed against two sides of each transverse frame. This assembly technique makes it possible to reduce the mounting clearances such that it is unnecessary to fit shims, resulting in a reduction of mounting time and manufacturing costs.
PROCEDE D'ASSEMBLAGE D'UNE STRUCTURE PRIMAIRE D'UN MÂT D'AERONEF
METHOD FOR ASSEMBLING A PRIMARY STRUCTURE OF AN AIRCRAFT BEAM
VERFAHREN ZUM ZUSAMMENBAU EINER PRIMÄRSTRUKTUR EINES TRÄGERS FÜR EIN LUFTFAHRZEUG
2019-12-04
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2019
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