A method for assembling an aircraft pylon including a primary structure and at least one internal system positioned at least partially within the primary structure, wherein the assembly method includes a first step of assembling a part of the primary structure so that the interior of the primary structure remains accessible, a step of mounting an internal systems module including at least one support and at least one internal system connected to the support, a second step of assembling the internal systems module and the partially assembled primary structure, a third step of assembling any element of the primary structure not assembled in the first assembly step, and an aircraft pylon assembled by such a method.
PROCÉDÉ D'ASSEMBLAGE D'UN MÂT D'AÉRONEF ET MÂT D'AÉRONEF OBTENU À PARTIR DE CE PROCÉDÉ
ASSEMBLING METHOD FOR AN AIRCRAFT PYLON AND AIRCRAFT PYLON OBTAINED BY THIS METHOD
MONTAGEVERFAHREN FÜR EINEN FLUGZEUGMAST UND FLUGZEUGMAST ERHALTEN DURCH DIESES VERFAHREN
2023-11-08
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
PROCEDE D'ASSEMBLAGE D'UNE STRUCTURE PRIMAIRE D'UN MÂT D'AERONEF
European Patent Office | 2019
|European Patent Office | 2019
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