The invention relates to a method for assembling an aircraft pylon having a primary structure (44) and at least one internal system (60) at least partially positioned within the primary structure (44), wherein the internal system is positioned inside the primary structure before the last lateral panel of the primary structure is attached. The absence of one of the lateral panels facilitates the installation of the internal systems (60).
本发明涉及一种用于组装飞行器吊挂架的方法,所述飞行器吊挂架包括主结构(44)以及至少部分地定位在所述主结构(44)内的至少一个内部系统(60)。所述组装方法的特征在于,在附接所述主结构的最后侧向面板之前将所述内部系统定位在所述主结构内部。缺少一个所述侧向面板有助于安装所述内部系统(60)。
Method for assembling aircraft pylon
用于组装飞行器吊挂架的方法
2020-07-28
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Method of assembling aircraft pylon and aircraft pylon obtained by method
European Patent Office | 2022
|METHOD FOR ASSEMBLING AN AIRCRAFT PYLON AND AIRCRAFT PYLON OBTAINED BY THIS METHOD
European Patent Office | 2022
|Method for assembling an aircraft pylon and aircraft pylon obtained by this method
European Patent Office | 2024
|