A stiffened structural component for an aircraft comprises a first material sheet with a first surface, and at least one elongate bulge that bulges out in a direction transverse to the first surface in order to stiffen the structural component, wherein each of the at least one bulge comprises two edges that extend along the first surface, wherein a continuous bulging surface extends between the edges, and wherein the bulges are formed integrally into the first material sheet through pressing.
一种用于飞行器的加强结构部件,所述加强结构部件包括:具有第一表面的第一材料片材,以及至少一个长形凸起,所述至少一个长形凸起在横向于所述第一表面的方向上凸出,以便加强所述结构部件,其中,所述至少一个凸起中的每一个凸起包括两个边缘,所述边缘沿所述第一表面延伸,其中,连续的凸起表面在所述边缘之间延伸,并且其中,所述凸起通过压制一体地成形于所述第一材料片材中。
A STIFFENED STRUCTURAL COMPONENT FOR AN AIRCRAFT
用于飞行器的加强结构部件
09.10.2020
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Method for manufacturing a stiffened structural panel for an aircraft
Europäisches Patentamt | 2022
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