An aircraft panel (1) having two larger sides (2, 3), wherein at least one side (2, 3) has a surface with an undulated cross-sectional profile (4) comprising a first end (5) and a second end (6); at least one peak (7) and one valley (8), both between the first (5) and the second end (6) of the profile (4); and a center (9) coincident either with a peak (7) or a valley (8); wherein the distance between the center (9) and the closest peak (7) or valley (8) in a first direction (D1) defined by the center (9) and the first end (5) is equal to the distance between the center (9), and the closest peak (7) or valley (8) in a second direction (D2) defined by the center (9) and the second end (6); and wherein the panel (1) is continuous and has been manufactured as a single-piece.
PANEL FOR AN AIRCRAFT
PANEEL FÜR EIN FLUGZEUG
PANNEAU POUR AÉRONEF
2020-04-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Manufacturing method of aircraft panel and aircraft panel
European Patent Office | 2023
|AIRCRAFT PANEL SYSTEM, AIRCRAFT, AND METHOD OF OPERATING THE AIRCRAFT PANEL SYSTEM
European Patent Office | 2020
|AIRCRAFT PANEL MANUFACTURING METHOD AND AIRCRAFT PANEL MANUFACTURING SYSTEM
European Patent Office | 2017
|Aircraft panel production method and aircraft panel production system
European Patent Office | 2021
|