A wing panel structure for an aerospace vehicle or the like may include an outer layer of material having a predetermined thickness. A core structure may be placed on at least a portion of the outer layer of material. An inner layer of material may be placed at least on the core structure. The inner layer of material may have a selected thickness less than the predetermined thickness of the outer layer of material.
WING PANEL STRUCTURE
FLÜGELPLATTENSTRUKTUR
STRUCTURE DE PANNEAU D'AILE
2019-12-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
WING PANEL STRUCTURE FOR AIRCRAFT, WING STRUCTURE, AND AIRCRAFT
Europäisches Patentamt | 2022
|WING PANEL STRUCTURE FOR AIRCRAFT, WING STRUCTURE, AND AIRCRAFT
Europäisches Patentamt | 2022
|