A leading-edge device for an aerodynamic component is disclosed having a first skin element having an inner surface and an aerodynamic outer surface, and further includes a second skin element having an inner surface and an aerodynamic outer surface. The leading-edge device includes a first coupling element protruding from the inner surface of the first skin element and a second coupling element protruding from the inner surface of the second skin element. The first and second coupling elements are coupled to each other in a coupling region. The first skin element and the first coupling element are formed as a single-piece structure.
LEADING EDGE DEVICE FOR AN AERODYNAMIC COMPONENT AND METHOD FOR MANUFACTURING A LEADING-EDGE DEVICE FOR AN AERODYNAMIC COMPONENT
27.03.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2024
|Europäisches Patentamt | 2021
|Leading edge buckling due to aerodynamic heating
SLUB | 1960
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