A leading edge structure for an aerodynamic surface of an aircraft with an outer wall part curved in a streamlined manner around an interior compartment and having an inner surface pointing toward the interior compartment and an outer surface provided for contact with the external surrounding flow. The outer wall part has a first outer wall section extending from a leading edge point in an incident flow direction in a convexly curved manner in the direction of a first side. The outer wall part has a second outer wall section which extends from the leading edge point in the incident flow direction in a convexly curved in the direction of a second side. An inner wall part is arranged in the interior compartment opposite the inner surface of the outer wall part and extends from the first outer wall section to the second outer wall section.
Leading edge structure for an aerodynamic surface of an aircraft
07.03.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LEADING EDGE STRUCTURE FOR AN AERODYNAMIC SURFACE OF AN AIRCRAFT
Europäisches Patentamt | 2021
|Aircraft Aerodynamic Surface With A Detachable Leading Edge
Europäisches Patentamt | 2017
|AIRCRAFT AERODYNAMIC SURFACE WITH A DETACHABLE LEADING EDGE
Europäisches Patentamt | 2017
|Europäisches Patentamt | 2021
|