A wing structure is disclosed having a first span portion including a depth that reduces in a spanwise outward direction, and a second span portion outboard of the first span portion and having a substantially uniform spanwise depth D3. The second span portion may be non-tapered, and may include parallel fore and aft spar portions. In some embodiments the non-tapered portion supports a movable wing tip device. A wing assembly and an aircraft are also disclosed.
WING ASSEMBLIES AND STRUCTURES FOR SUPPORTING WING TIP DEVICES
2023-11-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
WING ASSEMBLIES AND STRUCTURES FOR SUPPORTING WING TIP DEVICES
European Patent Office | 2023
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