An adaptive wing for an aircraft includes a first wing portion, a second wing portion, and a third wing portion. The second wing portion is telescopically attached to the first wing portion to selectively change an overall length of the wing based on real-time flight conditions or airport space constraints. The third wing portion is rotate-ably attached to one end of the second wing portion, and a dihedral angle between the second wing portion and the third wing portion is changeable based on real-time flight conditions or airport space constraints.
Adaptive wing for an aircraft
18.10.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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