An Unmanned Aerial Vehicle (UAV) has a fuselage, a rotor system, and a wing configured for selective positioning during flight of the UAV to a fully deployed position, a fully stowed position, and to positions between the fully deployed position and the fully stowed position.
UAV with In-Flight Adjustable Wings
13.12.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
NTIS | 1994
NTIS | 1994