Devices, systems, and methods are provided in which a wing of a tiltrotor aircraft is rotated during operational flight, for example from a position perpendicular to the aircraft's fuselage through an angle of 30° or more in the direction of flight. This effectively narrows the maximum width of the aircraft, and facilitates maneuvering through closely spaced obstacles.
Devices and methods for modifying width of rotor aircraft during operational flight
2022-06-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Devices And Methods For Modifying Width Of Rotor Aircraft During Operational Flight
European Patent Office | 2020
|DEVICES AND METHODS FOR MODIFYING WIDTH OF ROTOR AIRCRAFT DURING OPERATIONAL FLIGHT
European Patent Office | 2019
|SYSTEM AND METHOD FOR MODIFYING FLIGHT TRAJECTORY OF AIRCRAFT
European Patent Office | 2020
|Multi-rotor flight control method, flight controller and aircraft
European Patent Office | 2022
|