An aircraft includes a wing which is configured to provide lift during a wing-borne mode of flight and a stoppable rotor which includes a first blade and a second blade. The stoppable rotor is configured to rotate about a vertical axis of rotation during a hover mode of flight and stop with the first blade pointing forward and the second blade pointing backward at least some of the time during the wing-borne mode of flight. The aircraft also includes a combination rotor which rotates about a longitudinal axis of rotation in a first direction at least some of the time during the hover mode of flight and in a second direction at least some of the time during the wing-borne mode of flight.
STOPPED ROTOR AIRCRAFT
2018-07-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |