This disclosure is directed to hybrid tilt propeller/tilt wing aircraft. The aircraft includes a fuselage, a first wing, and a second wing. The first wing and the second wing each include a fixed inner portion and an outer portion rotatably coupled to the inner portion. The aircraft includes a first propeller and a second propeller respectively associated with the first wing and the second wing and that can respectively rotate together with the outer portion of the associated wing. The aircraft includes an third wing and a third propeller mounted to the third wing. The third wing and the third propeller can rotate with respect to the fuselage. The aircraft can control movement in all directions without cyclic control of the first propeller, the second propeller, and the third propeller.
Hybrid Tilt Propeller/Tilt Wing Aircraft
2024-07-11
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |