In one embodiment, a tiltrotor aircraft (100, 200, 300, 400, 500) may comprise a fuselage (102, 202, 302, 402, 502); a biplane wing (120, 220, 320, 420, 520, 530) coupled to the fuselage (102, 202, 302, 402, 502), wherein the biplane wing (120, 220, 320, 420, 520, 530) comprises an upper wing structure (121a-b, 221a-b, 231a-b, 241a-b, 251a-b, 321, 331, 341, 421a-b) and a lower wing structure (122a-b, 222a-b, 232a-b, 242a-b, 252a-b, 322, 332, 342, 422a-b); a plurality of tiltrotors (110a-b, 210a-b, 410a-b) coupled to the biplane wing (120, 220, 320, 420, 520, 530); and at least one engine to power the plurality of tiltrotors (110a-b, 210a-b, 410a-b).
BIPLANE TILTROTOR AIRCRAFT
DOPPELDECKER-KIPPROTORFLUGZEUG
AÉRONEF À ROTORS BASCULANTS BIPLAN
2020-12-16
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |