In a front view of this aircraft (10), there is an overlap portion (66) where at least a part of a fuselage (12) and at least a part of two cruising rotors (22) overlap, and a rear portion (12r) of the fuselage (12) has an inclined surface (68) which is displaced downward from upward progressing from the front to the rear, such that the area of the overlap portion (66) gradually becomes smaller progressing from the front to the rear.
AIRCRAFT
FLUGZEUG
AÉRONEF
2023-12-20
Patent
Elektronische Ressource
Englisch
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