FIELD: transport.
SUBSTANCE: proposed aircraft has fuselage, wheels to run on ground attached to fuselage bottom, wings to create the lift arranged in symmetry on fuselage both sides and propellers mounted on wings and fuselage to generate the lift and traction. Said wings are attached to fuselage by means of position variators, each including multiple variable-volume chambers and volume variator arranged on one side of variable-volume chambers to adjust their expansion to allow every wing to be folded.
EFFECT: higher flight stability.
15 cl, 8 dwg
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