| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: aircraft comprises fuselage, nose horizontal empennage, tail horizontal empennage and takeoff-landing wings suspended to fuselage by suspension units with their axes located above fuselage centerline along its lengthwise axis of symmetry to turn said takeoff-landing wings. Retracted takeoff-landing wings are located under suspension units along fuselage lengthwise axis of symmetry. Outer surface of said wings makes extension of fuselage outer surface. Said wings in retracted position cover, at least, 30% of fuselage surface located between nose and tail horizontal empennages. ^ EFFECT: lower drag. ^ 7 cl, 21 dwg |
