DRONE AIRCRAFT

摘要

FIELD: transport. ^ SUBSTANCE: invention relates to aircraft engineering. Proposed drone comprises wing with integral high-sweep leading edge and low-sweep trailing edge, twin-finned tail, rudders on the latter and tail elevens. Fins are dropped to drone mirror plane at angle ¿ to vertical exceeding 45 are jointed at tail cross-section. Tail trailing edge makes with wing leading edge the angle åëê92-95. Rudders and elevens are used as controls. ^ EFFECT: higher efficiency of controls. ^ 8 dwg