AEROMOBILE OF HOVER TAKE-OFF Russian patent published in 2018 - IPC B60F5/02 B64C29/00 

FIELD: transportation.

SUBSTANCE: invention relates to transport engineering, in particular to construction of aeromobiles. Aeromobile of vertical take-off is designed according to the scheme of double fuselage and with three tandem-wings, each of which is low aspect. Lifting fuselages have wing airfoils with a relative thickness, providing the possibility of placing the cabin, the passenger cab and propulsion section. On the axis of symmetry on pylon in breaking of transverse V of the interfusel mid-wing carrying system comprising two single-bladed rotors with the opposite rotation providing only vertical take-off and landing (VTOL) and short take off and landing (STOL) is located. Pusher screws are located in annular channels integrated with the rear edges of the lifting fuselages and the interfusel aft of wing, provide the creation of control moments in implementation of VTOL and hovering and march drawing bar in high-speed forward flight with fixed blade wings of lifting propellers.

EFFECT: provides an increase in the speed and flying range, simplification of transverse handling in pitch under VTOL regimes.

6 cl, 1 dwg, 1 tbl