AIRCRAFT CAPABLE OF VERTICAL TAKE-OFF Russian patent published in 2019 - IPC B64C27/22 B64C27/30 

FIELD: aviation.

SUBSTANCE: invention relates to the field of aviation, in particular to the designs of multi-propeller aircrafts. Aircraft (1) comprises support structure (2) comprising at least one central fuselage (3) and two pylons (4), each of which is located sideways at a distance from fuselage (3). Aircraft (1) also comprises wing assembly (5), at least four rotors (6) and at least one propulsor (7). Each bearing screw (6) is attached to support structure (2), contains propeller (61) having two blades (62), and is intended for creation of lifting force (FV) acting on aircraft (1) in vertical direction. Propulsor (7) is intended for creation of driving force (FH) acting on supporting structure (2) in horizontal direction. Each pylon (4) contains two rotors (6), which provide stopping of corresponding blades (62) of propellers in certain position relative to pylons (4). Propellers (61) are located in pylons (4) so that they are enclosed by pylon on at least two opposite sides.

EFFECT: providing fixation of propellers in position, at which their blades do not extend beyond pylons, including at fast forward flight, which improves aerodynamic characteristics of the device.

14 cl, 6 dwg