FIELD: aviation.
SUBSTANCE: invention relates to structures of aircraft bearing systems. Bearing system of vertical takeoff and landing aircraft consists of air blower, air flow guide, two and more wings of aerodynamic profile, horizontal and vertical steering surfaces. Said aerofoil wing comprises a ledge on upper surface to provide pressure reduction over wing top surface, and crosswise relative to wing rib profile on wing lower surface to obtain increased air pressure under wing bottom surface.
EFFECT: reduced weight and overall dimensions of vertical lift takeoff and landing aircraft bearing system.
2 cl, 3 dwg
