FIELD: aviation.
SUBSTANCE: invention concerns the design of vertical take-off and landing (VTOL) aircraft. The VTOL aircraft contains a fuselage, in the nose part of which there is a variable pitch propeller, the axis of which is located along the longitudinal axis of the fuselage, equipped with a swashplate, and a high wing with flaps. At the nose of the fuselage, two control planes of the airfoil with a deflectable trailing edge are attached, performing the function of ailerons and located in the lower sector of the sweep circle of the specified propeller, also forming a parking support for the fuselage, which prevents the propeller from touching the ground.
EFFECT: simplified design, eliminated need for pre-landing evolution by pitching up and eliminated need to tilt the cabin during take-off and landing.
1 cl, 6 dwg
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