AIRCRAFT WITH BLADE DEVICES Russian patent published in 2016 - IPC B64C29/00 B64C27/28 

FIELD: aircraft engineering.

SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft heavier than the air. Aircraft comprises two blade devices installed on a common shaft on opposite sides and at a required distance from the fuselage, an engine to drive the blade devices, a fuselage for attachment and arrangement of units composing the aircraft with the blade devices. Common rotary shaft is articulated with drive shafts of the blade devices. Tail fin is represented by a vertical and a horizontal planes. Control system of the aircraft with blade devices changes the position of the blade devices relative to the horizontal surface, the position of the blade devices relative to each other, the position of the blade devices guide flows, the position of vertical and horizontal planes of the tail fin relative to the fuselage, varies the speed of the blade devices blades movement depending on the engine output shaft angular speed. Blade devices comprise protective outer casings.

EFFECT: provided is higher safety of the aircraft operation.

1 cl, 12 dwg