SWASH PLATE OF SINGLE-ROTOR AIRCRAFT AND METHOD OF ITS OPERATION Russian patent published in 2020 - IPC B64C27/24 B64C27/54 

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to design of swashplate of bearing rotor-wing of combined helicopter-aircraft. Swashplate consists of a base, to which an inner post is attached by means of bolts, on which a bearing rotating cylinder is installed by means of support bearings and a thrust bearing. On the outer side of the cylinder there is a driven gear, to which energy is supplied from the engine through the drive shaft with the drive gear. Drive shaft is located in bearings. One more drive is designed to control rotation arrest of bearing rotating cylinder. Note here that control action is transmitted to outer tray outer race and, then, to upper cage inner cage, also connected via gimbal joint with sliding bushing and tie rod to overturned wing-wing. In the central part of the blade-wing there is a turning mechanism of the overturning blade, on both sides of which there are support-thrust bearings. Blade-wing and bearing rotary cylinder are connected via blade motion bearings.

EFFECT: higher speed of horizontal flight of vertical takeoff and landing aircraft.

2 cl, 2 dwg