AIRCRAFT WITH THE POSSIBILITY OF HIGH ACCELERATIONS, FUEL SAVING, STABILITY DUE TO ROTARY PULSE JET ENGINES AND DISPLACEMENTS OF THE CENTRE OF MASS Russian patent published in 2016 - IPC B64C39/06 B64C29/00 

FIELD: aircraft engineering.

SUBSTANCE: invention relates to aviation and space, particularly to aircraft engines. Aircraft comprises an engine, a chute with two masses M1, M2 on the ends adjacent in the center with a shaft and a planetary reduction gear. Shaft with the reduction gear is also coupled with the second chute with two masses M3, M4 on the ends via a clutch gear. Shaft is coupled through the second clutch gear with a capsule able to be displaced normally to the axis of rotation and rigidly coupled with the housing and through a bearing with the shaft. Aircraft is additionally equipped with four jet (rocket) engines and two closed toroid-shape chambers with holes of about 45°-90° along the perimeter in the rear part of the chambers.

EFFECT: provided is the possibility to take off from any sites.

7 cl, 4 dwg