| 摘要 |
FIELD: aviation. ^ SUBSTANCE: invention is related to aerospace equipment, namely, to design of aircraft bearing unit. Bearing unit of aircraft (1st version) includes jet or hybrid jet-rocket engine equipped with slotted nozzle, wing located behind slotted nozzle in zone of gas flow action that washes wing panels and suspended on engine body by means of horizontal hinged joints with the possibility to vary angle of wing attack relative to direction of gas flow, to create controlled lifting force of bearing unit. Aircraft bearing unit (2nd version) includes hybrid engine and wing, at that engine is equipped with four opposite slotted nozzles and is installed inside annular wing split into four segments, with the possibility to vary angle of segments attack relative to direction of gas flow to create lifting force that transports apparatus only in vertical direction. Bearing unit is equipped with two supply systems that provide for engine operation on kerosene and oxygen, and also on rocket fuel with oxidant for flight in airless space. ^ EFFECT: creation of additional lifting force of aircraft in conditions of rarefied atmosphere or in airless space. ^ 4 cl, 3 dwg |
