Engine with front air compressor, three-stage rotary engine with continuous firing process and swiveling air jet nozzles as drive for vertical take-off aircraft

摘要

There is a "Pegasus" type rotary jet engine consisting of a front air compressor used to generate compressed air, a turbo engine as an engine that operates a front air compressor, and four steerable air jet jets for both lift and propulsion. In existing invention, a three-stage rotary engine with continuous burning of the fuel (3), which shows significant savings in weight and fuel consumption compared to the turbo engine, is used as an engine and is known from DE 10 2013 016 274.2, operates the front air compressor (1), without reducer. In order to create the conditions for more rational installation of this engine in the fuselage or wing of the aircraft and other savings. In contrast to the "Pegasus" type, the engine according to the invention has four spheroidal air jet nozzles (6) and (8), which are arranged pivotably between two pairs of spheroids by means of two crosswise ball guides (11) and (12), by the two pairs of spheroidal Air jets for buoyancy during vertical take-off, transition flights and vertical landing, as well as for propulsion. Engine, centered in the flying machine (quasi in the center of gravity) placed, without additional control systems ensures all necessary maneuvers of the aircraft by pivoting nozzles allows the entire thrust vector to turn in different directions from vertical to almost horizontal thrust in the sub-hemisphere.