ROTARY GAS TURBINE ENGINE Russian patent published in 2022 - IPC F02C5/04 

FIELD: engine technology.

SUBSTANCE: invention relates to turbine construction. A rotary gas turbine engine contains a body with annular shells. There are combustion chambers, fuel supply and ignition devices. A vane wheel located in the housing with blade rings, on the ends of which flat bandage rings are fixed. Bypass channels are made in the housing. Diffusers are adjacent to the outer contour of the blade rings. Axial and centrifugal air blowers with diffusers are located at the ends of the housing, connected to the inlets made in the housing, connected to the blades made on the hub of the vane wheel. Purge holes are made in the housing partially combined with holes made in annular shells. Outlet openings with regulators are connected to horizontal nozzles, with turbines located on the shaft, with bypass channels, with fuel superchargers, with turbines located on the same shaft with air superchargers and with bypass channels on which air superchargers are installed. Vertical nozzles with regulators are located between the outlet openings with regulators. A shaft is mounted in bearings with the possibility of rotating the housing assembly, and a shaft mounted in bearings with the possibility of rotating the housing assembly with chambers made between symmetrical parts of the housing, with compressor-free engines of high-speed aircraft installed in them.

EFFECT: invention provides an increase in power, torque on the engine shaft and jet thrust, and an expansion of its applicable scope in aircraft, land, water vehicles and stationary installations.

7 cl, 14 dwg