TURBOJET ENGINE Russian patent published in 2022 - IPC F02K3/10 

FIELD: engine building.

SUBSTANCE: invention relates to internal combustion engines and can be used as a power unit on aerial vehicles. The engine comprises an inlet apparatus, a low-pressure compressor, a high-pressure compressor, an annular combustion chamber, an extension pipe, an afterburner combustion chamber, and an adjustable nozzle.

EFFECT: turbojet engine allows for safe takeoff from unpaved airfields and unprepared runway strips; event of hitting birds during takeoff and landing of the plane will not lead to the destruction of the engine; reduced dimensions of the engine and weight thereof allow for an increase in the amount of fuel on the plane.

1 cl, 3 dwg