FIELD: motors and pumps.
SUBSTANCE: ejector is designed for use in the aircraft engine industry. Ejector consists of two annular channels and an annular mixing chamber. At the exit from the annular channels and at the exit from the mixing chamber are nozzle apparatuses. Directions of the exit edges of the blades of the nozzle apparatuses located at the exit from the annular channels coincide.
EFFECT: reduction in the length of the mixing chamber.
3 cl, 3 dwg
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