Las fuerzas aeroespaciales
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AI-222-25
Aircraft engine

The two-shaft turbofan aircraft engine consists of a two-stage low-pressure compressor manufactured using "blisk" technology (the blades are made integral with disk), an 8-stage high-pressure compressor, an annular combustion chamber, a single-stage LP turbine and a single-stage HP turbine, and a nozzle. The engine has a bottom-mounted accessory gear box.

The engine is designed to power the Yak-130 training aircraft.


Principales características
Max thrust, kgf
2500
Length, mm
2317
Inlet diameter, mm
624
Specific fuel consumption, kg/h
0,64+2%
Dry weight, kg
440+2%
etiquetas: AI-222-25, Engines,