Ivchenko-Progress AI-222

Maximum Takeoff Thrust

24.7 kN

Bypass Ratio

1.19

Diameter

640 mm

Length

1960 mm

Dry Weight

440 kg

Thrust To Weight

5.68

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber annular
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 2	Bypass Ratio 1.19	Overall Pressure Ratio —	Afterburner Yes

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Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
TEI-TF6000	TEI	26.7	1.08	22	Compare
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HAL HTFE-25	Hindustan Aeronautics Limited	25	0.5		Compare

All data (17 fields)

Name: Ivchenko-Progress AI-222
Aircraft Engine Manufacturer: Ivchenko-Progress ZMKB
Aircraft Engine Type: Turbofan
Dry Weight (kg): 440
Diameter (mm): 640
Length (mm): 1960
Wikipedia Article (URL): en.wikipedia.org/wiki/Ivchenko-Progress_AI-222
Geared Fan: No
Combustion Chamber: annular
Afterburner: Yes
Streams: 2
Bypass Ratio: 1.19
Maximum Takeoff Thrust (kN): 24.7
Thrust To Weight: 5.68
Afterburner Thrust (kN): 24.7
Compressor Description: axial, 2-stage LP compressor and 8-stage HP compressor
Turbine Description: 1-stage HP, 1-stage LP