Ivchenko-Progress AI-222
The Ivchenko-Progress AI-222 (Ukrainian: AI-222, Russian: АИ-222-25) are a family of low-bypass turbofan engines.
| AI-222 | |
|---|---|
 | |
| Type | Turbofan |
| National origin | Ukraine |
| Manufacturer | Ivchenko-Progress (development) / Motor Sich (Ukraine) and FGUP Saljut (Russia) (manufacturing) |
| First run | 2003 |
| Major applications | Yakovlev Yak-130 Hongdu L-15 |
| Developed from | Progress AI-22 |
Design and development
The development of the engine started at Ivchenko-Progress of Zaporizhzhia, Ukraine in 1999. The engine was originally intended for the Yakovlev Yak-130 trainer aircraft. An after-burning version, the AI-222-25F (from Russian/Ukrainian "Форсаж", meaning reheat) is also available with thrust vectoring. In 2015 Russian manufacturer "Saljut" began to produce AI-222-25 without any Ukrainian involvement.[1]
Variants
- AI-222-25[2]
- AI-222-25F
- AI-222-25KVT
- AI-222-25KFK
- AI-222-28
- AI-222-28F
Applications
Specifications (AI-222-25)
Data from [3]
General characteristics
- Type: Two-spool low-bypass turbofan
- Length: 1,960 mm (77.17 in)
- Diameter: 640 mm (25.20 in)
- Dry weight: 440 kg (970.03 lb) in base configuration, 560 kg (1,234.59 lb) in afterburning configuration
Components
- Compressor: axial, 2-stage LP compressor and 8-stage HP compressor
- Combustors: annular
- Turbine: 1-stage HP, 1-stage LP
Performance
- Maximum thrust: 2520 kgf / 24.7 kN (5,552.78 lbf) in takeoff mode (non-afterburning), 4200 kgf / 41.2 kN (9,262.13 lbf) afterburning.
- Overall pressure ratio: 15.43:1
- Bypass ratio: 1.19:1
- Turbine inlet temperature: 1,470 K (1,200 °C)
- Specific fuel consumption: 0.66 kg/(kgf h)
- Thrust-to-weight ratio: 5.68 (non-afterburning), 7.5 (afterburning)
See also
Related development
Comparable engines
Related lists
References
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Wikimedia Commons has media related to Ivchenko-Progress AI-222. |
- http://vpk-news.ru/news/24874
- "AI-222-25". Rosoboronexport.
- "Motorsich".
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