View source for Engineering:Ivchenko-Progress AI-322

{{short description|Ukrainian afterburning turbofan engine}}
{|{{Infobox aircraft begin
| name = AI-322
| image = Motor Sich AI-322F engine, Kyiv 2018, 100.jpg
| caption = Ivchenko-Progress AI-322F
}}{{Infobox aircraft engine
 |type= [[Engineering:Turbofan|Turbofan]]
 |national origin= {{wipe|Ukraine}} 
 |manufacturer=
 |design group= [[Company:Ivchenko-Progress|Ivchenko-Progress]]
 |builder= [[Company:Motor Sich|Motor Sich]] 
 |design=
 |first run=
 |major applications= [[Engineering:Baykar Bayraktar Kızılelma|Baykar Bayraktar Kızılelma]]
 |produced=
 |number built=
 |developed from= [[Engineering:Ivchenko-Progress AI-222|Ivchenko-Progress AI-222]]
 |variants with their own articles=
}}
|}

The '''Ivchenko-Progress AI-322''' ({{lang-ua|AI-322}}, {{lang-ru|АИ-322}}) are a family of low-bypass [[Engineering:Turbofan|turbofan]] engines developed from the [[Engineering:Ivchenko-Progress AI-222|AI-222]] engine.

==Design and development==
The development of the engine continues at [[Company:Ivchenko-Progress|Ivchenko-Progress]] of Zaporizhzhia, {{wipe|Ukraine}}. The engine was originally intended for the [[Engineering:Hongdu L-15|Hongdu L-15]] trainer aircraft and it is now planned to be used in [[Engineering:Baykar Bayraktar Kızılelma|Baykar Bayraktar Kızılelma]] fighter UAV. An afterburning version, the AI-322F is also available.

==Variants==
;AI-322
;AI-322F

==Applications==
* [[Engineering:Baykar Bayraktar Kızılelma|Baykar Bayraktar Kızılelma]]
* [[Engineering:Hongdu L-15|Hongdu L-15]]
* [[Engineering:TAI Anka-3|TAI Anka-3]]

==Specifications (AI-322F) ==
{{jetspecs
<!-- If you do not understand how to use this template, please ask at Wikipedia talk:WikiProject Aircraft -->
<!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> -->
|ref=<ref>{{cite web |title= Motorsich AI-222-25F |url= http://motorsich.com.ua/AI-222-25F}}</ref>
|type=Two-spool [[Engineering:Bypass ratio|low-bypass]] [[Engineering:Turbofan|turbofan]]
|length={{convert|1960|mm|in|abbr=on}}
|diameter={{convert|640|mm|in|abbr=on}}
|weight={{convert|440|kg|lb|abbr=on}} in base configuration, {{convert|560|kg|lb|abbr=on}} in afterburning configuration
|compressor=axial, 2-stage LP compressor and 8-stage HP compressor
|combustion=annular
|turbine=1-stage HP, 1-stage LP
|fueltype=
|oilsystem=
|power=
|thrust= {{convert|2500|kgf|kN lbf|abbr=on|1}} in takeoff mode (non-afterburning), {{convert|4200|kgf|kN lbf|abbr=on|1}} afterburning.
|compression=15.43:1
|bypass=1.19:1
|aircon=
|turbinetemp={{convert|1470|K|C}}
|fuelcon= 0.66 kg/kgf.h (18.7 g/kNs) (non-afterburning), 1.9 kg/kgf.h (53.8 g/kNs) (afterburning)
|specfuelcon=0.66 kg/(kgf h)
|power/weight=
|thrust/weight= 5.68 (non-afterburning), 7.5 (afterburning)
}}

==See also==
{{aircontent
<!-- first, the related articles that do not fit the specific entries: -->
|see also=

<!-- designs which were developed into or from this aircraft or engine: -->
|related=
* [[Engineering:Ivchenko-Progress AI-222|Ivchenko-Progress AI-222]]

<!-- relevant lists that this engine appears in: -->
|lists=
*[[Engineering:List of aircraft engines|List of aircraft engines]]
<!-- Engines that are similar to this design: -->
|similar engines=
*[[Engineering:HAL HTFE-25|HAL HTFE-25]]
*Honeywell/ITEC F124
*[[Engineering:IHI Corporation XF5|IHI Corporation XF5]]
*[[Engineering:Lotarev DV-2|Lotarev DV-2]]
*[[Engineering:Rolls-Royce Turbomeca Adour|Rolls-Royce Turbomeca Adour]]
}}

==References==
{{Reflist}}

==External links==
*[http://motorsich.com/en/aviadvigateli/turboreaktivnye-dvuhkonturnye/ai-222-ai-322/ Motorsich AI-322 page]


[[Category:Low-bypass turbofan engines]]

{{Sourceattribution|Ivchenko-Progress AI-322}}