179:
is tasked with the manufacturing of the high-pressure compressor, combustion chamber, high-pressure turbine, air starter, air separator, start valve, air bypass valve, parts for piping, and fasteners used in the assembly of the
183:
125:
64:
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is tasked with the manufacturing of the low-pressure compressor and fan, the low-pressure turbine, middle and rear support, transmission units, engine mountings, and oil system units.
702:
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173:
is tasked with the manufacturing of external piping and cabling. It also conducts tests and performs the final assembly of the engine.
158:
A successful start of a full-size engine was made on
September 26, 2000. Further development of the engine is suspended indefinitely.
155:
design consisting of 10 modules. Materials and special coatings of parts allow the engine to operate in various climatic conditions.
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201:
The specific emissions of the engine during the landing and takeoff cycle are as follows:
8:
683:
652:
565:
170:
117:
56:
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is tasked with the manufacturing of the thrust reverser, jet nozzle, and cowlings.
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4,340 kgf (42.6 kN; 9,600 lbf) in maximum emergency mode
176:
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726:
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592:
769:
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840 kgf (8.2 kN; 1,900 lbf) in maximum cruising mode
113:
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46:
245:
ivchenko-progress.com, aviaros.narod.ru and trade.tatcenter.ru
339:
3,820 kgf (37.5 kN; 8,400 lbf) in takeoff mode
140:
The AI-22 was developed in the 1990s and is designed for the
345:
775 kgf (7.60 kN; 1,710 lbf) in cruising mode
552:
550:
166:
The AI-22 is created in a cooperation of four enterprises:
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The engine is based on a gas generator version of the
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390:125.85 kg/s (277.5 lb/s) in takeoff mode
446:
839:
16:2000s Ukrainian/Russian turbofan aircraft engine
580:
393:45.6 kg/s (101 lb/s) in cruising mode
407:1,249 °C (2,280 °F) in cruising mode
668:
404:1,450 °C (2,640 °F) in takeoff mode
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661:
248:
558:"More about the AI-22 gas turbine engine"
237:
627:"Aircraft turbojet bypass engine AI-22"
840:
656:
633:. Ivchenko-Progress. Archived from
564:. Ivchenko-Progress. Archived from
13:
848:Ivchenko-Progress aircraft engines
14:
864:
418:0.63 kg/(kgf⋅h) in cruising mode
269:1,020 mm (40 in) (fan)
218:
161:
320:
135:
1:
439:
279:
196:
7:
422:
275:765 kg (1,687 lb)
263:3,060 mm (120 in)
10:
869:
399:Turbine inlet temperature:
768:
721:
693:
414:Specific fuel consumption
257:Two-spool turbofan engine
21:
434:List of aircraft engines
297:Annular with 16 nozzles
249:General characteristics
853:2000s turbofan engines
362:19.16 in cruising mode
352:Overall pressure ratio
238:Specifications (AI-22)
731:auxiliary power units
631:ivchenko-progress.com
562:ivchenko-progress.com
379:4.57 in cruising mode
359:15.49 in takeoff mode
116:engine, developed by
376:4.94 in takeoff mode
288:Fan & 5LP + 7HP
144:regional airliner.
78:September 26, 2000
509:trade.tatcenter.ru
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684:Ivchenko-Progress
151:engine. It has a
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687:aircraft engines
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597:aviaros.narod.ru
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511:. Archived from
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312:T-1, TS-1 or RT
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231:Yakovlev Yak-48
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38:National origin
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22:Progress AI-22
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695:Piston engines
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505:"AI-22 engine"
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385:Air mass flow:
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225:Tupolev Tu-324
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177:Motor Sich JSC
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142:Tupolev Tu-324
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122:Motor Sich JSC
110:Progress AI-22
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96:Developed into
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84:Developed from
80:
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61:Motor Sich JSC
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637:on 2012-05-29
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568:on 2012-05-12
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515:on 2009-07-13
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428:Related lists
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213:
211:NOx = 45 g/kN
210:
207:
205:CO = 110 g/kN
204:
203:
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171:ZMKB Progress
169:
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53:Manufacturer
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639:. Retrieved
635:the original
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600:. Retrieved
596:
570:. Retrieved
566:the original
561:
517:. Retrieved
513:the original
508:
427:
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412:
398:
384:
369:Bypass ratio
367:
350:
326:
309:
300:
291:
285:
272:
266:
260:
254:
242:
241:
219:Applications
214:SN = 20 g/kN
208:HC = 12 g/kN
200:
165:
162:Organisation
157:
146:
139:
109:
107:
723:Turboshafts
321:Performance
286:Compressor:
273:Dry weight:
136:Development
842:Categories
727:turboprops
641:15 October
602:21 October
572:15 October
519:2 November
440:References
310:Fuel type:
293:Combustors
280:Components
233:(proposed)
227:(proposed)
75:First run
770:Turbofans
316:type fuel
306:1HP + 3LP
267:Diameter:
243:Data from
197:Emissions
774:propfans
423:See also
327:Maximum
314:kerosene
114:turbofan
31:Turbofan
593:"AI-22"
302:Turbine
261:Length:
180:engine.
153:modular
43:Ukraine
797:AI-322
787:AI-222
755:AI-450
329:thrust
101:AI-222
47:Russia
827:D-436
822:D-236
807:D-18T
792:AI-25
782:AI-22
760:D-136
750:AI-24
745:AI-20
733:(APU)
713:AI-26
708:AI-14
255:Type:
112:is a
27:Type
817:D-36
812:D-27
802:DV-2
772:and
740:AI-9
729:and
703:AI-4
643:2021
604:2021
574:2021
521:2021
190:KAPO
184:KMPO
149:DV-2
130:KAPO
128:and
126:KMPO
108:The
89:DV-2
69:KAPO
65:KMPO
844::
629:.
612:^
595:.
582:^
560:.
529:^
507:.
448:^
132:.
124:,
120:,
67:,
63:,
59:,
45:,
725:/
676:e
669:t
662:v
645:.
606:.
576:.
523:.
416::
371::
354::
331::
304::
295::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.