278:
447:
258:
36:
205:
developed the PS-90 to satisfy the demands of economy, performance and exhaust emissions. It represented a huge advance over previous generations of 1960s era Soviet engines. The PS-90 is almost double the efficiency of those engines and is reasonably competitive to western engines of the 1980s such
379:. These features improve the performance and reduce maintenance costs by 40%. Fuel consumption is on par with current western engines, and its noise levels are below the current regulatory requirements. The PS-90A2 is the first Russian engine to be
416:
aircraft. It is unclear whether the US and
European components of the PS-90A2 remain or whether they have been replaced by Russian ones. If the US components have indeed been replaced, then this engine could be fitted to the
300:. For the first time, it allowed Russian airliners to achieve similar performance and economy to their western counterparts. PS-90A is rated nominally at 16000 kgf (157 kN, 35,300 lbf) thrust, 13.3% less than the
936:
269:
There are several variants: the basic PS-90A, the PS-90A-76, and the improved PS-90A versions. The latter include the PS-90A1, PS-90A2, PS-90A-42 and the PS-90A3 engines.
386:
It has the same thrust rating as the PS-90A, 16000 kgf (157 kN, 35,300 lbf) thrust. It is also capable of 18000 kgf (176 kN, 39,600 lbf) thrust.
327:, and performance will be markedly improved and noise pollution reduced to comply with the new strict requirements. With the large fleet of both civil and military
383:-180 min rated. It is offered in newly built aircraft and is completely interchangeable with the PS-90A, allowing simple upgrades on present airliners.
312:
This variant is a modification of the basic PS-90A engine. It is rated nominally up to 14,500 kgf (142 kN, 32,000 lbf) take-off thrust.
389:
Future
American involvement in engine development has been put in doubt after attempts to block sale of PS-90A2 engines to an Iranian customer.
375:. It has a fair proportion of western components from France, Germany, Sweden and the USA. It is also lighter than PS-90A and features improved
1119:
929:
1124:
922:
331:
aircraft still in operation, a potentially large market exists for engine replacement. An example of such a modified version is the
1129:
783:
409:
According to the manufacturer, it is a modification of the PS-90A2. It was certified in
January 2011 and intended to power the
359:
This variant is also a modification of the basic PS-90A engine. It was certified in 2007 and is offered as an option on the
733:"Top Managers of Pratt & Whitney and Perm Motors Group Companies Discussed PS-90A2 Aero-Engine Development Program"
822:
594:
589:
858:
844:
611:
880:
762:
711:
682:
645:
732:
579:
559:
171:
1010:
990:
218:
It incorporates many firsts in a one-of-a-kind
Russian engine with advanced technology features such as
277:
584:
1098:
1093:
1088:
1078:
1073:
970:
914:
1005:
985:
115:
372:
304:
E4 engine (which is also offered on the Tu-204), and the fuel consumption is 8.2% less than it.
599:
301:
949:
179:
65:
1068:
1058:
1048:
1043:
1038:
1033:
324:
282:
160:
808:
1028:
1020:
451:
297:
293:
175:
156:
152:
148:
136:
93:
89:
85:
909:
1113:
1083:
1063:
1053:
995:
980:
975:
965:
316:
226:
787:
945:
544:
371:
The PS-90A2 is an advanced derivative of the PS-90A, developed in cooperation with
202:
168:
164:
128:
61:
446:
957:
398:
144:
257:
140:
509:
262:
784:"ΠΠΌΠ΅ΡΠΈΠΊΠ°Π½ΡΠΊΠΈΠ΅ ΡΠ°Π½ΠΊΡΠΈΠΈ ΠΏΡΠΈΠ·Π΅ΠΌΠ»ΠΈΠ»ΠΈ Π’Ρ-204Π‘Π :: Π‘ΡΠ°ΡΡΠΈ :: Π ΠΠ daily"
422:
132:
51:
830:
518:
410:
288:
The PS-90A engine is the initial variant and is standard equipment for
20:
740:
631:
535:
418:
413:
336:
207:
872:
754:
703:
653:
19:"PS-90" redirects here. For the Belgian semi-automatic carbine, see
904:
674:
445:
380:
376:
360:
348:
344:
340:
332:
328:
320:
289:
276:
256:
236:
35:
918:
339:
is the standard on the newly built, modernized versions of the
249:
It was first certified in 1992 and has been in service since.
474:
Twin-spool high bypass turbofan with a single-stage fan
201:
With the advent of new generation of Soviet airliners,
323:, the service life of the aircraft can be extended.
1019:
956:
242:
Long service life based on on-condition maintenance
397:This is a version of the PS-90A2 intended for the
147:) thrust. It powers Russian airliners such as the
232:Acoustically treated exhaust duct for low noise
930:
8:
937:
923:
915:
437:Gas turbine PS-90GP-2 derivative of PS90A2
155:series and transport aircraft such as the
540:17,400 kgf; 38,400 lbf (171 kN)
486:1,900 mm (75 in) (fan diameter)
623:
235:Full-authority digital engine control (
222:High-bypass turbofan design for economy
245:Modular design for ease of maintenance
25:
16:1990s Russian turbofan aircraft engine
7:
632:"β russianplanes.net β Π½Π°ΡΠ° Π°Π²ΠΈΠ°ΡΠΈΡ"
910:PS-90 production list (in Russian)
14:
859:"Airliners.net - Aviation Forums"
845:"Airliners.net - Aviation Forums"
809:"PS-90A-42 turbojet aero-engine"
167:, which is the successor of the
34:
883:from the original on 2017-09-09
765:from the original on 2017-09-09
714:from the original on 2017-09-09
685:from the original on 2017-09-09
823:"PS-90A3 Engine flight-ready!"
1:
1120:Aviadvigatel aircraft engines
492:2,950 kg (6,500 lb)
480:4,964 mm (195.4 in)
1125:High-bypass turbofan engines
829:. 2011-01-28. Archived from
739:. 2007-11-15. Archived from
401:search and rescue aircraft.
159:. It is made by the Russian
905:Manufacturer specifications
174:. "PS" are the initials of
1146:
595:Pratt & Whitney PW4000
590:Pratt & Whitney PW2000
208:Pratt & Whitney PW2000
18:
461:Aviadvigatel Perm Engine.
183:
42:
33:
28:
948:, Soloviev and Shvetsov
612:List of aircraft engines
442:Specifications (PS-90A1)
225:Integrated exhaust with
675:"PS-90Π-76 Aero Engine"
580:CFM International CFM56
505:4-stage LP, 13-stage HP
466:General characteristics
1130:1990s turbofan engines
560:Thrust-to-weight ratio
523:2-stage HP, 4-stage LP
454:
425:and its subsidiaries.
285:
266:
197:Design and development
172:Soloviev Design Bureau
873:"PS-90Π1 Aero Engine"
755:"PS-90Π2 Aero Engine"
704:"PS-90Π1 Aero Engine"
600:Rolls-Royce RB211-535
449:
434:GTE-25P, GTU-25P unit
302:Rolls-Royce RB211-535
280:
260:
153:Tupolev Tu-204/Tu-214
646:"PS-90Π Aero Engine"
585:General Electric CF6
450:PS-90 mounted on an
373:Pratt & Whitney
229:for good efficiency
187:Γ‘Π²Π΅Π» ΠΠ»Π΅ΠΊΡΓ‘Π½Π΄ΡΠΎΠ²ΠΈΡ
43:Aviadvigatel PS-90
29:Aviadvigatel PS-90
574:Comparable engines
455:
294:Tupolev Tu-204-100
290:Ilyushin Il-96-300
286:
267:
125:Aviadvigatel PS-90
81:Major applications
1107:
1106:
555:0.595 kg/kgf hour
553:Fuel consumption:
315:By replacing the
121:
120:
1137:
939:
932:
925:
916:
892:
891:
889:
888:
869:
863:
862:
855:
849:
848:
841:
835:
834:
819:
813:
812:
805:
799:
798:
796:
795:
786:. Archived from
780:
774:
773:
771:
770:
751:
745:
744:
729:
723:
722:
720:
719:
700:
694:
693:
691:
690:
671:
665:
664:
662:
661:
652:. Archived from
642:
636:
635:
628:
192:
112:
105:1000 as of 2018
102:
82:
66:UEC-Perm Engines
38:
26:
1145:
1144:
1140:
1139:
1138:
1136:
1135:
1134:
1110:
1109:
1108:
1103:
1015:
952:
943:
901:
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895:
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884:
871:
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857:
856:
852:
843:
842:
838:
821:
820:
816:
807:
806:
802:
793:
791:
782:
781:
777:
768:
766:
753:
752:
748:
731:
730:
726:
717:
715:
702:
701:
697:
688:
686:
673:
672:
668:
659:
657:
644:
643:
639:
630:
629:
625:
620:
571:
530:
499:
468:
444:
431:
407:
395:
369:
357:
325:Fuel efficiency
310:
275:
255:
216:
214:Design features
199:
161:aircraft engine
135:rated at 16000
110:
100:
92:
88:
80:
24:
17:
12:
11:
5:
1143:
1141:
1133:
1132:
1127:
1122:
1112:
1111:
1105:
1104:
1102:
1101:
1096:
1091:
1086:
1081:
1076:
1071:
1066:
1061:
1056:
1051:
1046:
1041:
1036:
1031:
1025:
1023:
1021:Radial engines
1017:
1016:
1014:
1013:
1008:
1003:
998:
993:
988:
983:
978:
973:
968:
962:
960:
954:
953:
944:
942:
941:
934:
927:
919:
913:
912:
907:
900:
899:External links
897:
894:
893:
864:
850:
836:
833:on 2014-08-09.
814:
800:
775:
746:
743:on 2014-10-06.
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452:Ilyushin Il-96
443:
440:
439:
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430:
427:
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403:
394:
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368:
365:
356:
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343:, such as the
309:
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298:Tupolev Tu-214
274:
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230:
223:
215:
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198:
195:
176:Pavel Soloviev
157:Ilyushin Il-76
149:Ilyushin Il-96
119:
118:
113:
111:Developed into
107:
106:
103:
97:
96:
94:Ilyushin Il-76
90:Tupolev Tu-204
86:Ilyushin Il-96
83:
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804:
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790:on 2011-07-24
789:
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656:on 2017-09-09
655:
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606:Related lists
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514:Fully annular
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319:on the older
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227:exhaust mixer
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127:is a Russian
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58:Manufacturer
57:
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53:
50:
47:
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41:
37:
32:
27:
22:
1000:
958:Gas turbines
950:aero engines
946:Aviadvigatel
885:. Retrieved
876:
867:
853:
839:
831:the original
826:
817:
803:
792:. Retrieved
788:the original
778:
767:. Retrieved
758:
749:
741:the original
736:
727:
716:. Retrieved
707:
698:
687:. Retrieved
678:
669:
658:. Retrieved
654:the original
649:
640:
626:
605:
604:
573:
572:
558:
552:
545:Bypass ratio
543:
533:
517:
508:
502:
489:
483:
477:
471:
460:
457:
456:
429:Gas Turbines
408:
396:
388:
385:
370:
358:
314:
311:
287:
268:
248:
217:
203:Aviadvigatel
200:
188:
184:
165:Aviadvigatel
124:
122:
101:Number built
62:Aviadvigatel
877:www.avid.ru
759:www.avid.ru
708:www.avid.ru
679:www.avid.ru
650:www.avid.ru
528:Performance
503:Compressor:
490:Dry weight:
421:ordered by
399:Beriev A-42
345:Il-76MD-90A
131:commercial
129:high-bypass
1114:Categories
887:2018-05-19
794:2010-11-13
769:2018-05-19
718:2018-05-19
689:2018-05-19
660:2018-05-19
618:References
510:Combustors
497:Components
363:aircraft.
361:IL-96-400T
333:Il-76MD-90
281:PS-90A on
265:Tu-204-300
72:First run
484:Diameter:
458:Data from
393:PS-90A-42
337:PS-90A-76
308:PS-90A-76
283:MAKS-2021
263:Air Koryo
143:, 35,300
881:Archived
763:Archived
712:Archived
683:Archived
569:See also
534:Maximum
423:Iran Air
419:Tu-204SM
414:Tu-204SM
347:and the
253:Variants
163:company
151:and the
133:turbofan
52:Turbofan
827:avid.ru
737:avid.ru
519:Turbine
478:Length:
411:Tupolev
405:PS-90A3
367:PS-90A2
355:PS-90A1
349:Il-76MF
206:as the
191:ΠΎΠ»ΠΎΠ²ΡΡΠ²
180:Russian
21:FN PS90
1049:ASh-82
1044:ASh-73
1039:ASh-62
1034:ASh-21
1006:PD-18R
536:thrust
335:. The
317:D-30KP
273:PS-90A
169:Soviet
1029:ASh-2
1011:PD-30
1001:PS-90
996:PS-30
991:PS-12
986:PD-14
472:Type:
381:ETOPS
377:FADEC
341:Il-76
329:Il-76
321:Il-76
237:FADEC
139:(157
116:PD-14
75:1983
48:Type
1099:M-81
1094:M-80
1089:M-72
1084:M-71
1079:M-70
1074:M-64
1069:M-63
1064:M-25
1059:M-22
1054:M-11
981:D-30
976:D-25
971:D-21
966:D-20
296:and
123:The
564:5.9
549:5.4
261:An
193:).
145:lbf
137:kgf
1116::
879:.
875:.
825:.
761:.
757:.
735:.
710:.
706:.
681:.
677:.
648:.
351:.
292:,
210:.
182::
141:kN
64:/
938:e
931:t
924:v
890:.
861:.
847:.
811:.
797:.
772:.
721:.
692:.
663:.
634:.
562::
547::
538::
521::
512::
239:)
189:Π‘
185:Π
178:(
23:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
