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in the 1980s. The engine first ran in 1985 and was subsequently certified in 1987. Several variants have been developed and are currently in service with a variety of aircraft.
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166:. The D-436 incorporated an updated, higher RPM fan, a lower emissions combustor, and new compressor sections. Several variants of the engine incorporate a
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The Motor-Sich plant in
Zaporozhie, where the assembly line for D-436 engines was located, was destroyed by Russian forces in late May 2022 following the
661:
300:
The "TX" variant uses the same core at the "T3", but includes an updated turbine and a geared fan. It is in the 117–135 kN (26,000–30,000 lb
200:
The "K" variant was the initial model of the engine. It had a bypass ratio of 6.2 and a pressure ratio of 21.0. Proposed for use in the defunct
1237:
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The "T3" variant added a booster section behind the new wide-chord fan and had a maximum thrust around 93 kN (21,000 lb
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162:. The engine took several of its design features from that engine and another Progress engine, the
326:
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228:. See detailed specifications below. The variant was also proposed for use on the now-defunct
262:
The "TP" variant is a specific "maritime" corrosion-resistant version developed for use in the
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325:) of thrust. Irkut has since replaced the AI-436T12 with the 137.89 kN (31,000 lbf)
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in
Ukraine. It was initially developed to meet the requirements for late versions of the
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The "T1-134" variant was proposed as a replacement for the engines on the
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948:"MC-21 test aircraft flies with PD-14 engines after swap from PW-1400Gs"
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amphibious aircraft. This variant produces 7,500 kgf (16,534 lbf) each.
60:
437:
287:
277:
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239:
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610:"Ukraine bans deliveries of D-436 civil aircraft engines to Russia"
609:
318:
317:
This derivative engine was designed for use on the Irkut/Ilyushin
184:
167:
1031:
662:"Be-200 Indigenous Engine Delays Drive Be-12 Life Extension"
632:"Ivchenko-Progress D-436 (Ukraine), Aero-engines - Turbofan"
906:"An-148 design tweaked as date for first flight approaches"
684:"Russia Says It Destroyed Ukrainian Military Engine Plant"
483:
1,550 K (2,790 °R; 1,280 °C; 2,330 °F)
321:. It was projected to produce 117 kN (26,000 lb
248:
The "T2" variant is uprated to 80 kN (18,000 lb
290:. This version is derated to 67 kN (15,000 lb
286:
The "-148" variant was developed specifically for the
158:
The D-436 engine was developed as a follow on to the
449:: 1,500 kgf (3,307 lbf; 14.71 kN) at
1143:
1096:
1068:
453:
0.75 speed, 11,000 m (36,000 ft) altitude
445:: 7,650 kgf (16,865 lbf; 75.02 kN);
224:and has been offered for use on the in-development
717:. Vol. 143, no. 23. pp. 89–90, 92.
706:
972:Turbofan and turbojet engines: Database handbook
416:Axial flow, 1-stage fan, 6-stage IP, 7-stage HP
876:"An-148 final assembly gets under way at Kiev"
708:"Russian AWACS programs face funding problems"
276:). The T3 variant was also considered for the
1043:
495:: 10.6 g/(kN⋅s) (0.37 lb/(lbf⋅h));
8:
814:
812:
772:. 28 October – 3 November 2003. p. 57.
210:The "M" variant was proposed for use on the
499:: 17.3 g/(kN⋅s) (0.61 lb/(lbf⋅h))
1050:
1036:
1028:
601:
18:
686:. Newsweek, May 26, 2022. 26 May 2022
36:D-436-148 turbofan engine for An-148
7:
397:1.373 m (4 ft 6.1 in)
846:"India needs more power for Il-214"
825:. 23–29 November 2004. p. 61.
294:) of thrust for longer engine life.
134:developed by the Ukrainian company
1223:Ivchenko-Progress aircraft engines
797:. 1–7 September 1999. p. 73.
714:Aviation Week and Space Technology
425:1-stage HP, 1-stage IP, 3-stage LP
391:3.03 m (9 ft 11 in)
14:
705:Fricker, John (4 December 1995).
477:606.3 lb/s (275.0 kg/s)
189:A Progress D-436 installed on an
1015:
510:
385:Three-spool high-bypass turbofan
220:The "T1" variant is used on the
175:2022 Russian invasion of Ukraine
27:
950:. FlightGlobal, October 7, 2022
638:. 31 March 2009. Archived from
252:) of thrust and is used on the
909:. Paris Air Show Report 2003.
1:
937:. No. 100, September 10, 2008
935:DEFENSE and SECURITY (Russia)
403:1,450 kg (3,200 lb)
1238:Three-spool turbofan engines
1228:High-bypass turbofan engines
664:. AINonline, April 20, 2019
1254:
573:Pratt & Whitney PW6000
481:Turbine inlet temperature:
612:. Tass, February 19, 2018
488:Specific fuel consumption
366:Specifications (D-436-T1)
35:
26:
21:
975:. Elodie Roux. pp.
819:"ZMKB Progress (2004)".
590:List of aircraft engines
553:CFM International CFM56
377:General characteristics
1233:1980s turbofan engines
458:Overall pressure ratio
193:
154:Design and development
138:, and manufactured by
16:Soviet turbofan engine
1106:auxiliary power units
766:"Tu-324/414 (2003)".
558:General Electric CF34
373:Elodie Roux, page 159
188:
1024:at Wikimedia Commons
969:Élodie Roux (2007).
912:Flight International
882:Flight International
852:Flight International
822:Flight International
794:Flight International
769:Flight International
744:Flight International
256:and the Tu-334-200D.
636:Jane's Aero-Engines
525:Related development
791:"Tupolev (1999)".
747:. 8 October 1996.
547:Comparable engines
327:Aviadvigatel PD-14
194:
90:Major applications
1210:
1209:
1059:Ivchenko-Progress
1020:Media related to
885:. 15 March 2004.
855:. 29 April 2002.
642:on 14 August 2009
578:Rolls-Royce BR700
136:Ivchenko-Progress
120:
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71:Ivchenko-Progress
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132:turbofan engine
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1010:External links
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124:Progress D-436
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110:Developed from
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99:Tupolev Tu-334
95:Antonov An-148
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584:Related lists
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536:Lotarev D-136
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67:Manufacturer
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952:. Retrieved
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792:
786:
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688:. Retrieved
678:
666:. Retrieved
656:
644:. Retrieved
640:the original
635:
626:
614:. Retrieved
604:
583:
582:
546:
545:
531:Lotarev D-36
524:
523:
496:
492:
486:
480:
474:
467:Bypass ratio
465:
456:
446:
442:
435:
419:
413:
400:
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388:
382:
370:
369:
334:Applications
172:
160:Lotarev D-36
157:
130:high-bypass
128:triple-spool
123:
121:
115:Lotarev D-36
57:Soviet Union
1098:Turboshafts
430:Performance
414:Compressor:
401:Dry weight:
309:Derivatives
254:Tu-334-100D
235:D-436T1-134
73:, UMPO and
1217:Categories
1102:turboprops
596:References
408:Components
140:Motor Sich
81:First run
75:NPC Saljut
1145:Turbofans
999:804131087
921:0015-3710
891:0015-3710
861:0015-3710
831:0015-3710
803:0015-3710
778:0015-3710
753:0015-3710
723:0005-2175
646:12 August
563:IAE V2500
395:Diameter:
371:Data from
314:AI-436T12
283:D-436-148
1149:propfans
954:June 10,
616:July 29,
504:See also
436:Maximum
304:) class.
181:Variants
146:and the
45:Turbofan
493:Takeoff
443:Takeoff
421:Turbine
389:Length:
297:D-436TX
269:D-436T3
259:D-436TP
245:D-436T2
217:D-436T1
212:Yak-42M
61:Ukraine
1172:AI-322
1162:AI-222
1130:AI-450
997:
987:
919:
889:
859:
829:
801:
776:
751:
721:
497:Cruise
447:Cruise
438:thrust
288:An-148
278:Il-214
264:Be-200
240:Tu-134
230:An-174
226:Tu-414
222:Tu-334
207:D-436M
197:D-436K
22:D-436
1202:D-436
1197:D-236
1182:D-18T
1167:AI-25
1157:AI-22
1135:D-136
1125:AI-24
1120:AI-20
1108:(APU)
1088:AI-26
1083:AI-14
383:Type:
319:MC-21
168:FADEC
126:is a
84:1985
41:Type
1192:D-36
1187:D-27
1177:DV-2
1147:and
1115:AI-9
1104:and
1078:AI-4
995:OCLC
985:ISBN
956:2023
917:ISSN
887:ISSN
857:ISSN
827:ISSN
799:ISSN
774:ISSN
749:ISSN
719:ISSN
692:2022
670:2022
648:2009
618:2022
471:4.95
462:25.2
451:Mach
122:The
981:160
977:159
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983:.
879:.
849:.
811:^
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59:/
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