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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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177:. 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
672:
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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
211:
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
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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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173:. The engine took several of its design features from that engine and another Progress engine, the
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239:. See detailed specifications below. The variant was also proposed for use on the now-defunct
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The "TP" variant is a specific "maritime" corrosion-resistant version developed for use in the
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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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959:"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.
71:
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621:"Ukraine bans deliveries of D-436 civil aircraft engines to Russia"
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This derivative engine was designed for use on the Irkut/Ilyushin
195:
178:
1042:
673:"Be-200 Indigenous Engine Delays Drive Be-12 Life Extension"
643:"Ivchenko-Progress D-436 (Ukraine), Aero-engines - Turbofan"
917:"An-148 design tweaked as date for first flight approaches"
695:"Russia Says It Destroyed Ukrainian Military Engine Plant"
494:
1,550 K (2,790 °R; 1,280 °C; 2,330 °F)
332:. It was projected to produce 117 kN (26,000 lb
259:
The "T2" variant is uprated to 80 kN (18,000 lb
301:. This version is derated to 67 kN (15,000 lb
297:
The "-148" variant was developed specifically for the
169:
The D-436 engine was developed as a follow on to the
460:: 1,500 kgf (3,307 lbf; 14.71 kN) at
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1107:
1079:
464:
0.75 speed, 11,000 m (36,000 ft) altitude
456:: 7,650 kgf (16,865 lbf; 75.02 kN);
235:and has been offered for use on the in-development
728:. Vol. 143, no. 23. pp. 89–90, 92.
717:
983:Turbofan and turbojet engines: Database handbook
427:Axial flow, 1-stage fan, 6-stage IP, 7-stage HP
887:"An-148 final assembly gets under way at Kiev"
719:"Russian AWACS programs face funding problems"
287:). The T3 variant was also considered for the
1054:
506:: 10.6 g/(kN⋅s) (0.37 lb/(lbf⋅h));
8:
825:
823:
783:. 28 October – 3 November 2003. p. 57.
221:The "M" variant was proposed for use on the
510:: 17.3 g/(kN⋅s) (0.61 lb/(lbf⋅h))
1061:
1047:
1039:
612:
29:
697:. Newsweek, May 26, 2022. 26 May 2022
47:D-436-148 turbofan engine for An-148
7:
408:1.373 m (4 ft 6.1 in)
857:"India needs more power for Il-214"
836:. 23–29 November 2004. p. 61.
305:) of thrust for longer engine life.
145:developed by the Ukrainian company
1234:Ivchenko-Progress aircraft engines
808:. 1–7 September 1999. p. 73.
725:Aviation Week and Space Technology
436:1-stage HP, 1-stage IP, 3-stage LP
402:3.03 m (9 ft 11 in)
25:
716:Fricker, John (4 December 1995).
488:606.3 lb/s (275.0 kg/s)
200:A Progress D-436 installed on an
1026:
521:
396:Three-spool high-bypass turbofan
231:The "T1" variant is used on the
186:2022 Russian invasion of Ukraine
38:
961:. FlightGlobal, October 7, 2022
649:. 31 March 2009. Archived from
263:) of thrust and is used on the
920:. Paris Air Show Report 2003.
1:
948:. No. 100, September 10, 2008
946:DEFENSE and SECURITY (Russia)
414:1,450 kg (3,200 lb)
1249:Three-spool turbofan engines
1239:High-bypass turbofan engines
675:. AINonline, April 20, 2019
1265:
584:Pratt & Whitney PW6000
492:Turbine inlet temperature:
623:. Tass, February 19, 2018
499:Specific fuel consumption
377:Specifications (D-436-T1)
46:
37:
32:
986:. Elodie Roux. pp.
830:"ZMKB Progress (2004)".
601:List of aircraft engines
564:CFM International CFM56
388:General characteristics
1244:1980s turbofan engines
469:Overall pressure ratio
204:
165:Design and development
149:, and manufactured by
27:Soviet turbofan engine
1117:auxiliary power units
777:"Tu-324/414 (2003)".
569:General Electric CF34
384:Elodie Roux, page 159
199:
1035:at Wikimedia Commons
980:Élodie Roux (2007).
923:Flight International
893:Flight International
863:Flight International
833:Flight International
805:Flight International
780:Flight International
755:Flight International
267:and the Tu-334-200D.
18:Progress D-436-148FM
647:Jane's Aero-Engines
536:Related development
802:"Tupolev (1999)".
758:. 8 October 1996.
558:Comparable engines
338:Aviadvigatel PD-14
205:
101:Major applications
1221:
1220:
1070:Ivchenko-Progress
1031:Media related to
896:. 15 March 2004.
866:. 29 April 2002.
653:on 14 August 2009
589:Rolls-Royce BR700
147:Ivchenko-Progress
131:
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82:Ivchenko-Progress
16:(Redirected from
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121:Developed from
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963:. Retrieved
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699:. Retrieved
689:
677:. Retrieved
667:
655:. Retrieved
651:the original
646:
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625:. Retrieved
615:
594:
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557:
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542:Lotarev D-36
535:
534:
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503:
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491:
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478:Bypass ratio
476:
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381:
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345:Applications
183:
171:Lotarev D-36
168:
141:high-bypass
139:triple-spool
134:
132:
126:Lotarev D-36
68:Soviet Union
1109:Turboshafts
441:Performance
425:Compressor:
412:Dry weight:
320:Derivatives
265:Tu-334-100D
246:D-436T1-134
84:, UMPO and
1228:Categories
1113:turboprops
607:References
419:Components
151:Motor Sich
92:First run
86:NPC Saljut
1156:Turbofans
1010:804131087
932:0015-3710
902:0015-3710
872:0015-3710
842:0015-3710
814:0015-3710
789:0015-3710
764:0015-3710
734:0005-2175
657:12 August
574:IAE V2500
406:Diameter:
382:Data from
325:AI-436T12
294:D-436-148
1160:propfans
965:June 10,
627:July 29,
515:See also
447:Maximum
315:) class.
192:Variants
157:and the
56:Turbofan
504:Takeoff
454:Takeoff
432:Turbine
400:Length:
308:D-436TX
280:D-436T3
270:D-436TP
256:D-436T2
228:D-436T1
223:Yak-42M
72:Ukraine
1183:AI-322
1173:AI-222
1141:AI-450
1008:
998:
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900:
870:
840:
812:
787:
762:
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508:Cruise
458:Cruise
449:thrust
299:An-148
289:Il-214
275:Be-200
251:Tu-134
241:An-174
237:Tu-414
233:Tu-334
218:D-436M
208:D-436K
33:D-436
1213:D-436
1208:D-236
1193:D-18T
1178:AI-25
1168:AI-22
1146:D-136
1136:AI-24
1131:AI-20
1119:(APU)
1099:AI-26
1094:AI-14
394:Type:
330:MC-21
179:FADEC
137:is a
95:1985
52:Type
1203:D-36
1198:D-27
1188:DV-2
1158:and
1126:AI-9
1115:and
1089:AI-4
1006:OCLC
996:ISBN
967:2023
928:ISSN
898:ISSN
868:ISSN
838:ISSN
810:ISSN
785:ISSN
760:ISSN
730:ISSN
703:2022
681:2022
659:2009
629:2022
482:4.95
473:25.2
462:Mach
133:The
992:160
988:159
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70:/
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