The Progress D-436 is a three-shaft high by-pass turbofan engine developed by the Ukrainian company Ivchenko-Progress, and manufactured by Motor Sich in Ukraine.[1] It was initially developed to meet the requirements for late versions of the Yakovlev Yak-42 and the Antonov An-72 in the 1980s. The engine first ran in 1985 and was subsequently certified in 1987.[2] Several variants have been developed and are currently in service with a variety of aircraft.
The D-436 engine was developed as a follow on to the Lotarev D-36. The engine took several of its design features from that engine and another Progress engine, the Progress D-18. The D-436 incorporated an updated, higher RPM fan, a lower emissions combustor, and new compressor sections. Several variants of the engine incorporate a FADEC.
The Motor-Sich plant in Zaporozhie, where the assembly line for D-436 engines was located,[3] was destroyed by Russian forces in late May 2022 following the 2022 Russian invasion of Ukraine.[4]
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 Antonov An-71.[5]
D-436M
The "M" variant was proposed for use on the Yak-42M.[6]
D-436T1
The "T1" variant is used on the Tu-334 and has been offered for use on the in-development Tu-414.[7] See detailed specifications below. The variant was also proposed for use on the now-defunct An-174.
D-436T1-134
The "T1-134" variant was proposed as a replacement for the engines on the Tu-134.
D-436T2
The "T2" variant is uprated to 80 kN (18,000 lbf) of thrust and is used on the Tu-334-100D and the Tu-334-200D.[8]
D-436TP
The "TP" variant is a specific "maritime" corrosion-resistant version developed for use in the Be-200 amphibious aircraft. This variant produces 7,500 kgf (16,534 lbf) each.
D-436T3
The "T3" variant added a booster section behind the new wide-chord fan and had a maximum thrust around 93 kN (21,000 lbf).[9] The T3 variant was also considered for the Il-214, but the aircraft's thrust requirements exceeded the max engine thrust of 98 kN (22,000 lbf).[10]
D-436-148
The "-148" variant was developed specifically for the An-148.[11] This version is derated to 67 kN (15,000 lbf) of thrust for longer engine life.[12]
D-436TX
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 lbf) class.[9]
Derivativesedit
AI-436T12
This derivative engine was designed for use on the Irkut/Ilyushin MC-21. It was projected to produce 117 kN (26,000 lbf) of thrust.[13] Irkut has since replaced the AI-436T12 with the 137.89 kN (31,000 lbf) Aviadvigatel PD-14.[14][15]
Wikimedia Commons has media related to Progress D-436.
Notesedit
^"Ukraine bans deliveries of D-436 civil aircraft engines to Russia". Tass, February 19, 2018. Retrieved July 29, 2022.
^. 31 March 2009. Archived from the original on 14 August 2009. Retrieved 12 August 2009. {{cite encyclopedia}}: |work= ignored (help); Missing or empty |title= (help)
^"Be-200 Indigenous Engine Delays Drive Be-12 Life Extension". AINonline, April 20, 2019. Retrieved September 19, 2022.
^"Russia Says It Destroyed Ukrainian Military Engine Plant". Newsweek, May 26, 2022. Retrieved September 19, 2022.
^Fricker, John (4 December 1995). "Russian AWACS programs face funding problems". Aviation Week and Space Technology. Vol. 143, no. 23. pp. 89–90, 92. ISSN 0005-2175.
^"An-148 final assembly gets under way at Kiev". Flight International. 15 March 2004. ISSN 0015-3710.
^"An-148 design tweaked as date for first flight approaches". Paris Air Show Report 2003. Flight International. 23 June 2003. ISSN 0015-3710.
^ENGINES (2008). DEFENSE and SECURITY (Russia). No. 100, September 10, 2008
^"Irkut Removes Pratt & Whitney Engine Option From The MC-21". SimpleFlying, April 25, 2022. Retrieved June 10, 2023.
^"MC-21 test aircraft flies with PD-14 engines after swap from PW-1400Gs". FlightGlobal, October 7, 2022. Retrieved June 10, 2023.
^Élodie Roux (2007). Turbofan and turbojet engines: Database handbook. pp. 159–160. ISBN9782952938013. OCLC 804131087.
November 15, 2023
progress, three, shaft, high, pass, turbofan, engine, developed, ukrainian, company, ivchenko, progress, manufactured, motor, sich, ukraine, initially, developed, meet, requirements, late, versions, yakovlev, antonov, 1980s, engine, first, 1985, subsequently, . The Progress D 436 is a three shaft high by pass turbofan engine developed by the Ukrainian company Ivchenko Progress and manufactured by Motor Sich in Ukraine 1 It was initially developed to meet the requirements for late versions of the Yakovlev Yak 42 and the Antonov An 72 in the 1980s The engine first ran in 1985 and was subsequently certified in 1987 2 Several variants have been developed and are currently in service with a variety of aircraft D 436D 436 148 turbofan engine for An 148Type TurbofanNational origin Soviet Union UkraineManufacturer Ivchenko Progress UMPO and NPC SaljutFirst run 1985Major applications Antonov An 148Tupolev Tu 334Beriev Be 200Developed from Lotarev D 36 Contents 1 Design and development 2 Variants 2 1 Derivatives 3 Applications 4 Specifications D 436 T1 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 6 1 NotesDesign and development editThe D 436 engine was developed as a follow on to the Lotarev D 36 The engine took several of its design features from that engine and another Progress engine the Progress D 18 The D 436 incorporated an updated higher RPM fan a lower emissions combustor and new compressor sections Several variants of the engine incorporate a FADEC The Motor Sich plant in Zaporozhie where the assembly line for D 436 engines was located 3 was destroyed by Russian forces in late May 2022 following the 2022 Russian invasion of Ukraine 4 Variants edit nbsp A Progress D 436 installed on an Antonov An 158D 436K 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 Antonov An 71 5 D 436M The M variant was proposed for use on the Yak 42M 6 D 436T1 The T1 variant is used on the Tu 334 and has been offered for use on the in development Tu 414 7 See detailed specifications below The variant was also proposed for use on the now defunct An 174 D 436T1 134 The T1 134 variant was proposed as a replacement for the engines on the Tu 134 D 436T2 The T2 variant is uprated to 80 kN 18 000 lbf of thrust and is used on the Tu 334 100D and the Tu 334 200D 8 D 436TP The TP variant is a specific maritime corrosion resistant version developed for use in the Be 200 amphibious aircraft This variant produces 7 500 kgf 16 534 lbf each D 436T3 The T3 variant added a booster section behind the new wide chord fan and had a maximum thrust around 93 kN 21 000 lbf 9 The T3 variant was also considered for the Il 214 but the aircraft s thrust requirements exceeded the max engine thrust of 98 kN 22 000 lbf 10 D 436 148 The 148 variant was developed specifically for the An 148 11 This version is derated to 67 kN 15 000 lbf of thrust for longer engine life 12 D 436TX 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 lbf class 9 Derivatives edit AI 436T12 This derivative engine was designed for use on the Irkut Ilyushin MC 21 It was projected to produce 117 kN 26 000 lbf of thrust 13 Irkut has since replaced the AI 436T12 with the 137 89 kN 31 000 lbf Aviadvigatel PD 14 14 15 Applications editAntonov An 148 Antonov An 72 74 Beriev Be 200 Tupolev Tu 334 Yakovlev Yak 42MSpecifications D 436 T1 editData from Elodie Roux 16 page 159 General characteristics Type Three spool high bypass turbofan Length 3 03 m 9 ft 11 in Diameter 1 373 m 4 ft 6 1 in Dry weight 1 450 kg 3 200 lb Components Compressor Axial flow 1 stage fan 6 stage IP 7 stage HP Turbine 1 stage HP 1 stage IP 3 stage LPPerformance Maximum thrust Takeoff 7 650 kgf 16 865 lbf 75 02 kN Cruise 1 500 kgf 3 307 lbf 14 71 kN at Mach 0 75 speed 11 000 m 36 000 ft altitude Overall pressure ratio 25 2 Bypass ratio 4 95 Air mass flow 606 3 lb s 275 0 kg s Turbine inlet temperature 1 550 K 2 790 R 1 280 C 2 330 F Specific fuel consumption Takeoff 10 6 g kN s 0 37 lb lbf h Cruise 17 3 g kN s 0 61 lb lbf h See also edit nbsp Aviation portalRelated development Lotarev D 36 Lotarev D 136 Progress D 236Comparable engines CFM International CFM56 General Electric CF34 IAE V2500 PowerJet SaM146 Pratt amp Whitney PW6000 Rolls Royce BR700Related lists List of aircraft enginesReferences edit nbsp Wikimedia Commons has media related to Progress D 436 Notes edit Ukraine bans deliveries of D 436 civil aircraft engines to Russia Tass February 19 2018 Retrieved July 29 2022 Ivchenko Progress D 436 Ukraine Aero engines Turbofan 31 March 2009 Archived from the original on 14 August 2009 Retrieved 12 August 2009 a href Template Cite encyclopedia html title Template Cite encyclopedia cite encyclopedia a work ignored help Missing or empty title help Be 200 Indigenous Engine Delays Drive Be 12 Life Extension AINonline April 20 2019 Retrieved September 19 2022 Russia Says It Destroyed Ukrainian Military Engine Plant Newsweek May 26 2022 Retrieved September 19 2022 Fricker John 4 December 1995 Russian AWACS programs face funding problems Aviation Week and Space Technology Vol 143 no 23 pp 89 90 92 ISSN 0005 2175 ZMKB Progress Flight International 8 October 1996 ISSN 0015 3710 Tu 324 414 2003 Flight International 28 October 3 November 2003 p 57 ISSN 0015 3710 Tupolev 1999 Flight International 1 7 September 1999 p 73 ISSN 0015 3710 a b ZMKB Progress 2004 Flight International 23 29 November 2004 p 61 ISSN 0015 3710 India needs more power for Il 214 Flight International 29 April 2002 ISSN 0015 3710 An 148 final assembly gets under way at Kiev Flight International 15 March 2004 ISSN 0015 3710 An 148 design tweaked as date for first flight approaches Paris Air Show Report 2003 Flight International 23 June 2003 ISSN 0015 3710 ENGINES 2008 DEFENSE and SECURITY Russia No 100 September 10 2008 Irkut Removes Pratt amp Whitney Engine Option From The MC 21 SimpleFlying April 25 2022 Retrieved June 10 2023 MC 21 test aircraft flies with PD 14 engines after swap from PW 1400Gs FlightGlobal October 7 2022 Retrieved June 10 2023 Elodie Roux 2007 Turbofan and turbojet engines Database handbook pp 159 160 ISBN 9782952938013 OCLC 804131087 Retrieved from https en wikipedia org w index php title Progress D 436 amp oldid 1159507788, wikipedia, wiki, book, books, library,
