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Progress D-436
Soviet turbofan engine
Soviet turbofan engine
| Field | Value |
|---|---|
| name | D-436 |
| image | D-436-148 MAKS-2009.jpg |
| caption | D-436-148 turbofan engine for An-148 |
| engine_type | Turbofan |
| national_origin | Soviet Union/Ukraine |
| manufacturer | Ivchenko-Progress, UMPO and NPC Saljut |
| first_run | 1985 |
| major_applications | |
| developed_from | Lotarev D-36 |
The Progress D-436 is a triple-spool high-bypass turbofan engine developed by the Ukrainian company Ivchenko-Progress during the Soviet era, and manufactured by Motor Sich in Ukraine. 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. Several variants have been developed and are currently in service with a variety of aircraft.
Design and development
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, was destroyed by Russian forces in late May 2022 following the 2022 Russian invasion of Ukraine.
Variants
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;D-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. ;D-436M: The "M" variant was proposed for use on the Yak-42M. ;D-436T1: The "T1" variant is used on the Tu-334 and has been offered for use on the in-development Tu-414. 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 Tupolev Tu-134. ;D-436T2: The "T2" variant is uprated to 80 kN of thrust and is used on the Tu-334-100D and the Tu-334-200D. ;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. The T3 variant was also considered for the Il-214, but the aircraft's thrust requirements exceeded the max engine thrust of 22,000 lbf. ;D-436-148: The "-148" variant was developed specifically for the An-148. This version is derated to 67 kN of thrust for longer engine life. ;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 - class.
Derivatives
;AI-436T12: This derivative engine was designed for use on the Irkut/Ilyushin MC-21. It was projected to produce 117 kN of thrust. Irkut has since replaced the AI-436T12 with the 31000 lbf Aviadvigatel PD-14.
Applications
- Antonov An-148
- Antonov An-72/74
- Beriev Be-200
- Tupolev Tu-334
- Yakovlev Yak-42M
Specifications (D-436-T1)
and start a new, fully-formatted line with
|power/weight= |thrust/weight=
References
References
- "Ukraine bans deliveries of D-436 civil aircraft engines to Russia". Tass, February 19, 2018.
- {{cite encyclopedia
- "Be-200 Indigenous Engine Delays Drive Be-12 Life Extension". AINonline, April 20, 2019.
- (26 May 2022). "Russia Says It Destroyed Ukrainian Military Engine Plant". Newsweek, May 26, 2022.
- "Russian AWACS programs face funding problems".
- (8 October 1996). "ZMKB Progress".
- "Tu-324/414 (2003)".
- "Tupolev (1999)".
- "ZMKB Progress (2004)".
- (29 April 2002). "India needs more power for Il-214".
- (15 March 2004). "An-148 final assembly gets under way at Kiev".
- (23 June 2003). "An-148 design tweaked as date for first flight approaches".
- ENGINES (2008). ''DEFENSE and SECURITY (Russia)''. No. 100, September 10, 2008
- "MC-21 test aircraft flies with PD-14 engines after swap from PW-1400Gs". FlightGlobal, October 7, 2022.
- Élodie Roux. (2007). "Turbofan and turbojet engines: Database handbook". Elodie Roux.
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