Skip to content
Surf Wiki
Save to docs
general/ivchenko-progress-aircraft-engines

From Surf Wiki (app.surf) — the open knowledge base

Progress D-436

Soviet turbofan engine

Progress D-436

Summary

Soviet turbofan engine

FieldValue
nameD-436
imageD-436-148 MAKS-2009.jpg
captionD-436-148 turbofan engine for An-148
engine_typeTurbofan
national_originSoviet Union/Ukraine
manufacturerIvchenko-Progress, UMPO and NPC Saljut
first_run1985
major_applications
developed_fromLotarev 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

A Progress D-436 installed on an [[Antonov An-158

;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

  1. "Ukraine bans deliveries of D-436 civil aircraft engines to Russia". Tass, February 19, 2018.
  2. {{cite encyclopedia
  3. "Be-200 Indigenous Engine Delays Drive Be-12 Life Extension". AINonline, April 20, 2019.
  4. (26 May 2022). "Russia Says It Destroyed Ukrainian Military Engine Plant". Newsweek, May 26, 2022.
  5. "Russian AWACS programs face funding problems".
  6. (8 October 1996). "ZMKB Progress".
  7. "Tu-324/414 (2003)".
  8. "Tupolev (1999)".
  9. "ZMKB Progress (2004)".
  10. (29 April 2002). "India needs more power for Il-214".
  11. (15 March 2004). "An-148 final assembly gets under way at Kiev".
  12. (23 June 2003). "An-148 design tweaked as date for first flight approaches".
  13. ENGINES (2008). ''DEFENSE and SECURITY (Russia)''. No. 100, September 10, 2008
  14. "MC-21 test aircraft flies with PD-14 engines after swap from PW-1400Gs". FlightGlobal, October 7, 2022.
  15. Élodie Roux. (2007). "Turbofan and turbojet engines: Database handbook". Elodie Roux.
Wikipedia Source

This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.

Want to explore this topic further?

Ask Mako anything about Progress D-436 — get instant answers, deeper analysis, and related topics.

Research with Mako

Free with your Surf account

Content sourced from Wikipedia, available under CC BY-SA 4.0.

This content may have been generated or modified by AI. CloudSurf Software LLC is not responsible for the accuracy, completeness, or reliability of AI-generated content. Always verify important information from primary sources.

Report