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词条 Progress D-436
释义

  1. Design and development

  2. Variants

     Derivatives 

  3. Applications

  4. Specifications (D-436-T1)

  5. See also

  6. References

     Notes  Bibliography 
name=D-436image= D-436-148 MAKS-2009.jpgcaption=D-436-148 turbofan engine for An-148

}}{{Infobox Aircraft Engine

type=Turbofannational origin =Soviet Union/Ukrainemanufacturer=Ivchenko-Progress , UMPO and NPC Saljut1985}}major applications=Antonov An-148
Tupolev Tu-334
Beriev Be-200		number built =program cost =unit cost =developed from =Lotarev D-36developed into =variants with their own articles =
}}

The Progress D-436 is a three-shaft high by-pass turbofan engine developed by the Ukrainian company Ivchenko-Progress. 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.[1] 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.

Variants

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[2]
D-436M
  • The "M" variant was proposed for use on the Yak-42M.[3]
D-436T1
  • The "T1" variant is used on the Tu-334 and has been offered for use on the in-development Tu-414.[4] 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 {{convert|80|kN|abbr=on}} of thrust and is used on the Tu-334-100D and the Tu-334-200D.[5]
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 {{convert|93|kN|abbr=on}}.[6] The T3 variant was also considered for the Il-214, but the aircraft's thrust requirements exceeded the max engine thrust of {{convert|93|kN|abbr=on}}.[7]
D-436-148
  • The "-148" variant was developed specifically for the An-148.[8] This version is derated to {{convert|67|kN|abbr=on}} of thrust for longer engine life[9]
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 {{convert|117|-|135|kN|abbr=on}}class.[10]

Derivatives

AI-436T12
  • This derivative engine was designed for use on the Irkut/Ilyushin MC-21. It was projected to produce {{convert|117|kN|abbr=on}} of thrust.[11] Irkut has since replaced the AI-436T12 with the 14,000 kgf (31,000 lbf)Aviadvigatel PD-14.{{cn|date=April 2018}}

Applications

  • Antonov An-148
  • Antonov An-72/74
  • Beriev Be-200
  • Tupolev Tu-334
  • Yakovlev Yak-42M

Specifications (D-436-T1)

{{jetspecs
|ref=ivchenko-progress.com,[12] Flight,[13] Jane's Aero Engines and forecastinternational.com[14]
|type=Three-spool high bypass turbofan
|length={{convert|3030|mm|in|abbr=on}}
|diameter={{convert|1390|mm|in|abbr=on}}
|weight={{convert|1450|kg|abbr=on}}
|compressor=Axial flow, 1-stage 33-blade fan, 6-stage IP, 7-stage HP
|combustion=
|turbine=Single-stage HP, single-stage IP, 3-stage LP
|fueltype=
|oilsystem=
|power=
|thrust={{convert|75.02|kN|kgf|abbr=on}}; (16,859 lbf)
|compression=21.9 : 1
|aircon=
|turbinetemp=1,197 C (2,186 F)
|fuelcon=
|specfuelcon=61 kg/kN/h (0.608 lb/lbf*hr)
|power/weight=
|thrust/weight=5.6
}}

See also

{{aircontent
|see also=
|related=
|similar engines=
  • General Electric CF34
  • IAE V2500
  • PowerJet SaM146
  • Pratt & Whitney PW6000
  • Rolls-Royce BR700
  • Rolls-Royce RB.183 Tay

|lists=
  • List of aircraft engines

}}

References

{{Commons category}}

Notes

1. ^"Ivchenko-Progress D-436". Jane's.
2. ^Fricker, John. RUSSIAN AWACS PROGRAMS FACE FUNDING PROBLEMS (1995).Aviation Week and Space Technology. Vol. 143, No. 23; Pg. 89.
3. ^ZMKB Ivchenko Progress (1997). Flight International. 24-30 Sept 1997, pg 50.
4. ^Tu-324/414 (2003). Flight International. 28 Oct - 3 Nov 2003, pg. 57.
5. ^Tupolev (1999). Flight International. 1-7 Sept 1999, pg. 73.
6. ^ZMKB Progress (2004).Flight International.23-29 Nov 2004, pg.61
7. ^India needs more power for 11-214 (2002). Flight International. 30 April - 6 May 2002, pg. 20.
8. ^An-148 final assemblygets under way at Kiev (2004). Flight International. 16–22 March 2004, pg. 10.
9. ^An-148 design tweaked as date for first flight approaches (2003). Flight International. 24-30 Jun 2003, pg. 22.
10. ^ZMKB Progress (2004).Flight International.23-29 Nov 2004, pg.61
11. ^ENGINES (2008). DEFENSE and SECURITY (Russia). No. 100, September 10, 2008
12. ^D-436T1 at ivchenko-progress.com
13. ^Engine Directory: ZMKB Ivchenko Progress (1997). Flight International. September 24, 1997.
14. ^Russia, Central/Eastern Europe and China Turbofan and Turbojet Engines{{dead link|date=April 2018 |bot=InternetArchiveBot |fix-attempted=yes }}

Bibliography

{{refbegin}}
  • Ivchenko-Progress D-436 (Ukraine), Aero-engines - Turbofan.Jane's. http://www.janes.com/articles/Janes-Aero-Engines/Ivchenko-Progress-D-436-Ukraine.html. Retrieved Aug 12 2009.
  • Ivchenko-Progress D-436. Jane's Aero-Engines. Modified 31 Mar 2009, Retrieved 12 Aug 2009.
{{refend}}{{Ivchenko aeroengines}}

4 : Ivchenko-Progress aircraft engines|High-bypass turbofan engines|Turbofan engines 1980–1989|Three-spool turbofan engines
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