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词条 Progress D-18T
释义

  1. Design and development

  2. Applications

  3. Specifications (D-18T)

  4. See also

  5. References

  6. External links

name=D-18Timage=Engine D-18T.jpgcaption=D-18T engine installed on an Antonov An-124 "Ruslan" prototype

}}{{Infobox Aircraft Engine

type=Turbofannational origin =Soviet Union/Ukrainedesigner = Ivchenko-Progressmanufacturer = Motor Sich1980}}major applications=Antonov An-124 Ruslan
Antonov An-225 Mriya
number built =188[1]program cost =unit cost =developed from =developed into =variants with their own articles =
}}

The Progress D-18T (or Lotarev D-18T) is a triple-drive shaft, {{cvt|51,500|lbf|kN}} high-bypass turbofan, powering the Antonov An-124 Ruslan and An-225 large freighters.

Design and development

The engine was developed in the second half of the 1970s by the then Soviet Ivchenko-Progress design bureau.[2] It is manufactured by the Motor Sich factory in Zaporizhia, Ukraine. It was the first engine in the USSR that could deliver more than 20,000 kgf (~196 kN or ~44,000 lbf) of thrust.

The first start of a full-scale engine occurred on September 19, 1980, the An-124 maiden flight on December 24, 1982 and the engine passed official bench tests on December 19, 1985.

An upgraded 3M version was developed to reduce emissions and increase the life of the hot section to 14,000 h, and is introduced on An-124s of Antonov Airlines.[2]

Currently 188 D-18T engines are in operation with a total flight time of over 1 million hours.

Applications

  • Antonov An-124
  • Antonov An-225

Specifications (D-18T)

{{jetspecs|
|ref=forecastinternational.com[3]
|type=Three-spool high bypass turbofan engine with a single-stage fan
|length=5.4 m (212.6 in)
  • Width: 2.93 m (115.6 in)
  • Height: 2.79 m (109.9 in)
  • Fan diameter: 2.33 m (91.73 in)

|weight=4,100 kg (9,039 lb)
|compressor=Seven-stage IP compressor, seven-stage HP axial compressor
|combustion=Annular combustion system
|turbine=Single-stage HP turbine, single-stage IP turbine, four‑stage LP turbine
|fueltype=
|oilsystem=
|power=
|thrust=23,430 Kgf; {{convert|229.85|kN|abbr=on}}
|compression=27.5
  • Bypass ratio: 5.7

|aircon=
|turbinetemp=1,600 K (1,327 °C; 2,420 °F)
|fuelcon=
|specfuelcon=
|power/weight=
|thrust/weight=Approx 5.7:1
}}

See also

{{Aircontent
|related=
|similar engines=
  • General Electric CF6
  • Pratt & Whitney JT9D
  • Pratt & Whitney PW4000
  • Rolls-Royce RB211-524
  • Rolls-Royce Trent 500

|lists=
  • List of aircraft engines

|see also=
}}

References

1. ^D18T at deagel.com
2. ^{{cite news |url= http://aviationweek.com/propulsion/freighter-growth-and-possible-124-reengining-boost-cf6-prospects#comment-1081811 |title= Freighter Growth And Possible An-124 Reengining Boost CF6 Prospects |date= Oct 10, 2018 |author= Guy Norris |work= Aviation Week & Space Technology}}
3. ^D-18 by Lotarev

External links

{{Commons category}}
  • D-18T Series 3 Turbofan Aero Engine - SE Ivchenko-Progress
  • {{Citation

| url = http://www.ivchenko-progress.com/welcome.do?id=163&lang=en
| title = Information about D-18T engine
| publisher = Ivchenko-Progress
| archiveurl = https://web.archive.org/web/20120214031151/http://www.ivchenko-progress.com/welcome.do?id=163&lang=en
| archivedate = 2012-02-14
}}{{Ivchenko aeroengines}}

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

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