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词条 Lyulka TR-1
释义

  1. Development

  2. Applications

  3. Specifications (TR-1)

  4. See also

  5. References

  6. External links

name= TR-1 image= caption=

}}{{Infobox Aircraft Engine

type=Turbojetmanufacturer= Lyulkanational origin=Soviet Unionfirst run=9 August 1946major applications= Ilyushin Il-22
Sukhoi Su-10
Sukhoi Su-11
Alekseyev I-21
produced=number built=program cost=unit cost=developed from=variants with their own articles=
}}

The Lyulka TR-1 was a turbojet designed by Arkhip Lyulka and produced by his Lyulka design bureau. It was the first indigenous Soviet jet engine.

Development

In May 1944 Lyulka was ordered to begin development of a turbojet with a thrust of {{convert|12.3|kN|lbf|abbr=on}}. He demonstrated an eight-stage axial-flow engine in March 1945 called the S-18. In early 1946 the Council of Ministers ordered that the S-18 be developed into an operational engine with a thrust of {{convert|15.5|kN|lbf|abbr=on}}. The TR-1 was developed in early 1946 and had its first static run on 9 August. It was tested in the air on a pylon fitted to a Lend-Lease B-25 Mitchell piston-engined bomber.[1]

The TR-1 was not a success, proving to have less thrust and a higher specific fuel consumption than designed. Its failure led directly to the cancellation of the first Soviet jet bomber, the Ilyushin Il-22.[2] Lyulka further developed the engine into the TR-1A of {{convert|20.5|kN|lbf|abbr=on}} of thrust, but its specific fuel consumption was very high and it too was cancelled.[1]

Applications

  • Alekseyev I-21
  • Ilyushin Il-22
  • Mikoyan-Gurevich MiG-9 I-305 (izdeliye FT)
  • Sukhoi Su-10
  • Sukhoi Su-11

Specifications (TR-1)

{{jetspecs
|ref=Gordon, OKB Ilyushin: A History of the Design Bureau and its Aircraft.
|type=Turbojet
|length=
|diameter=
|weight=885 kg (1,951 lb)[3]
|compressor=eight-stage axial-flow
|combustion=
|turbine=single stage[3]
|fueltype=
|oilsystem=
|power=
|thrust={{convert|12.8|kN|lbf|abbr=on}}
|compression=
|aircon=
|turbinetemp=
|fuelcon=
|specfuelcon=129 - 137 kg/kN·h (1.27-1.35 lb/lbf·h)
|power/weight=
|thrust/weight=14.5 N/kg (1.47 lbf/lb)
}}

See also

{{aircontent
|see also=
|related=
|similar engines=
  • BMW 003
  • Heinkel HeS 011
  • Heinkel HeS 30
  • Junkers Jumo 004

|lists=
  • List of aircraft engines

}}

References

Notes
1. ^{{cite web|url=http://www.deadlybirds.com.br/deadlybirds_blg/en/tag/lyulka/|title=The USSR into the world Jet|accessdate=2009-09-05|deadurl=yes|archiveurl=https://web.archive.org/web/20110706152053/http://www.deadlybirds.com.br/deadlybirds_blg/en/tag/lyulka/|archivedate=2011-07-06|df=}}
2. ^Gordon, p. 112
3. ^Gunston pp. 99–100
Bibliography
{{Refbegin}}
  • {{Cite book|author=Gordon, Yefim|authorlink =Yefim Gordon|author2=Komissarov, Dmitriy and Sergey |title=OKB Ilyushin: A History of the Design Bureau and its Aircraft|publisher=Ian Allan |location=London|year=2004|isbn= 1-85780-187-3}}
  • {{cite book |title= World Encyclopaedia of Aero Engines|last=Gunston|first=Bill|edition=2| year=1959|volume= |publisher=Patrick Stephens Ltd |location=Wellingborough |isbn=1-85260-163-9}}
  • {{cite book|last=Kay|first=Anthony L.|title=Turbojet History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary |publisher=The Crowood Press|location=Ramsbury|date=2007|edition=1st|volume=|isbn=978-1861269393}}
{{Refend}}

External links

{{Commons category|Ljulka aircraft engines}}
  • [https://web.archive.org/web/20110706152053/http://www.deadlybirds.com.br/deadlybirds_blg/en/tag/lyulka/ Early Lyulka jet engines]
{{Lyulka aeroengines}}

2 : Lyulka aircraft engines|Turbojet engines 1940–1949

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