Lyulka TR-3

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TR-3
Type turbojet
National origin Soviet Union
Manufacturer Lyulka
First run 9 September 1947
Major applications Ilyushin Il-30
Developed from Lyulka AL-5

The Lyulka TR-3 was a Soviet axial turbojet designed after World War II by Arkhip Mikhailovich Lyulka.

Development[edit]

The Lyulka TR-3 was a single-shaft turbojet with a seven-stage axial compressor. It had an annular combustion chamber with 24 nozzles and a single-stage turbine. It had a fixed exhaust nozzle and had a pneumatic SV-3 starting unit, although this was later replaced by a turbine unit. It had a thrust of 46 kN (10,000 lbf). It was used in the Ilyushin Il-30 during 1949, but was superseded by later versions. The improved TR-3A version was redesignated as the AL-5 to honor Lyulka in 1950.[1]

Applications[edit]

Specifications (TR-3)[edit]

Data from Kay, Turbojet

General characteristics

  • Type: turbojet
  • Length:
  • Diameter:
  • Dry weight: 1,900 kg (4,200 lb)

Components

  • Compressor: seven-stage axial-flow
  • Combustors: annular combustion chamber
  • Turbine: single-stage

Performance

See also[edit]

Related development
Related lists

References[edit]

Notes
  1. ^ Kay, pp. 27–28
Bibliography
  • Kay, Anthony L. Turbojet: History and Development 1930–1960: Volume 2: USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy, Czechoslovakia and Hungary. Marlborough, Wiltshire: Crowood Press, 2007 ISBN 978-1-86126-939-3
  • Gunston, Bill. The Osprey Encyclopaedia of Russian Aircraft 1875–1995. London, Osprey, 1995 ISBN 1-85532-405-9

External links[edit]