| 词条 | Lyulka TR-3 | ||||||||||||||
| 释义 |
The Lyulka TR-3 was a Soviet axial turbojet designed after World War II by Arkhip Mikhailovich Lyulka. DevelopmentThe 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 {{convert|46|kN|lbf|abbr=on}}. It was used in the Ilyushin Il-30 during 1949, but was superseded by later versions.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
Specifications (TR-3){{jetspecs|ref=Kay, Turbojet |type=turbojet |length= |diameter= |weight={{convert|1900|kg|abbr=on}} |compressor=seven-stage axial-flow |combustion=annular combustion chamber |turbine=single-stage |fueltype= |oilsystem= |power= |thrust={{convert|46|kN|lbf|abbr=on}} |compression= |bypass= |aircon= |turbinetemp= |fuelcon= |specfuelcon=approximately 1.1 |power/weight= |thrust/weight=2.38 }} See also{{aircontent|see also= |related=
|similar engines= |lists=
References
1. ^Kay, pp. 27–28
External links{{Commons category|Ljulka aircraft engines}}
2 : Lyulka aircraft engines|Turbojet engines 1940–1949 |
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