Kuznetsov TV-022
| TV-022 | |
|---|---|
| |
| A hand-drawn cutaway view of the TV-022 | |
| Type | Turboprop |
| National origin | Soviet Union |
| Manufacturer | Kuybyshev Engine Design Bureau |
| First run | June 1949[1] |
| Developed from | Junkers Jumo 022 |
| Developed into | TV-2 |
The Kuznetsov TV-022 was the first Soviet turboprop engine, designed by the Kuybyshev Engine Design Bureau.
Development
[edit]Development of the TV-022 began in 1947[2] at the State Union Experimental Plant No. 2 near Kuybyshev.[3] A team of both Soviet and deported German engineers worked on the project.[3]
The TV-022 was based on the uncompleted Junkers Jumo 022 turboprop designed by Junkers during the later stages of World War II.[2]
Factory tests of the TV-022 took place in June 1949[1] and state tests where passed in October 1950.[1] The TV-022 featured a reduction gearbox (i=0.145)[1] for two coaxial contra-rotating AB-41 propellers.[1] The engine was started with a 50 kW "Rut" air starter.[1]
Modifications to the TV-022 resulted in the TV-2, which had more power (6,250 hp).[1] The TV-2 was then further modified into the NK-12.[2]
Specifications (TV-022)
[edit]Data from Otechestvennaya aviatsionno-kosmicheskaya tekhnika - SAMARSKIY NTK,[1] and engine.aviaport.ru[4]
General characteristics
- Type: Turboprop engine
- Length: 4,170 mm (164 in)[1] without propellers
- Diameter: 1,050 mm (41 in)[1] without propellers
- Dry weight: 1,700 kg (3,700 lb)
Components
- Compressor: 14-stage[1] compressor
- Combustors: 12 annular combustion chambers made of heat resistant steel (EI417)[1]
- Turbine: 3-stage[1] turbine, of which only the first and second stages are cooled[1]
Performance
- Maximum power output:
- Overall pressure ratio: 5.6[4]
- Air mass flow: 30 kg/s (66 lb/s)[1]
- Turbine inlet temperature: 1,120 K (850 °C; 1,560 °F)[4]
- Specific fuel consumption: 0.21 kg/(hp⋅h)[4]
See also
[edit]Comparable engines
Related lists
References
[edit]- ^ a b c d e f g h i j k l m n o Otechestvennaya aviatsionno-kosmicheskaya tekhnika - SAMARSKIY NTK (in Russian). Samara, Russia: SNTK imeni N.D.Kuznetsova. pp. 10, 11, 72.
- ^ a b c "Junkers Jet Engine Developments". tanks45.tripod.com. Retrieved 12 October 2021.
- ^ a b "Creation of the TV-2 (NK-12) Turboprop Engine". airpages.ru. Retrieved 12 October 2021.
- ^ a b c d e f "Tot samyy "NK"". engine.aviaport.ru (in Russian). Nikolay Aleksandrov. Retrieved 4 October 2021.