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The Mikulin AM-38 was a 1940s Soviet aircraft piston engine. It was a further development of the Mikulin AM-35 design.[1] The AM-38 was used on the Il-2 Shturmovik and Il-10 ground attack aircraft. The AM-38 was installed experimentally in a MiG-3 and tested during August 1941. A slight performance improvement was seen at low-altitude but the engine experienced overheating problems due to the cooling and oil systems remaining unchanged from the AM-35A.[2]
| AM-38 | |
|---|---|
 | |
| Preserved Mikulin AM-38F engine | |
| Type | Liquid-cooled V-12 piston engine |
| National origin | USSR |
| Manufacturer | Mikulin |
| First run | 1941 |
| Major applications | Ilyushin Il-2 |
| Number built | 43,191 |
| Developed from | Mikulin AM-35 |
| Developed into | Mikulin AM-42 |
Description
The AM-38 was a low-altitude engine for ground attack aircraft that evolved from the earlier AM-35A. Compared to the AM-35A it had a reduced compression ratio, strengthened crankshaft, a single-speed geared centrifugal supercharger optimized for low-altitude performance, revised cooling system and revised oil system. The AM-38 was developed by the design bureau of Factory No. 24 now called the Salyut factory in Moscow. The first examples were produced in October 1939 and passed its Factory tests in November 1939. The AM-38 was placed in production at the start of 1941 despite not passing its State tests until July 1941. The majority of engines were produced at Factory No. 24 which was evacuated to Kuybyshev at the end of 1941. In June 1942 production also began at Factory No. 45 which used the former workshops of Factory No. 24 in Moscow. The AM-38 was the most produced Mikulin engine with 43,191 built by the time it was phased out of production in 1946.[3]
Variants
- AM-38F: A version with higher RPM for takeoff and a 10-minute forsazh (war emergency power) mode. It also had an oil centrifuge, strengthened camshafts, strengthened cylinder block, strengthened inlet valves and cylinder heads made from a new alloy. The diameter of the GCS impeller was also reduced and its compression ration was lowered to accommodate lower quality fuel. Series production began in at Factory No. 24 in October 1942 and Factory No. 45 in 1943. The engine did not pass State test until May 1943.
- GAM-38F: A proposed marine version of the AM-38F.[3]
Specifications (AM-38F)
Data from Kotelnikov.[4]
General characteristics
- Type: 12-cylinder 60° V aircraft piston engine
- Bore: 160 mm (6.30 in)
- Stroke: 190 mm (7.48 in) (196.7 mm (7.74 in) for cylinders with articulated connecting rods)
- Displacement: 46.66 L (2,847 cu in)
- Dry weight: 880 kg (1,940 lb)
Components
- Supercharger: Single-speed geared centrifugal supercharger
- Cooling system: Liquid-cooled
Performance
- Power output: 1,270 kW (1,700 hp) at 2,350 rpm
- Specific power: 27.2 kW/L (0.60 hp/in³)
- Compression ratio: 6.0:1
- Power-to-weight ratio: 1.53 kW/kg (0.93 hp/lb)
Applications
See also
Related development
Related lists
References
Notes
- Gunston 1989, p.104.
- Gordon, Yefim (1998). Soviet combat aircraft of the Second World War. Khazanov, Dmitriĭ. Leicester: Midland Pub. p. 74. ISBN 1857800834. OCLC 40494691.
- Kotelnikov 2005, p. 111.
- Kotelnikov 2005, p. 111.
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Kotelnikov, Vladimir. Russian Piston Aero Engines. Marlborough, Wiltshire. The Crowood Press Ltd. 2005. ISBN 1-86126-702-9.
На других языках
[de] Mikulin AM-38
Der Mikulin AM-38 war ein V12-Flugmotor, der im sowjetischen Schlachtflugzeug Iljuschin Il-2 zum Einsatz kam. Das Kürzel AM bezieht sich auf seinen Konstrukteur Alexander Mikulin.- [en] Mikulin AM-38
[es] Mikulin AM-38
El Mikulin AM-38 fue un motor de aviación refrigerado por líquido desarrollado en la Unión Soviética, evolución[1] del modelo previo AM-35, entrando en producción en 1941, y siendo empleado en los aviones de ataque Ilyushin Il-2. La producción del motor alcanzó las 36.163 unidades.[it] Mikulin AM-38
Il Mikulin AM-38, citato anche come M-38, era un motore aeronautico 12 cilindri a V di 60° raffreddato a liquido progettato dall'OKB 34 diretto da Aleksandr Aleksandrovič Mikulin e sviluppato in Unione Sovietica negli anni quaranta.[ru] АМ-38
Микулин АМ-38 — советский поршневой авиационный двигатель конструктора А. А. Микулина. Являясь дальнейшей разработкой двигателя АМ-34, АМ-38 использовался на самолётах МиГ-3 и Ил-2 во время Второй мировой войны. Создание мотора АМ-38 было очередным стратегическим прорывом в отечественном моторостроении.Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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