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.Kotelnikov 2005, p. 111.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.Specifications (AM-38F)
Applications
* Ilyushin Il-2 * Ilyushin Il-10See also
References
Notes
Bibliography
* Gunston, Bill. ''World Encyclopedia of Aero Engines''. Cambridge, England. Patrick Stephens Limited, 1989. * Kotelnikov, Vladimir. ''Russian Piston Aero Engines''. Marlborough, Wiltshire. The Crowood Press Ltd. 2005. . {{Mikulin aeroengines Mikulin aircraft engines 1940s aircraft piston engines