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Shvetsov M-25

From Wikipedia, the free encyclopedia
Soviet aircraft engine
M-25
TypeRadial engine
ManufacturerShvetsov
Number built13,888
Developed fromWright R-1820
Developed intoShvetsov ASh-62

TheShvetsov M-25 was an aircraftradial engine produced in theSoviet Union (USSR) in the 1930s and 1940s, a licensed production variant of theWright R-1820-F3.

Design and development

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The first M-25s were produced from kits imported from the United States; the main difference between the later M-25 and the R-1820-F3 was the use of metric components. 13,888 M-25s were produced in the USSR at factories inPerm andKazan. There were a number of sub-variants which differed from the original M-25 in that they hadreduction gears, rather thandirect drive. Performance was similar to the equivalent Wright engines. The M-25 was later developed into theASh-62 and was later used as a pattern for the M-70. The M-70, a twin-row 18-cylinder engine, eventually developed into theASh-73 which powered theTupolev Tu-4, an unlicensed, reverse-engineered copy of theBoeing B-29 Superfortress.

Applications

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Specifications (Shvetsov M-25)

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Family tree of Shvetsov engines

General characteristics

  • Type: 9-cylinder, air-cooled,radial engine
  • Bore: 155.5 mm (6.122 in)
  • Stroke: 174.5 mm (6.870 in)
  • Displacement: 29.876 L (1,823.1 cu in)
  • Length: 1,100 mm (43.307 in)
  • Diameter: 1,365 mm (53.740 in)
  • Dry weight: 434 kg (957 lb)

Components

  • Supercharger: Single speed, single stage, geared centrifugal supercharger
  • Fuel system: 1 K-25 (Solex) Carburetor

Performance

  • Power output: 520–600 kW (700–800 hp) depending on model
  • Compression ratio: 6.4:1

See also

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Related development

Related lists

References

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Wikimedia Commons has media related toShvetsov M-25.
  • Gunston, Bill (1986).World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 175.
  • Kotelnikov, Vladimir (2005).Russian Piston Aero Engines. Crowood Press Ltd. pp. 118–119.
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