fbpx
Wikipedia

Mikulin AM-37

The Mikulin AM-37 was a Soviet aircraft piston engine designed prior to Russia's entry into World War II. An improved version of the Mikulin AM-35 V-12 engine, it was only produced in small numbers because of its unreliability.

Mikulin AM-37
Type liquid-cooled, V12 engine
National origin Soviet Union
Manufacturer Mikulin
First run 5 January 1941
Produced 1941
Number built 39+
Developed from Mikulin AM-35

Development

Design work on a development of the AM-35 with boosted supercharging and an intercooler positioned behind the supercharger began on the factory's initiative in December 1939. A batch of ten prototypes was completed in 1940 and bench-testing began on 5 January 1941. It passed its State acceptance trials the following April and was approved for production. It was tested in a variety of aircraft, but proved to be unreliable and prone to overheating. Factory No. 24 in Moscow built only twenty-nine AM-37s, as the new engine was designated, in 1941 before the German advance forced the factory to evacuate in October. Mikulin had been unable to resolve the issues with the AM-37 in the meantime and production was not resumed.[1]

Variants

AM-37A
Planned version to be tested in February 1940, but no information if it was tested or it was even completed. 1,600 hp (1,200 kW) and a weight of 850 kg (1,870 lb).
AM-37TK
TK for toorbokompressor. Planned version with a turbocharger, no further information known.
AM-37P
P for Pushechnyy or cannon. A 1940 project for a model with an autocannon mounted in the space between the cylinders, firing through a hollow reduction-gear shaft. No further information available.
Am-37u/v or AM-37UV
UV for udlinyonniy val or lengthened shaft. An engine with a lengthened shaft and remote gearing for use in the Gudkov G-1 fighter that carried the engine behind the pilot. Ordered developed in 1940 and design work started in 1941, but it was not completed.

Applications

Specifications

Data from Kotelnikov, Russian Piston Aero Engines

General characteristics

Components

Performance

See also

Related development

Related lists

References

Notes

  1. ^ Kotelnikov, p. 110

Bibliography

  • Kotelnikov, Vladimir (2005). Russian Piston Aero Engines. Ramsbury, Marlborough: Crowood Press. ISBN 1-86126-702-9.

mikulin, redirects, here, united, states, navy, minesweeper, sanderling, soviet, aircraft, piston, engine, designed, prior, russia, entry, into, world, improved, version, mikulin, engine, only, produced, small, numbers, because, unreliability, type, liquid, co. AM 37 redirects here For the United States Navy minesweeper see USS Sanderling AM 37 The Mikulin AM 37 was a Soviet aircraft piston engine designed prior to Russia s entry into World War II An improved version of the Mikulin AM 35 V 12 engine it was only produced in small numbers because of its unreliability Mikulin AM 37Type liquid cooled V12 engineNational origin Soviet UnionManufacturer MikulinFirst run 5 January 1941Produced 1941Number built 39 Developed from Mikulin AM 35 Contents 1 Development 2 Variants 3 Applications 4 Specifications 4 1 General characteristics 4 2 Components 4 3 Performance 5 See also 6 References 6 1 Notes 6 2 BibliographyDevelopment EditDesign work on a development of the AM 35 with boosted supercharging and an intercooler positioned behind the supercharger began on the factory s initiative in December 1939 A batch of ten prototypes was completed in 1940 and bench testing began on 5 January 1941 It passed its State acceptance trials the following April and was approved for production It was tested in a variety of aircraft but proved to be unreliable and prone to overheating Factory No 24 in Moscow built only twenty nine AM 37s as the new engine was designated in 1941 before the German advance forced the factory to evacuate in October Mikulin had been unable to resolve the issues with the AM 37 in the meantime and production was not resumed 1 Variants EditAM 37A Planned version to be tested in February 1940 but no information if it was tested or it was even completed 1 600 hp 1 200 kW and a weight of 850 kg 1 870 lb AM 37TK TK for toorbokompressor Planned version with a turbocharger no further information known AM 37P P for Pushechnyy or cannon A 1940 project for a model with an autocannon mounted in the space between the cylinders firing through a hollow reduction gear shaft No further information available Am 37u v or AM 37UV UV for udlinyonniy val or lengthened shaft An engine with a lengthened shaft and remote gearing for use in the Gudkov G 1 fighter that carried the engine behind the pilot Ordered developed in 1940 and design work started in 1941 but it was not completed Applications EditMikoyan Gurevich MiG 1 Mikoyan Gurevich MiG 3 Mikoyan Gurevich DIS Polikarpov TIS Tupolev Tu 2 Yermolaev Yer 2Specifications EditData from Kotelnikov Russian Piston Aero Engines General characteristics Type supercharged liquid cooled V12 engine Bore 160 mm 6 3 in Stroke 190 mm 7 5 in Displacement 45 84 L 2 797 in Dry weight 885 kg 1 951 lb Designer Alexander MikulinComponents Supercharger single speed geared centrifugal supercharger Cooling system liquid cooledPerformance Power output 1 500 hp 1 119 kW Compression ratio 7 0 1 Power to weight ratio 0 77 hp lb 1 26 kW kg See also EditRelated development Mikulin AM 35Related lists List of aircraft enginesReferences EditNotes Edit Kotelnikov p 110 Bibliography Edit Kotelnikov Vladimir 2005 Russian Piston Aero Engines Ramsbury Marlborough Crowood Press ISBN 1 86126 702 9 Retrieved from https en wikipedia org w index php title Mikulin AM 37 amp oldid 896028940, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.