Английская Википедия:Armstrong Siddeley Serval

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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English

Шаблон:Infobox Aircraft Engine

The Armstrong Siddeley Serval was a British ten-cylinder aero engine developed by Armstrong Siddeley in the late 1920s. Following company tradition, the engine was named for the serval.

Design and development

The Serval was a ten-cylinder, double-row, air-cooled radial piston engine. It was developed from the Armstrong Siddeley Mongoose and was, more or less, two Mongooses built around a single crankcase. In fact, it first appeared as the Double Mongoose in May 1928.[1]

Built in several variants, power output was about 340 hp (254 kW).

Variants

Serval I initially Double Mongoose

(1931) 340 hp.
Serval III
(1932)
Serval IIIB
(1932) 310 hp.
Serval IV
310 hp.
Serval V
(1933) 340 hp.

Applications

Файл:Saro cloud 001.jpg
AS Serval powered Saro Cloud

Specifications (Serval I)

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See also

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References

Notes

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Bibliography

Шаблон:Refbegin

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. Шаблон:ISBN
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. Шаблон:ISBN.

Шаблон:Refend

Шаблон:ASaeroengines

  1. Gunston 1989, p.17.