Английская Википедия:Armstrong Siddeley Serval
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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English
Шаблон:Infobox Aircraft EngineThe 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
- Airco DH.9
- Armstrong Whitworth Atalanta
- BFW M.36
- Canadian Vickers Vancouver
- Fairey Fox
- ICAR Comercial
- Saro Cloud
- Stampe et Vertongen SV.5 Tornado
Specifications (Serval I)
See also
References
Notes
Bibliography
- 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.
- ↑ Gunston 1989, p.17.
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