Clerget 9B
The Clerget 9B was a nine-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. Manufactured in both Great Britain (Gwynne Limited) and France, it was used on such aircraft as the Sopwith Camel. The Clerget 9Bf was an increased stroke version.[2]
Variants
- Clerget 9B
(1913) 130 hp (97 kW). 1,300 produced by Ruston Proctor & Co Ltd of Lincoln
- Clerget 9Bf
(1915) 140 hp (104 kW). Extended stroke (172 mm (6.75 in)) version, increasing capacity to 17.5 L (1,066.5 cu in). 1,750 produced by Gwynnes Ltd. and 600 produced by Ruston Proctor.
Applications
Clerget 9B
Clerget 9Bf
Engines on display
Specifications (Clerget 9B)
Data from Lumsden.[2]
General characteristics
- Type: Nine-cylinder air-cooled rotary engine
- Bore: 120 mm (4.72 in)
- Stroke: 160 mm (6.30 in)
- Displacement: 16.29 L (993.8 cu in)
- Dry weight: 175 kg (385 lb)
Components
- Fuel system: Bloctube carburettor
- Cooling system: Air-cooled
Performance
See also
- Related development
- Comparable engines
- Related lists
References
Notes
Bibliography
- Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
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