1900s French aircraft piston engine
The Gnome 7Σ Sigma (commonly called the Gnome 60 hp) is a French seven-cylinder, air-cooled rotary aero engine.[1]
The Sigma produced 60 hp (45 kW) from its capacity of 9.5 L (579.73 cu in).
Specifications (7 Sigma)
Data from Société Des Moteurs Gnome[2]
General characteristics
Components
- Valvetrain: pushrod operated overhead exhaust valves plus pressure-driven inlet valves located in the piston crowns[3]
- Fuel system: a single static Bloctube carburretor feeding the crankcase
- Fuel type: 40 / 50 octane gasoline
- Oil system: pressure-fed total loss, castor oil
- Cooling system: Air-cooled
- Reduction gear: Direct drive, right-hand tractor, left-hand pusher
- Power output: 45 kW (60 hp) at 1,200 rpm
See also
Comparable engines
Related lists
References
Notes
Bibliography
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
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Gnome rotary engines | |
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Le Rhône rotary engines | |
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Gnome et Rhône radial engines | |
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