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Gnome Delta
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The Gnome 9 Delta was a French designed, nine-cylinder, air-cooled rotary aero engine that was produced under license in Britain. Powering several World War I era aircraft types it produced 100 hp (75 kW) from its capacity of 16 litres (980 cu in).[1]
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Variants
- Delta
- The baseline 9-cylinder 100 hp (75 kW) rotary engine.
- Delta-Delta
- An 18-cylinder 200 hp (150 kW) two-row rotary engine - Two Deltas on a common crankshaft.
Applications
List from Lumsden
Engines on display
- A preserved Gnome 9 Delta engine is on public display at the Musée des Arts et Métiers, Paris
Specifications (9 Delta)

General characteristics
- Type: 9-cylinder, single-row, rotary engine
- Bore: 124 mm (4.88 in)
- Stroke: 150 mm (5.91 in)
- Displacement: 16.28 L (993.47 cu in)
- Length: 1,150 mm (45.28 in)
- Diameter: 1,020 mm (40.16 in)
- Dry weight: 135 kg (297.6 lb)
Components
- Valvetrain: Automatic centre-piston inlet valve, one overhead exhaust valve per cylinder.
- Fuel system: one static Bloctube carburettor feeding the crankcase
- Fuel type: 40 / 50 Octane gasoline
- Oil system: Total loss pressure fed
- Cooling system: Air-cooled
Performance
- Power output: 75 kW (100 hp) at 1,200 rpm
- Specific fuel consumption: 362 g/(kW·h) (0.6 lb/(hp·h))
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See also
Comparable engines
Related lists
References
External links
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