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Gnome Delta

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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

Specifications (9 Delta)

Thumb
Gnome 18 Delta-Delta from the 1913 Gnome catalog

Data from Lumsden.[1][4][5]

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

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See also

Comparable engines

Related lists

References

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