Gnome Omega

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Type Rotary aero engine
Manufacturer Gnome Engine Company
First run 1908
Major applications Blériot XI
Bristol Boxkite
Number built 4,000 until 1914[ 1] (more later)
Unit cost £520 in 1909[ 1]

The Gnome 7 Omega (commonly called the Gnome 50 hp) is a French seven-cylinder, air-cooled aero engine.[ 1] It was shown at the Paris Aero Salon held in December 1908 and was first flown in 1909. It was the world's first[ 1] rotary engine produced in quantity. Its introduction revolutionized the aviation industry[ 1] and it was used by many early aircraft. It produced 50 horsepower (37 kW) from its capacity of 8 litres (488 cubic inches).[1] A Gnome Omega engine powers the 1912 Blackburn Monoplane, owned and operated by the Shuttleworth Collection, the oldest known airworthy British-designed aeroplane worldwide.[2] A two-row version of the same engine was also produced, known as the Gnome 14 Omega-Omega or Gnome 100 hp. The prototype Omega engine still exists, and is on display at the United States' National Air and Space Museum.[3]

sectional views of the Gnome Omega

Variants

Gnome 7 Omega
Single-row 7-cyl. original version; 50 hp (37 kW).
Gnome 14 Omega-Omega
Two-row, 14-cylinder version using Omega cylinders; 100 hp (75 kW).

Applications

Gnome 7 Omega

Gnome Omega-powered airworthy Blackburn Monoplane of the Shuttleworth Collection
  • Short S.37 Tractor Monoplane
  • Short Triple Twin
  • Short S.47 Triple Tractor
  • Short S.62
  • Sopwith Bee
  • Sopwith Sparrow
  • Valkyrie Type B
  • Vickers No.6 Monoplane
  • Vickers No.7 Monoplane
  • Vickers Boxkite School Biplane

Gnome 14 Omega-Omega

Engines on display

Specifications (7 Omega)

Brown staining of the Shuttleworth example caused by burnt castor oil

Data from Lumsden.[1]

General characteristics

  • Type: 7-cylinder, single-row, rotary engine
  • Bore: 110 mm (4.3 in)
  • Stroke: 120 mm (4.7 in)
  • Displacement: 8 L (488.5 cu in)
  • Length: 79 cm (31 in)
  • Diameter: 84 cm (33 in)
  • Dry weight: 75 kg (165 lb)

Components

  • Valvetrain: pressure-driven inlet valves were located on the pistons[ 1]
  • Oil system: Total loss, castor oil
  • Cooling system: Air-cooled
  • Reduction gear: Direct drive, right-hand tractor, left-hand pusher

Performance

  • Power output: 37 kW (50 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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