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Gnome Omega

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(Redirected from Gnome 14 Omega-Omega) 1900s French aircraft piston engine
Omega
Gnome 7 Omega on display at the Newark Air Museum
Type Rotary aero engine
Manufacturer Société des Moteurs Gnome
First run 1908
Major applications Blériot XI
Bristol Boxkite
Number built 4,000 until 1914

The Gnome 7 Omega (commonly called the Gnome 50 hp) is a French seven-cylinder, air-cooled aero engine produced by Gnome et Rhône. It was shown at the Paris Aero Salon held in December 1908 and was first flown in 1909. It was the world's first aviation rotary engine produced in quantity. Its introduction revolutionized the aviation industry and it was used by many early aircraft. It produced 37 kW (50 hp) from its 8 L (490 cu in) engine capacity. A Gnome Omega engine powers the 1912 Blackburn Monoplane, owned and operated by the Shuttleworth Collection, the oldest known airworthy British-designed aeroplane worldwide. 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.

Like all early Gnome et Rhône engines the Omega features a single pushrod driven exhaust valve on the cylinder head; the intake valve is located in the piston crown, opening by inertia on the downstroke and feeding the intake charge from the crankcase into the upper part of the cylinder. No throttle is provided, the pilot controls the aircraft's speed by switching off the ignition when necessary.

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
Gnome 14 Omega-Omega, as shown in a 1913 Gnome catalog.

Gnome 14 Omega-Omega

Engines on display

Specifications (7 Omega)

Brown staining of the Shuttleworth example caused by burnt castor oil

Data from Lumsden.

General characteristics

Components

Performance

  • Power output: 37 kW (50 hp) at 1,200 rpm

See also

Comparable engines

Related lists

Footnotes

  1. ^ Nahum 1999, pp. 12–14
  2. ^ Smithsonian Institution 2018
  3. Murphy 2005
  4. ^ Lumsden 2003, p. 152
  5. Shuttleworth 2018
  6. Schiere 1969, pp. 15–16
  7. Hurley 2018

References

Further reading

External links

Gnome-Rhône aircraft engines
Gnome rotary engines
Le Rhône rotary engines
Gnome et Rhône radial engines
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