Rolls-Royce Eagle

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For the 1940s engine, see Rolls-Royce Eagle (1944)
Eagle
Rolls-Royce Eagle VIII at the Canada Aviation Museum
Type Piston V-12 aero-engine
Manufacturer Rolls-Royce Limited
First run February 1915
Major applications Airco D.H.4
Vickers Vimy
Number built 4,681
Developed into Rolls-Royce Falcon

The Rolls-Royce Eagle was an aero-engine developed during the First World War by Rolls-Royce that was used to power a number of military aircraft.

Contents

Design and development

The design was a liquid cooled V12 engine with the cylinders inclined at 60 degrees and the valves driven by overhead camshafts. It first ran in 1915. Bore and stroke were 4.5 inches by 6.5 inches (115 x 165 mm) giving a 20 litre capacity. The whole engine weighed 900 lb (408 kg) producing 360 hp (268 kW) at 1800 rpm.

Production ran until 1928 by which point 4,681 had been built.[1]

There is an example of this engine in the Science Museum, London.

Applications

Specifications (Eagle IX)

Data from: Lumsden[2]

General characteristics

  • Type: 12-cylinder liquid-cooled 60° Vee aircraft piston engine
  • Bore: 4.5 in (115 mm)
  • Stroke: 6.5 in (165 mm)
  • Displacement: 1,239 in³ (20.32 L)
  • Length: 72.6 in (1844 mm)
  • Width: 42.6 in (1082 mm)
  • Height: 46.4 in (1178 mm)
  • Dry weight: 900 lb (408 kg)

Components

Performance

See also

References

Notes

  1. ^ Lumsden 2003, p.183.
  2. ^ Lumsden 2003, p.186.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
  • Rubbra, A.A.Rolls-Royce Piston Aero Engines - A Designer Remembers. Rolls-Royce Heritage Trust. Historical Series no 16. ISBN 1-872922-00-7]

External links

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