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RAF 4

From PlaneSpottingWorld, for aviation fans everywhere

The RAF 4 was a British air-cooled, V-12 engine developed for aircraft use during World War I. Based on the eight–cylinder RAF 1 it was designed by the Royal Aircraft Factory but produced by the two British companies of Daimler and Siddeley-Deasy. The RAF 5 was a pusher version of the same engine.[1]

Variants

RAF 4
1914 - Prototype engine, 140 horsepower (104 kW).
RAF 4a
1917 - Main production variant, 160 horsepower (119 kW). 3,608 built.
RAF 4d
1916 - 180 horsepower (134 kW), experimental supercharger installation. 16 built.
RAF 4e
1917 - 240 horsepower (180 kW), strengthened cylinders and enlarged valves.
RAF 5
1915 - 150 horsepower (112 kW), pusher version with fan-cooling.
RAF 5b
170 horsepower (127 kW), increased bore version of RAF 5.

Applications

RAF 4

File:Royal Aircraft Factory RE8 1.jpg
The Royal Aircraft Factory R.E.8

RAF 5

Engines on display

A preserved RAF 4a engine is on public display at the Science Museum (London).

Specifications (RAF 4a)

Template:Pistonspecs

See also

Related development

Related lists

References

Notes

  1. Gunston, 1989, p. 156.

Bibliography

  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.

External links

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This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "RAF 4".