PlaneSpottingWorld welcomes all new members! Please gives your ideas at the Terminal.

RAF 1

From PlaneSpottingWorld, for aviation fans everywhere

The RAF 1 was a British air-cooled, V-8 engine developed for aircraft use during World War I. Based on a French design it was designed by the Royal Aircraft Factory but built by six different British companies including Rolls-Royce and the Wolseley Motor Company.

Design and development

The RAF 1 was based on a Renault engine of the time, but featured larger cylinders (3.9 in × 5.5 inches or 100 mm × 140 mm ) for a total displacement of 540 cubic inches (8.8 L). It was rated at 92 hp (70 kW) at 1,600 rpm. The heads were cast integrally with the cylinders, but the intake and exhaust valves were set into a detachable section. In late 1915, the bore was increased to 4.1 inches (105 mm) leading to an increased displacement of 590 cubic inches (9.7 L) and power of 86 kW (115 hp) at 1,800 rpm.

Applications

Specifications (RAF 1a)

Template:Pistonspecs

See also

Related development

Related lists

References

Notes

Bibliography

Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens, 151. 

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.

Template:Royal Aircraft Factory aeroengines

cs:Royal Aircraft Factory R.A.F.1

This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "RAF 1".