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词条 RAF 4
释义

  1. Turbocharger

  2. Variants

  3. Applications

     RAF 4  RAF 5 

  4. Engines on display

  5. Specifications (RAF 4a)

  6. See also

  7. References

     Notes  Bibliography 
name=RAF 4image=RAF4engine.JPGcaption=Preserved RAF 4a engine at the Science Museum (London)

}}{{Infobox Aircraft Engine

type=Piston inline aero enginemanufacturer=Royal Aircraft Factorydesigner=A.J. Rowledge1914}}major applications=Royal Aircraft Factory R.E.8number built = >3,600program cost =unit cost =developed from = RAF 1developed into =variants with their own articles =
}}

The RAF 4 was a British air-cooled, V12 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]

Turbocharger

In April 1918 a turbocharged experimental version of the RAF 4d was developed using a Rateau turbocharger, the engine being flown in the R.E.8 B738.[2]

Variants

RAF 4

1914 - Prototype engine, 140 horsepower (104 kW).

RAF 4a

1917 - Main production variant, 150 horsepower (112 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

  • Armstrong Whitworth F.K.8
  • Bristol F.2 Fighter
  • Royal Aircraft Factory B.E.12
  • Royal Aircraft Factory R.E.7
  • Royal Aircraft Factory R.E.8
  • Siddeley-Deasy R.T.1
  • Vickers F.B.14

RAF 5

  • Royal Aircraft Factory F.E.2
  • Royal Aircraft Factory F.E.4

Engines on display

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

Specifications (RAF 4a)

{{pistonspecs|
|ref=Lumsden[3]
|type=12-cylinder, upright, 60-degree Vee engine
|bore=3.94 in (100 mm)
|stroke=5.51 in (140 mm)
|displacement=806.15 cu in (13.2 L)
|length=
|diameter=
|width=
|height=
|weight=680 lb (308 kg)
|valvetrain=EOI (side-valve inlet, exhaust overhead)
|supercharger=
|turbocharger=
|fuelsystem=Twin Claudel-Hobson Mk.1A carburettors
|fueltype=
|oilsystem=
|coolingsystem=Air-cooled
|power=163 hp (122 kW) at 1,800 rpm (takeoff power)
|specpower=0.2 hp/cu in (9.2 kW/L)
|compression=4.3:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=0.24 hp/lb (0.4 kW/kg)
|reduction_gear=0.5:1, Left-hand tractor
|general_other=
|components_other=
|performance_other=
}}

See also

{{aircontent
|see also=
|related=
  • RAF 1

|similar aircraft=
|lists=
  • List of aircraft engines

|similar engines=
  • Rolls-Royce Falcon

}}

References

{{commons category}}

Notes

1. ^Gunston, 1989, p. 156.
2. ^http://www.theaerodrome.com/forum/aircraft/50719-increasing-charge-3.html
3. ^Lumsden 2003, p. 224.

Bibliography

{{refbegin}}
  • 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}}.
{{refend}}{{Royal Aircraft Factory aeroengines}}

1 : Aircraft piston engines 1910–1919

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