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Curtiss D-12

From Wikipedia, the free encyclopedia
(Redirected fromCurtiss D-12E)
V12 aircraft engine
D-12/Felix
Preserved D-12 engine
TypeV-12piston engine
ManufacturerCurtiss Aeroplane and Motor Company
First run1923

TheCurtiss D-12, sometimes identified with the military designationCurtiss V-1150, was anaircraft engine of 18.8 literdisplacement. It was a water-cooledV12, producing 443 hp (330 kW) and weighing 693 lb (314 kg). It was designed byArthur Nutt in 1921 and used in theCurtiss CR-3 for the 1923Schneider Trophy race.Fairey Aviation of England imported 50Curtiss-built examples in 1926, renaming them theFairey Felix.[1][2]

The D-12 was one of the first truly successfulaluminum cast-block engines and was extremely influential in the interwar period. Numerous engines trace their design to the D-12, among them thePackard 1A-1500,Rolls-Royce Kestrel andJunkers Jumo 210.

Applications

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D-12

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Felix

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Specifications (Curtiss D-12/Felix)

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Data fromLumsden.[3]

General characteristics

  • Type: 12-cylinder liquid-cooled 60-degree V
  • Bore: 4.5 in (114.3 mm)
  • Stroke: 6.0 in (152.4 mm)
  • Displacement: 1,145 cu in (18.8 L)
  • Length: 56.75 in (1441 mm)
  • Width: 28.25 in (717.5 mm)
  • Height: 34.75 in (882.6 mm)
  • Dry weight: 693 lb (314 kg)

Components

  • Cooling system: Liquid-cooled

Performance

See also

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Comparable engines

Related lists

References

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Notes

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  1. ^Lumsden 2003, p.148.
  2. ^Skyways. July 1999.{{cite journal}}:Missing or empty|title= (help)
  3. ^Lumsden 2003, p.149.

Bibliography

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

External links

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Wikimedia Commons has media related toCurtiss D-12.
Inline engines
Radial engines
Four-stroke piston engines
H (four-bank
H-configuration inline)
IV (inverted-V inline)
L (single-bank inline)
O (opposed)
R (radial)
V (upright-V inline)
V (inverted-V inline)
VG (inverted-V inline)
W (three-bank
W-configuration inline)
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