avia.wikisort.org - EngineThe Curtiss D-12, sometimes identified with the military designation Curtiss V-1150, was an aircraft engine of 18.8 liter displacement. It was a water-cooled V12, producing 443 hp (330 kW) and weighing 693 lb (314 kg). It was designed by Arthur Nutt in 1921 and used in the Curtiss CR-3 for the 1923 Schneider Trophy race. Fairey Aviation of England imported 50 Curtiss-built examples in 1926, renaming them the Fairey Felix.[1][2]
The D-12 was one of the first truly successful aluminum cast-block engines and was extremely influential in the interwar period. Numerous engines trace their design to the D-12, among them the Packard 1A-1500, Rolls-Royce Kestrel and Junkers Jumo 210.
Applications
D-12
Felix
Specifications (Curtiss D-12/Felix)
Data from Lumsden.[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
- Power output: 443 hp (330 kW) at 2,200 rpm
- Compression ratio: 6:1
See also
Comparable engines
Related lists
References
Notes
- Lumsden 2003, p.148.
- Skyways. July 1999.
- Lumsden 2003, p.149.
Bibliography
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
|
---|
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) | |
---|
- See also: X-1800
- US military gas turbine aeroengines
- Piston engine configurations
|
На других языках
[de] Curtiss D-12
Der Curtiss D-12 (militärisch auch Curtiss V-1150) ist ein wassergekühlter V-12-Flugmotor des US-amerikanischen Herstellers Curtiss Aeroplane and Motor Company Incorporated.
- [en] Curtiss D-12
[fr] Curtiss D-12
Le Curtiss D-12 est un moteur d'avion de 18,8 litres. C'était un V12 refroidi par eau, d'une puissance de 443 ch (330 kW) et pesant 314 kg. Il a été conçu par Arthur Nutt et utilisé dans le Curtiss CR-3 (en) pour la Coupe Schneider de 1923. La compagnie anglaise Fairey Aviation a importé 50 exemplaires, construits par Curtiss, en 1926 et les a rebaptisés Felix Fairey[2].
[it] Curtiss D-12
Il Curtiss D-12 fu un motore aeronautico dodici cilindri a V raffreddato a liquido sviluppato dall'azienda statunitense Curtiss Aeroplane and Motor Company nei primi anni venti.
Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
2019-2025
WikiSort.org - проект по пересортировке и дополнению контента Википедии