Lorraine 12F Courlis
| 12F Courlis | |
|---|---|
| Type | Water-cooled W-12 piston engine | 
| National origin | France | 
| Manufacturer | Lorraine-Dietrich | 
| First run | Homologated 21 August 1929 | 
The Lorraine 12F Courlis was a W-12 (broad arrow) aero engine introduced in France in 1929. It was not widely used.
Design and development
In 1926 Lorraine introduced a series of V-12 and W-12 engines with steel cylinders screwed into aluminium alloy engine blocks. There were two W-12s which shared the name Courlis (Curlew), the first of them was the 12E which provided 340 kW (450 hp) from a swept volume of 24.4 L (1,490 cu in). This was followed by the larger 12F, giving 450 kW (600 hp) from 31.7 L (1,930 cu in).[1][2]
The 12F was officially homologated on 21 August 1929[2] and displayed at the 1930 Paris Salon.[3] Unlike the 12E, which powered many different aircraft types, the 12F was not so widely used.
Variants
- Lorraine 12Fa
 - Lorraine 12Fb
 - Lorraine 12Fd
 
Applications
- Hanriot A.3 (1924 STAé specification ?)
 - I.A.R. CW-8
 - Nieuport-Delage NiD.540
 - Nieuport-Delage NiD.580
 - Nieuport-Delage NiD.623
 - Potez 50
 - SAB AB-20
 
Specifications (12Fa)
Data from L'Aérophile January 1930[2]
General characteristics
- Type: Water-cooled W-12 four-stroke engine
 - Bore: 145 mm (5.7 in)
 - Stroke: 160 mm (6.3 in)
 - Displacement: 31.7 L (1,930 cu in)
 - Length: 1.656 m (5 ft 5.2 in)
 - Width: 1.140 m (3 ft 8.9 in)
 - Height: 1.062 m (3 ft 5.8 in)
 - Dry weight: 430 kg (950 lb) without propeller, with Viet starter
 
Components
- Valvetrain: 4 valves/cylinder, 3 overhead camshafts
 - Fuel system: 2 fuel pumps; 6 Zenith carburetters with automatic altitude correction and heated inlets; 2 fixed advance magnetos
 - Fuel type: Petrol
 - Oil system: Pumped
 - Cooling system: Centrifugal water pump
 - Reduction gear: optional
 - Construction: Steel cylinder in aluminium block; aluminium cylinder head; aluminium pistons; 5 bearing crankshaft
 
Performance
- Power output: 450 kW (600 hp) at 2,000 rpm nominal; maximum 490 kW (660 hp)
 - Compression ratio: 6
 - Specific fuel consumption: 0.34 kg/(kW.h) (0.51 lb/(hp.h))
 - Oil consumption: 4.2 kg/h (9.3 lb/h)
 
References
- ^ Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2 ed.). Wellingborough: Patrick Stephens Ltd. p. 95. ISBN 1-85260-163-9.
 - ^ a b c "Le Moteur Lorraine 600 CV (12Fa)". L'Aérophile. 38 (1–2): 23. 1–15 January 1930.
 - ^ "Premier regard sur les moteurs". Les Ailes (493): 13. 15. 27 November 1930.