• Source: Renault 12F

The Renault 12F is a family of liquid-cooled 22 L (1,300 cu in) 50 deg V12 aircraft engines that saw widespread use during World War I and the 1920s.
The 12F series was developed from Renault's 8G engines with the two series sharing the same cylinder bore and stoke. 12F series engines were built in Renault's factories in France, Russia and the United Kingdom.
Renault designated early engines in the series by their nominal output of 220 hp (160 kW). The engines were progressively improved with the introduction of aluminum pistons allowing for increased power and reduced weight. These progressive improvements eventually lead to the development of a 300 hp (220 kW) variant which was designated as the 12Fe by the Service Technique de l'Aéronautique (STAe) while being known, and marketed, as the 300 CV (cheval-vapeur) (French: "horsepower”) by Renault.




Design and development


In 1914, Renault began building their first water cooled V8 aircraft engines which became known as the 8G series. In 1915, Renault's engineers added two more cylinders to produce a V12 engine with the same bore, stroke and bank angle as the 8Gs. The series became known as the 12F.
Engines in the series are V12s with a 50 degree angle between two rows of cylinders each of which has a single overhead camshaft. The crankshaft is carried on four plain bearings with master-and-slave connecting rods allowing corresponding cylinders in each row to be arranged directly opposite each other. Cylinders have a bore of 125 mm (4.92 in), a stroke of 150 mm (5.91 in) and are built in pairs with water circulated in welded liners.
All engines in the series have ignition systems with 100% redundancy. Two spark plugs per cylinder and four magnetos (two per cylinder bank).

The early 12F engines were often supplied with an aluminium six-cylinder radial pneumatic starter motor which was mounted on the back of the engine. The pneumatic motor allowed the engine to be restarted mid-flight or on the ground without assistance from ground crew. The starter motor was fed from a pressurised vessel with enough air for ten starts. The device was not included in later models.
In late 1915 the 220 hp (12Fa) model used cast iron pistons. The engines were progressively improved with the introduction of aluminum pistons allowing for increased power output and reduced weight.
In 1917, the 12Fe model was homologated with a nominal rating of 300 hp (224 kW) (later increased to 320 hp (239 kW)). The 12Fe became the standard powerplant for the Breguet 14 and accounted for the vast majority of engines built from the series.
12F series engines were exported to the United States and produced in the United Kingdom.
In Russia, Renault 12F engines were assembled from imported parts by the Russian Renault Society in Petrograd. A total of 98 engines were assembled from July 1916 to September 1917. All the engines assembled were early 12F models with cast iron pistons. In 1921 the 12F was re-designated as the M-3 under a new Soviet numbering system which included the M-1 (RBVZ-6) and the M-2 (Le Rhone 9J).




Variants


Publications often refer to the 12Fe as the Renault 300 hp with earlier engines in the series referred to as the Renault 220 hp. Post WW1 the 12Fe engine was marketed as the 300 CV (cheval-vapeur) (French: "horsepower”).

12Fa
(1915) Rating of 220 hp (164 kW) at 1300 rpm. Used on the Breguet 14s and Henry Farman HF.35 prototypes. The HF.35 made its first flight in December 1915.
12Fb
(1916) Rating of 250 or 265 hp. Equipped the Paul Schmitt P.S.7 and the Breguet 5.
12Fc
Used on early model Bréguet 14s. 12Fcx (250 hp (186 kW) at 1500 rpm) and 12Fcy (280 hp (209 kW) at 1600 rpm) sub-variants. In US service 12Fc engines were all rated at 300 hp (224 kW).
12Fe

Rated for 300 hp (224 kW) at 1600 rpm. Main production variant in the series and the standard power-plant in the Breguet 14 from early in 1918 onwards. The names 12Fe and 300 CV / hp (cheval-vapeur / horsepower) are used interchangeably in post war technical documentation. Some of these engines were fitted with early experimental Rateau turbochargers.
12Ff
Sometimes used to describe a small number of engines produced with increased bore (128 mm) and stroke (160 mm). Rated for 350 hp (261 kW) at 1,600 rpm. These engines were fitted to a few late production Breguet 14s.




Applications






= 12Fa, 12Fb and 12Fc

=

Breguet 5
Breguet 14
Henry Farman HF.35
Nieuport 15
Paul Schmitt P.S.7
Curtiss Wanamaker Triplane
Grigorovich M-24
Sikorsky Ilya Muromets




= 12Fe (300 hp)

=

Breguet 14 (from late 1917 onwards)
Breguet 16
Caudron C.91
Farman F.60 Goliath
Farman F.70
Georges Levy G.L.40
Hanriot HD.18
Latécoère 14
Latécoère 17
Lioré et Olivier LeO 8
Lioré et Olivier LeO H-13
Paul Schmitt P.S.10
Potez XV
Voisin X
Airco DH.4
Royal Aircraft Factory R.E.7
Short Type 184




Specifications (12Fc)


Data from Angle,




= General characteristics

=
Type: Water–cooled, upright, 50-degree, V-12 piston engine
Bore: 125 mm (4.92 in)
Stroke: 150 mm (5.91 in)
Displacement: 22.08 L (1,347 cu in)
Dry weight: 379 kg (836 lb)




= Components

=
Valvetrain: SOHC (single overhead camshafts). Two valves per cylinder.
Fuel system: Two Zenith duplex carburetors. Heated by water jacket.
Fuel type: Gasoline
Oil system: Wet sump. 2 Gear pumps. One pump circulates oil. The other pump transfers oil from tank to sump.
Cooling system: Water-cooled. Two centrifugal pumps.
Reduction gear: None. Direct drive.
Rotation: Counterclockwise when looking end on at the propeller hub




= Performance

=
Power output: 285 hp (213 kW) @ 1550 rpm
Compression ratio: 4.6:1
Specific fuel consumption: 0.315 kg/kWh (0.518 lb/(hp⋅h))
Oil consumption: 0.033 kg/kWh (0.055 lb/(hp⋅h))
Power-to-weight ratio: 0.561 kW/kg (0.341 hp/lb)




See also



Related development

Renault 8G - A family of V8 engines sharing the same cylinder size and bank angle as the 12F

Comparable engines

Liberty L-12
Peugeot 8Aa
Rolls-Royce Eagle
Sunbeam Cossack
Related lists

List of aircraft engines




References






External links


Moteur d'aviation 220 chevaux. Engine manual.

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