Wikipedia

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.

Renault 12F
Renault 12Fe engine on display at the Polish Aviation Museum in Kraków
Type Water-cooled V12 aero engine
National origin France
Manufacturer Renault
Wolseley Motors
First run Late 1915
Major applications Breguet 14
Number built 12Fe: >7,000
Others: ~700
Developed from Renault 8G
Variants Renault 12Fe

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 320 hp (240 kW) variant which was designated as the 12Fe by the Service Technique de l'Aéronautique while being known, and marketed, as the 300 CV (cheval-vapeur) (French: "horsepower”) by Renault.

Design and development

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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 and stroke angle as the 8Gs. The series became known as the 12F.[1]

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.[2][3]

All engines in the series have ignition systems with 100% redundancy. Two spark plugs per cylinder and four magnetos (two per cylinder bank).[4][5]

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.[4][6] 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.[4] The device was not included in later models.[2][5][6]

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.[2]

In 1917, the 12Fe model was homologated with a nominal rating of 300 hp (224 kW) (later increased to 320 hp (239 kW)).[7] The 12Fe became the standard powerplant for the Breguet 14[8] and accounted for the vast majority of engines built from the series.[7]

12F series engines were exported to the United States[8] and produced in the United Kingdom.[9]

In Russia, Renault 12F engines were assembled from imported parts by the Russian Renault Society in Petrograd.[10][11] 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).[11]

Variants

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Publications often refer to the 12Fe as the Renault 300 hp with earlier engines in the series referred to as the Renault 220 hp.[6] Post WW1 the 12Fe engine was marketed as the 300 CV (cheval-vapeur) (French: "horsepower”).[12]

12Fa
(1915) Rating of 220 hp (164 kW) at 1300 rpm.[7][8] Used on the Breguet 14s and Henry Farman HF.35 prototypes.[7] The HF.35 made its first flight in December 1915.[13]
12Fb
(1916) Rating of 250 or 265 hp. Equipped the Paul Schmitt P.S.7[7] and the Breguet 5.[14]
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).[8]
12Fe
Main article: Renault 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.[8] The names 12Fe and 300 CV / hp (cheval-vapeur / horsepower) are used interchangeably in post war technical documentation.[15] Some of these engines were fitted with early experimental Rateau turbochargers.[16]
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.[16]

Applications

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Specifications (12Fc)

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Data from Angle,[3]

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

See also

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Related development

Comparable engines

Related lists

References

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  1. ^ Bodemer, Alfred (March 1985). "Les Premiers Constructeurs de Moteurs d'Avions Francais" [The first French aircraft engine manufacturers]. Pegase (in French) (37): 14.
  2. ^ a b c "Conferences sur les moteurs d'aviation 300 - 450 - 550 hp". Handout given to delegates at Renault factories (Annex A N.E. 21 & N.E. 21A). Renault. December 1921 – via Safran.
  3. ^ a b Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio, USA: The Otterbein Press. pp. 417–418.
  4. ^ a b c "Moteur d'aviation 220 chevaux" [Engine manual for 22L 220 hp model]. Renault.
  5. ^ a b "Moteur d'aviation 300 chevaux" [Engine manual for the 22L 300 hp engine]. Renault – via Safran.
  6. ^ a b c Les Moteurs D'Aviation Renault. Drager – via Safran.
  7. ^ a b c d e Hartmann, Gerard (2005). "Les moteurs d'aviation Renault" [Renault aviation engines] (PDF) (in French). Retrieved 10 December 2023.
  8. ^ a b c d e Toelle, Alan D (2003). "Motors and Cowlings". Breguet 14. Albatros Productions Limited (Windsock Datafile Special). pp. 52–53. ISBN 1902207610.
  9. ^ Lumsden, Alec (2002). British Piston Engines and their Aircraft. Airlife Publishing. p. 181. ISBN 1853102946.
  10. ^ "Klimov United Engine Corporation. Jsc klimov". Kupichic.ru. Retrieved 31 January 2013.
  11. ^ a b Kotelnikov, Vladimir (2010). Отечественные авиационные поршневые моторы. 1910–2009 [Domestic aircraft piston engines. 1910–2009] (in Russian). Litres. pp. 54–63. ISBN 978-5-91244-017-5.
  12. ^ Hatry, Gilbert (1984). Renault et l'aviation [Renault and aviation] (in French). Editions JCM. pp. 32–41 – via Safran.
  13. ^ Liron, J (1984). Les Avions Farman (in French). Docavia / Editions Lariviere. p. 46.
  14. ^ Treadwell, Terry (2011). "Société des Avions Louis Breguet". British and Allied Aircraft Manufacturers of the First World War. United Kingdom: Amberley. ISBN 9781445620091.
  15. ^ Type 14 A2. Model 1921 (PDF). Notice technique de l'avion Breguet (Report). Ministere de la guerre. 24 April 1922.
  16. ^ a b Bruce, J.M; Noel, Jean (1967). The Breguet 14. 157. United Kingdom: Profile Publications. ASIN B0007JXD5I.
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