Gnome-Rhône 14R-29
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The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the
Gnome-Rhône 14N The Gnome-Rhône 14N was a 14-cylinder two-row air-cooled radial engine designed and manufactured by Gnome-Rhône just before the start of World War II. A development of the Gnome-Rhône 14K, the 14N was used on several French and even one Ger ...
. The 14N
radial engine The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central crankcase like the spokes of a wheel. It resembles a stylized star when viewed from the front, and is ...
was itself an improved version of the popular pre-war Gnome-Rhône 14K ''Mistral Major'' series; designed and manufactured by
Gnome et Rhône Gnome et Rhône was a major French aircraft engine manufacturer. Between 1914 and 1918 they produced 25,000 of their 9-cylinder Delta and Le Rhône 110 hp (81 kW) rotary designs, while another 75,000 were produced by various licen ...
, a major French aircraft engine manufacturer whose origins pre-date the
First World War World War I (28 July 1914 11 November 1918), often abbreviated as WWI, was one of the deadliest global conflicts in history. Belligerents included much of Europe, the Russian Empire, the United States, and the Ottoman Empire, with fightin ...
. The improved 14R was initially known as the Gnome-Rhône 14P and then the Gnome-Rhône 14R. There were several improvements such as the introduction of a longer crankshaft and crankcase with a centre bearing, an increase in cylinder capacity, and a two-speed compressor. These changes allowed the engine to deliver 1,400hp at take-off and 1,300hp at 1,500m (1st gear) and 1200hp at 4000m (2nd gear). This came at the cost of a much increased total weight. It was expected that further development, such as the introduction of higher grade fuels, would lead to a power output of 1,660hp at low altitude. With the Fall of France, engine development was stopped under the occupation. After the war, development recommenced; however production of this engine after 1945 was transferred to the newly formed
SNECMA Safran Aircraft Engines, previously Snecma (''Société nationale d'études et de construction de moteurs d'aviation'') or Snecma Moteurs, is a French aerospace engine manufacturer headquartered in Courcouronnes and a subsidiary of Safran. It ...
and the engine was renamed the SNECMA 14R.


Variants

;14R-04:Improved higher performance using 92 Octane fuel. 14N with 2-speed supercharge (6.5:1 and 9:1), LH rotation, for take-off. ;14R-05:RH rotation version of 14R-4. ;14R-08:RPM increased from 2,400 to 2,600 improving power output. LH rotation. ;14R-09:RH rotation version of 14R-08 ;14R-24:LH rotation, . ;14R-25:RH rotation version of 14R-24. ;14R-26:LH rotation, . ;14R-27:RH rotation version of 14R-26. ;14R-28:LH rotation, . ;14R-29:RH rotation version of 14R-28. ;14R-32:LH rotation ;14R-100: ;14R-200:LH rotation ;14R-201:RH rotation ;14R-210: ;28T-1:28 cylinder, double 14R-24 engines placed back-to-back with co-axial contra-rotating propeller shafts, direct fuel injection, 2-speed supercharger, displacement, delivering for take-off using 100/130 octane fuel.


Specifications (14R-04)


See also


References

{{Snecma aeroengines 1930s aircraft piston engines Aircraft air-cooled radial piston engines 14R 14R