Gnome et Rhône

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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 licensees, powering the majority of aircraft in the first half of the war on both sides of the conflict. In the post-war era they started a new design series originally based on the Bristol Jupiter, but evolving into the excellent 1,000 hp-class (750 kW) Gnome-Rhône 14K Mistral Major radial, which was likewise licensed and used around the world during World War II. They were nationalized as a part of Snecma in 1949, but the brand lived on for a time as the manufacturer of motorcycles.

Contents 1 World War I 2 Post-war 3 Licensed versions and developments 4 Engines 4.1 World War I 4.2 Between wars 4.3 World War II 5 References 6 External links

[edit] World War I

In 1900 the 26-year old French engineer Louis Seguin bought a license for the Gnome gas engine from the German firm Motorenfabrik Oberursel. Sold under the French translation, the Gnome was a single-cylinder stationary engine of about 4 hp (3 kW) that ran on kerosene (known in Germany as paraffin) intended to be used in industrial applications. The Gnom used a unique valve system with only one rod-operated exhaust valve, and a "hidden" intake valve located on the cylinder head.

On June 6, 1905 he and his brother Laurent formed the Société Des Moteurs Gnôme (the Gnome motor company) to produce automobile engines. They soon started development of one of the first purpose-designed aircraft engines, combining several Gnone cylinders into a rotary engine. The design emerged in the spring of 1909 as the 7-cylinder rotary Gnome Omega, delivering 50 hp (37 kW) from 75 kg. More than 1,700 of these engines would be built in France, along with license-built models in Germany, Sweden, Britain, the United States and Russia. The Gnome powered Henry Farman's Voisin to take the world records for distance and endurance, as well as powering the first aircraft to break 100 km/h, and powered France to become the leading country in aviation.

All of the Gnome's were known for their unique solutions to getting fuel to the top of the piston without using piping. Early models used two valves, one in the cylinder head and a second embedded in the piston itself, counterweighted to open at the end of the stroke. Without any springs or pushrods, the valve would pop open on the downstroke, allowing fuel to be drawn into the cylinder from the crankcase area. Unfortunately it was also very difficult to service, requiring the cylinder to be disassembled. In order to improve reliability and maintenance, later models used the Monosoupape (single-valve) system instead, using a single exhaust valve at the top of the cylinder and using a series of ports to allow the fuel mixture into the cylinder when the piston dropped far enough.

The basic Gnome design was then delivered in a series of larger engines. The Gnome Lambda of 1911 was a larger 80 hp (60 kW) version of the Omega, followed by the 9-cylinder Gnome Delta, also called the Gnome Monosoupape as it used that engine design philosophy (for the first time), of 100 hp in 1914. Gnome also tried their hand at a 14-cylinder two-row version, the Double Lambda of 160 hp (120 kW), but this saw little use, even though it was copied by Oberursel as the U.III in Germany, and used in a few early Fokker fighter designs without success. To deliver more power with the advent of high-power inline engines late in the war, a completely new 9-cylinder Monosoupape design was delivered in 1918 as the Type-N, delivering 160hp. This design saw use on the little known but excellent Nieuport 28.

Another French engineer, Louis Verdet, designed his own small rotary engine in 1910 which did not see much use. In 1912 he delivered a larger 7-cylinder design, the 7C, which developed 70 hp from 90 kg. This proved much more popular and he formed Société des Moteurs Le Rhône later that year. He soon followed the 7C with the larger Le Rhône 9C, a 9-cylinder design delivering 80 hp (60 kW). Compared to the Gnome's, the Le Rhône was considerably more "conventional", using copper pipes to bring the fuel to the top of the engine, along with intake and exhaust valves. Like Gnome, the Le Rhône designs were widely licensed, in this case the 9C was produced in Germany (by Oberursel, whose Le Rhone engine copies received an "Ur." prefix), Austria, Britain and Sweden.

After several years of fierce competition, Gnome and Le Rhône finally decided to merge. Negotiations started in 1914, and on January 12, 1915, Gnome bought out Le Rhône to form Société des Moteurs Gnome et Rhône. Developments of the 9C continued to be their primary product, improving in power to about 110 hp (80 kW) in the 9J by the end of the war. The 9-series was the primary engine for most early-war designs, both in French and English service, as well as in Germany where, perhaps somewhat ironically, Oberursel had taken out a license just before the war.

[edit] Post-war

With the end of the war the company rapidly diversified, using their factories to produce chassis and engines for the Rolland Pilain and Ricard-Pictet cars, along with Ansaldo diesel engines, refrigerators, sewing machines and even jackhammers. In 1920 they also introduced their first motorcycle, simply known as the Gnome et Rhône 500 cc. Various models were produced up to the early 1950s, typically advertised as simply "Gnome Rhone" with no accents.

By 1920 their rotary engines were no longer competitive, and they had no new designs of their own. In 1921 they took out a license for the Bristol Jupiter, which was in the process of becoming the Gnome of its era. In 1922, Paul-Louis Weiller, a WWI ace, took over the company and decided to focus it on aircraft engines once again. Their Jupiter designs, the 9A, were soon selling very well. In 1926 they took out a license for the smaller 5-cylinder Bristol Titan, while Bristol licensed the Farman-style reduction gearing used by Gnome.

Not satisfied to simply produce Bristol designs under license, Gnome started a major design effort based around the mechanicals of the Titan. The results were introduced in 1927 as the K-series, spanning the 260 hp (190 kW) Gnome-Rhône 5K Titan, the 7-cylinder 370 hp (270 kW) version, the Gnome-Rhône 7K Titan Major, and the 9-cylinder 550 hp (405 kW) Gnome-Rhône 9K Mistral. All of these engines were delivered in a variety of improved versions, named with a three letter code; the first letter was the series number (a through f for instance), the second a r or l depending on which direction the engine turned, and the third indicating the charging system. With the introduction of the K-series, Gnome ended royalty payments to Bristol. By 1930 they had delivered 6,000 Jupiters, Mistrals and Titans, making them the largest engine company in France.

But the 550 hp (405 kW) Mistral was no longer nearly enough power for the rapidly evolving industry. To serve the needs for higher power, Gnome once again turned to the two-row solution using two banks of 7-cylinders, delivering the 625 hp (460 kW) Gnome-Rhône 14K Mistral Major in 1929. The new engine was an instant hit. By 1933 the 14Kfrs had improved the power to 1,025 hp (750 kW) through better supercharging (along with similar improvements in the Mistral, now at 770 hp or 570 kW), and the engine was once again being licensed around the world.

Leaving the idea of having many engines in a single "K-series", Gnome continued work with the basic mechanical design to produce the 18-cylinder two-row Gnome-Rhône 18L of 1400 hp (1030 kW). Its power-to-weight ratio was not very good and work on the design was eventually stopped in 1939. A smaller engine, the Gnome-Rhône 14M Mars would be introduced to replace the earlier K-series Mistral, notable primarily for its extremely compact frontal area, giving by far the most power for size of any engine of the era. It was especially used in Potez 631 aircraft family.

In 1936 the 14K-series was replaced by the Gnome-Rhône 14N delivering 1,100 hp (810 kW) from a slightly heavier engine that nevertheless had a much better power-to-weight ratio. Starting with the N they introduced a new naming scheme, replacing the earlier model letters with numbers, delivering the engine in versions that turned left with even numbers and right with odd. The original 14N-0/1 was run through a number of versions, the 14N-10/11 seeing use on the Bloch MB.210 bomber, the 14N-25 on early examples of the Bloch MB.152 fighter, and the 14N-49 on late MB.152s as well as LeO 451s and Amiot 351s. The N-series finally ended with the 14N-50/51, which delivered 1,210 hp (890 kW) for takeoff. The 14N was not as widely licensed, as the war was approaching and the French government was becoming increasingly wary of licensing designs to potential enemies.

The 14N-series was itself replaced by the ultimate pre-war evolution of the line, the Gnome-Rhône 14R. The first versions introduced in 1939, the 14R-4/5, produced 1,291 hp (950 kW) for takeoff and was only slightly heavier than the 14N. By 1940 the improved 14R-8/9 was delivering 1,578 hp (1,161 kW) by increasing RPM from 2,400 to 2,600. Although this was a good figure for the era, British and German design had already passed this mark, and would soon be pressing on 2,000 hp (1,500 kW).

With the fall of France in 1940, Gnome et Rhône was ordered to produce the BMW 801 under license, while the 14M saw limited use on some German designs. The company became infamous for slow production, building only 8,500 engines by May 1944, when the Germans had been estimating 25,000. That month a massive US air raid completely destroyed the original Gennevilliers factories.

With the end of the war, the company was in no condition to continue in the aero-engine business, although they picked up small contracts to produce M4 Sherman tanks for the French army. In order to save what was left, the company was nationalized on May 29, 1945, creating the Société Nationale d'Etude et de Construction de Moteurs d'Aviation, or SNECMA. In snecma the company would again start production of the 14N, 14R and the new 14U.

[edit] Licensed versions and developments

The 14K was one of the most popular engines of its era, widely licensed and used around the world. In Poland it was used for export fighter variants, most notable PZL P.24. In particular it was used in Romania, where it powered a number of Polish designed PZL fighters before finally becoming the main engine of the little-known but interesting IAR 80 fighter.

Isotta Fraschini and Piaggio of Italy both took out licenses, the former producing the K.14, the latter the P.XI. These were used on a number of designs in the pre-war period, many of which were exported. This led to Manfred Weiss taking out a license in Hungary, producing it as the WM K-14 in order to power their versions of the Reggiane Re 2000 fighter.

A particularly important licensee was Nakajima, who produced it as the Sakae. The Sakae was one of the most popular Japanese engines, powering the Mitsubishi Zero fighter as well as other designs.

The British firm Alvis had licensed the 14K and 18L, but neither entered production before the war ended. Nevertheless Alvis pressed ahead with development, releasing the 9-cylinder Alvis 501 Leonides and later the 14-cylinder Alvis 701 Leonides Major. The later saw some use on post-war helicopter designs.

Soviet Union license-built both the 9A (as M-22) and the 14K (as M-85).

[edit] Engines

[edit] World War I

• Gnome Omega
• Gnome Lambda
• Gnome Delta
• Gnome Lambda-Lambda
• Le Rhône 9C
• Le Rhône 9J - referred to widely as "the 110hp Le Rhône"
• Gnome 9N Monosoupape

[edit] Between wars

• Gnome-Rhône 9A Jupiter
• Gnome-Rhône 5K Titan
• Gnome-Rhône 7K Titan Major
• Gnome-Rhône 9K Mistral
• Gnome-Rhône 14K Mistral Major
• Gnome-Rhône 18L

[edit] World War II

• Gnome-Rhône 14M Mars
• Gnome-Rhône 14N
• Gnome-Rhône 14R

[edit] References

• A History of Aircraft Piston Engines, Herschel Smith, Sunflower University Press, 1981

[edit] External links

• Gnome

- includes an animation of the Gnome valve system