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Rapp Motorenwerke

From Wikipedia, the free encyclopedia

Rapp Motorenwerke GmbH
TypeGesellschaft mit beschränkter Haftung
IndustryManufacturing
Founded27 October 1913
FoundersKarl Rapp
Julius Auspitzer
Defunct21 July 1917
FateName changed to Bayerische Motorenwerke GmbH
SuccessorBMW
Headquarters,
ProductsAircraft engines

Rapp Motorenwerke GmbH was a German aircraft engine manufacturer in Munich. Founded in 1913, the company changed its name in 1917 to Bayerische Motorenwerke GmbH, which evolved into the automotive manufacturer known today as BMW.

Early engines

Karl Rapp and Julius Auspitzer founded the Rapp Motorenwerke GmbH on 27 October 1913 with a capital stock of RM 200,000. The company was established in Milbertshofen on the former site of the Munich branch of Flugwerk Deutschland GmbH, a firm at which Karl Rapp had held a leading position and that had gone into liquidation in the summer of 1913.[1] General Consul Auspitzer was the company's sole shareholder, with the operational side of the company managed by Karl Rapp. The company's stated purpose was to build and sell "engines of all types, in particular internal combustion engines for aircraft and motor vehicles".

With the acquisition of Flugwerk Deutschland, the company had also taken over the four-cylinder engines that Karl Rapp had developed there, and Rapp Motorenwerke immediately started to offer these engines to the Prussian military authorities as the Rapp 100 hp.[1][2] While the 100 hp four-cylinder engine was installed in some few contemporary aircraft, it apparently did not see a major success with the military authorities, which at this time by large already demanded six-cylinder engines due to their smoother operation. In addition to the four-cylinder engine, also the design of an 125 hp in-line six-cylinder engine with 215 kg (474 lb)[3] and a displacement of 14.8 l (901 cu in)[citation needed] for the second Kaiserpreis (Kaiser's Trophy) aircraft engine prize competition was started, but it was not completed in time.[2]

Further engine development based on the Rapp 100 hp led to the 150 hp Rapp Rp III inline-six engine in early 1914. Early into World War I, the output of the Rapp Rp III engine was increased to about 174 hp[2] (actual 162 hp @ 1400 rpm)[citation needed], but the engine generally met only little success with the German military authorities.[2] Also a Rapp 200 hp V-8 and a Rapp 300 hp V-12 engine with the same cylinder dimensions and the 125/145 hp Rapp Rp II V-8 of reduced cylinder dimensions were developed.

All of these engine designs were based on the Rapp 100 hp four-cylinder type and had overhead cam, with forged steel liners screwed to cast steel heads. Additionally, all the cylinders were in pairs. The aeroengines produced by Rapp were easily distinguished from the other aeroengines (Mercedes, Benz, Basse und Selve, etc.), because the vertical timing shaft that drove the overhead camshaft came up between the two rearmost cylinder pairs instead of at the rear end.

Wartime production

Rapp logo in an ad from 1916
Rapp logo in an ad from 1916

At the beginning of the First World War, the company was one of the key Bavarian companies for the war effort and appeared to have gained a certain reputation, despite the fact that none of the designs and developments achieved any real success. Since aircraft engine demand could not be met alone by the established companies like Argus, Daimler and Benz, the German military authorities also placed orders for engines at the Rapp-Motorenwerke.[2] With the influx of capital, the company expanded rapidly and employed 370 workers by end of September 1915.[2]

The first deliveries of Rapp engines however were rejected by the Prussian Army Administration as unsuitable, and so they refrained from further orders.[2] Despite this, the Bavarian Army administration as well as the German Navy administration still kept ordering Rapp engines in limited amounts, and also the Austro-Hungarian Army and the Austro-Hungarian Navy administrations, struggling with insufficient aircraft engine production, started ordering Rapp Rp II and Rapp Rp III engines. The engines were plagued with various problems like uneven running and vibrations, frequent bearing failures and problems with the carburetion,[2] which had been attributed to inadequate design of the engines in Austro-Hungarian reports.[1]

In response to a commission from the Prussian Army Administration, Karl Rapp further increased the output of his Rapp Rp III engine up to 175 hp.[2] However, the strengthening which this called for also increased the engine weight and vibrations. When the engine then finally also failed at the acceptance test in January 1916, no further orders were placed by the German authorities, and the Austro-Hungarian Navy remained the only customer.[2]

Later in 1916, Rapp also introduced a completely redesigned six-cylinder engine with four valves per cylinder, operated by a novel arrangement of pushrods and rocker arms from a single camshaft in the engine block.[4] While considered to be the Rapp IIIa by some sources,[4] the same name has also been used by other authors to refer to the 175 hp version of the Rapp Rp III engine with overhead camshaft.[5] Also the engine size and the choice of four valves per cylinder indicate the engine possibly being of a higher power class, such as the otherwise unknown 250 hp Rapp Rp IV six-cylinder engine.[6] Overall not much is known about this engine, it apparently was unable to gain any commercial success and could not improve the situation: the name Rapp had suffered to such an extent that the military departments no longer purchased engines from his company.

Meanwhile, Franz Josef Popp had noted the facilities of Rapp Motorenwerke were ideal for engine production, having the necessary workforce and equipment. Popp lobbied hard to manufacture, by license, the 12-cylinder Austro-Daimler aircraft engine. Popp succeeded in convincing the Bavarian Army Administration and the Imperial Naval Office of the Imperial Austro-Hungarian Army Administration to order Rapp engines licensed through Austro-Daimler. On behalf the Austrian war ministry, Popp was delegated to supervise the handling of the order in Munich. Popp was also the person who convinced Max Friz, an aircraft engine designer and engineer at Daimler, to come to Munich to assist in development and expansion. With Friz' arrival in 1916, the original Rapp designs were also worked on to create a "high altitude" aeroengine that would give the Imperial Army strategic air superiority in combat. 1917 marks the breakthrough by Friz and his team of engineers in developing the type III.

BMW Type III

On 20 May 1917, Rapp Motorenwerke registered the documentation for the construction design for the new engine, dubbed "type III". Friz' design, (based on Karl Rapp's original design) was laid out as an in-line six-cylinder, which guaranteed optimum balance, with few small vibrations. The engine was successful, but the real breakthrough came in 1917, when Friz integrated a basically simple throttle butterfly into the "high-altitude carburettor", enabling the engine to develop its full power high above the ground. This is precisely the reason why the engine, now dubbed "type IIIa", had unique superiority in air combat. Franz-Zeno Diemer, the pioneering aviator and test pilot for the company, sets a new world altitude record with a 32,000 ft (9,760 m) flight in 1919 flying a DFW F 37/III (experimental two-seater, often referred to as the C-IV) with a BMW Type IV aircraft engine. September of the same year, Diemer set another world altitude record- this one for a passenger aircraft (8 people on board, 6,750 meters) in a Junkers F 13 powered by a BMW IIIa aircraft engine.

Change of name

BMW IVa – this engine set the world altitude record in 1919 by Franz Zeno Diemer
BMW IVa – this engine set the world altitude record in 1919 by Franz Zeno Diemer

The decision by the Prussian Army Administration to order 600 units of the innovative high-altitude aeroengine (project name "BBE") prompted reorganizing the legal structure of the company. The aeroengine developed by Friz had turned Rapp Motorenwerke into an essential contributor to the war effort virtually overnight. From the middle of 1917 onward, the business, which would probably have disappeared from history never to be heard of again, now enjoyed the undivided attention of the armed services and other governmental bodies. Large subsidies flowed in and the Munich company received well-financed production orders.

The recognition that Max Friz gained with his engine made it clear to all the senior managers that, up to now, Karl Rapp and his inadequate engine designs had held the company back from success. In Friz, they now had an excellent chief designer on hand and were no longer dependent on Rapp. Therefore, on 25 July 1917, the partners in the company terminated Karl Rapp’s contract.

The end of this collaboration had been coming for a long time. When Rapp’s departure was finally a certainty, another important decision had to be made. If the man who had lent his name to the company was now leaving it, a new name was naturally required. So, on 21 July 1917, Rapp Motorenwerke GmbH was renamed Bayerische Motorenwerke GmbH. It was thus the first company to bear this name and to use the abbreviation “BMW”. BMW AG acknowledges this date to be the official beginning of the company we know today.[7]

The departure of Karl Rapp enabled a fundamental restructuring of BMW GmbH. While the development side was placed under Max Friz as Chief Designer, Franz Josef Popp took over the post of Managing Director. Until the end of the war, aeroengines remained the company's only product. The BBE aeroengine project was a big success under the designation BMW IIIa.

See also

References

  1. ^ a b c Pierer. 2011. pp. 9–19
  2. ^ a b c d e f g h i j Pletschacher. 1992, p. 124
  3. ^ Angle. 1921. p. 402
  4. ^ a b BMW Goup archives. Rapp IIIa
  5. ^ Grosz. 2000. pp. 5–7, 26
  6. ^ Huth. 1920. p. 232-233
  7. ^ "BMW Group". bmwgroup.com.

Bibliography

  • Pletschacher, Peter (1992). Die Königlich Bayerischen Fliegertruppen 1912-1919 (in German) (2 ed.). Planegg: Aviatic Verlag. ISBN 3-925505-20-2.

External links

This page was last edited on 31 January 2021, at 01:42
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