Английская Википедия:BMW VI

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Шаблон:Nofootnotes

The BMW VI was a water-cooled V-12 aircraft engine built in Germany in the 1920s. It was one of the most important German aero engines in the years leading up to World War II, with thousands built. It was further developed as the BMW VII and BMW IX, although these saw considerably less use. It was also produced in the Soviet Union as the M-17 and Japan as the Kawasaki Ha-9.

Design and development

Файл:BMW VI Front Side.jpg
Front view of the BMW VI

The BMW VI was the first twelve-cylinder engine built by the BMW. It essentially consisted of two cylinder banks from the six-cylinder BMW IV bolted to a common cast aluminium crankcase at a 60-degree included angle between the cylinder banks. Series production commenced in 1926 after type approval had been granted. From 1930 on, after 1000 engines of the BMW VI type had already been delivered, Germany was again permitted to construct military aircraft. The sudden additional demand resulted in the production figures increasing rapidly. In 1933 the BMW VI was used for BMW's first experiments with direct fuel injection.

The BMW VI was the chosen source of power for numerous record-breaking and long-distance flights, including an east-to-west crossing of the Atlantic in 1930 and a round-the world flight in 1932, both by Wolfgang von Gronau in an open Dornier Wal flying boat powered by two BMW VI engines.

The BMW VI was put to unusual use as a power unit for the "Rail Zeppelin" high-speed railcar. Many versions of the BMW VI engine were developed, and it was built under license in Japan and the Soviet Union. This was further evidence of the reliability of an engine with which BMW made a fundamental contribution to the build-up of German air transport. At least 9,200 were built between 1926 and 1938. The engine was license-built in the Soviet Union under the supervision of Mikulin, who then further developed it as the M-17. More license built engines were produced by Kawasaki Heavy Industries in Japan as the Kawasaki Ha9 (long designation:- Army Type 98 850hp Liquid Cooled In-line).

Variants

5.5, 6 or 7.3 denotes compression ratio. No additional letter denotes BMW carburetor and direct-drive propeller (7.3), u denotes a propeller reduction gear (7.3u), z denotes Zenith carburetor (7.3z), zu denotes Zenith carburetor and propeller reduction gear (7.3zu).

Файл:BMW VI right side front.jpg
BMW VI at the Technik-Museum Berlin
BMW VI 5.5
Compression ratio 5.5:1, Шаблон:Convert at up to 1600 rpm at sea level
BMW VI 6.0
Compression ratio 6:1, Шаблон:Convert at up to 1650 rpm at sea level, 80 Octane fuel
BMW VI 7.3
Compression ratio 7.3:1 Шаблон:Convert at up to 1700 rpm at sea level, 87 Octane fuel
Mikulin M-17
Шаблон:Main Licence production in the USSR
Kawasaki Ha9
(long designation:- Army Type 98 850hp Liquid Cooled In-line) licence production in Japan by Kawasaki

Applications

Файл:BMW VI valve covers.jpg
BMW VI head detail

Шаблон:Div col

Шаблон:Col div end

Specifications (BMW VI 7.3z)

Файл:BMW VI-106.jpg
Side view of the BMW VI

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

Further reading

Шаблон:Commons category Шаблон:BMW aeroengines Шаблон:Japanese Imperial Army aeroengines