BMW VI

BMW VI
BMW VI at the Technik-Museum Berlin
Type	V engine
Manufacturer	BMW
First run	1926

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

Contents 1 Design and development 2 Applications 3 Specifications (BMW VI) 4 See also 5 References 6 External links

Design and development

The first twelve-cylinder engine built by the Bayerische Motorenwerke AG, with a 60-degree included angle between the cylinder banks. The BMW VI was developed from the BMW IV by doubling the number of cylinders. 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 Ha-9.

Applications

• Albatros L 77
• Arado Ar 64
• Arado Ar 65
• Arado Ar 68
• Dornier Do 10
• Dornier Do 17
• Focke-Wulf Fw 42
• Heinkel He 45
• Heinkel He 51
• Heinkel He 59
• Heinkel He 60
• Heinkel He 70
• Kawasaki Type 92
• Tupolev TB-3 Mikulin M-17

Specifications (BMW VI)

Data from de:BMW VI

General characteristics

• Type: V-12
• Bore: 160 mm (6.3 in)
• Stroke: 190 mm (7.48 in)
• Displacement: 45.84 L (2,797.5 cuin)
• Length: 1810 mm (71.26 in)
• Width: 859 mm (33.82 in)
• Height: 1103 mm (43.43 in)
• Dry weight: 510 kg (1124 lb)

Components

• Fuel system: 2 x Zenith 60 DCL
• Fuel type: min. 87 octane gasoline
• Cooling system: Liquid-cooled

Performance

• Power output: 650 HP 641 hp
• Compression ratio: 5.50

See also

Related development

• Mikulin M-17
  

Comparable engines

• Liberty L-12
  

Related lists

• List of aircraft engines
  

References

• Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 25. 

External links

BMW aircraft engines Piston engines BMW IIIa · BMW IV · BMW V · BMW VI · BMW VI 5,5 · BMW VII A 7.3 · BMW X · BMW 114 · BMW 116 · BMW 117 · BMW 132 · BMW 139 · BMW 801 · BMW 802 · BMW 803 · Bramo 323 · BMW M2B15 Turbojets BMW 003 Turbofans BR700 Turboshafts 6012 · 6022

Imperial Japanese Army Air Service aeroengine designations 1-50 Ha-1 • Ha-5 • Ha-6 • Ha-9 • Ha-25 • Ha-26 • Ha-35 • Ha-40 • Ha-44 • Ha-45 51-100 Ha-60 • Ha-70 101-200 Ha-101 • Ha-102 • Ha-103 • Ha-104 • Ha-105 • Ha-112 • Ha-115 • Ha-140 • 200- Ha-201 • Ha-211 • Ha-214 • Ha-217 • Ha-505

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