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BMW VI

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(Redirected fromBMW VI 7.3 Z)
Aircraft engine family by BMW
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BMW VI
BMW VI at the Technik-Museum Berlin
TypeV engine
ManufacturerBMW
First run1926
Major applications
Developed fromBMW IV
Developed into

TheBMW VI was awater-cooledV-12aircraft engine built in Germany in the 1920s. It was one of the most important German aero engines in the years leading up toWorld War II, with thousands built. It was further developed as theBMW VII andBMW IX, although these saw considerably less use. It was also produced in theSoviet Union as theM-17 and Japan as theKawasaki Ha-9.

Design and development

[edit]
Front view of the BMW VI

The BMW VI was the first twelve-cylinder engine built by the BMW. It essentially consisted of twocylinder banks from the six-cylinderBMW 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 byWolfgang von Gronau in an openDornier 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 theSoviet Union under the supervision ofMikulin, who then further developed it as theM-17. More license built engines were produced byKawasaki Heavy Industries in Japan as theKawasaki Ha9 (long designation:-Army Type 98 850hp Liquid Cooled In-line).

Variants

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5.5,6 or7.3 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).

BMW VI at the Technik-Museum Berlin
BMW VI 5.5
Compression ratio 5.5:1, 600–650 PS (592–641 hp) at up to 1600 rpm at sea level
BMW VI 6.0
Compression ratio 6:1, 630–660 PS (621–651 hp) at up to 1650 rpm at sea level,80 Octane fuel
BMW VI 7.3
Compression ratio 7.3:1 680–750 PS (671–740 hp) at up to 1700 rpm at sea level,87 Octane fuel
Mikulin M-17
Main article:Mikulin M-17
Licence production in the USSR
Kawasaki Ha9
(long designation:-Army Type 98 850hp Liquid Cooled In-line) licence production in Japan by Kawasaki

Applications

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BMW VI head detail

Specifications (BMW VI 7.3z)

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Side view of the BMW VI

Data fromFlugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944[1]

General characteristics

  • Type: V-12, 60° water-cooled piston engine
  • Bore: 160 mm (6.30 in)
  • Stroke: 190 mm (7.48 in) / 199 mm (7.83 in) (different between right and left cylinder bank due toarticulated connecting rods).
  • Displacement: 46.9 L (2,862.01 cu in)
  • Length: 1,810 mm (71.26 in)
  • Width: 859 mm (33.82 in)
  • Height: 1,103 mm (43.43 in)
  • Dry weight: 510 kg (1,124 lb)

Components

Performance

  • Power output:
  • 750 PS (740 hp; 552 kW) for takeoff at 1,700 rpm (1 minute) at sea level
  • 690 PS (681 hp; 507 kW) at 1,650 rpm (5 minutes) at sea level
  • 620 PS (612 hp; 456 kW) at 1,590 rpm (30 minutes) at sea level
  • 550 PS (542 hp; 405 kW) at 1,530 rpm (max. duration) at sea level
  • 0.23 kg/PSh (0.514 lb/(hp⋅h); 0.313 kg/kWh) at 1,590 rpm
  • 0.225 kg/PSh (0.503 lb/(hp⋅h); 0.306 kg/kWh) at 1,530 rpm
  • Oil consumption: 0.003–0.01 kg/PSh (0.007–0.022 lb/(hp⋅h); 0.004–0.014 kg/kWh) at 1,530 rpm
  • Power-to-weight ratio: 1.47 PS/kg (0.66 hp/lb; 1.08 kW/kg)
  • B.M.E.P.: 6.9 atm (7.0 bar; 101 psi)

See also

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Related development

Comparable engines

Related lists

References

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  1. ^Schneider, Helmut (Dipl.Ing.) (1944).Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 (in German) (Facsimile reprint 1986 ed.). Leipzig: Herm. Beyer Verlag. p. 365.ISBN 381120484X.{{cite book}}:ISBN / Date incompatibility (help)

Further reading

[edit]
Wikimedia Commons has media related toBMW VI.
  • Gunston, Bill (1986).World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 25.
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Imperial Japanese Army Air Service aero engine designations
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