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Engine

BMW 116

Aircraft Engines

The BMW 116 was a piston aircraft engine that BMW developed in the 1930s, first under the designation BMW XII. It was a liquid-cooled V12 with a bore and stroke of 130 mm each, giving a displacement of 20.7 litres, and it used carburettor fuel feed with a radial supercharger. The engine was rated at 620 horsepower (460 kW) with a compression ratio of 6.5 to 1, and it weighed 470 kg dry, with an overall length of 1,637 mm. Development work stopped in 1937, so the engine remained a stage in BMW's line of large liquid-cooled aero engines and not a production powerplant. The comparable engines the source names are the Junkers Jumo 210 and the Rolls-Royce Kestrel.

Facts
Classification
Configuration
V-Configuration 1
Cylinder Count
12 1
Connections

Of Make

Source BMW 116 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source BMW 116 (Wikipedia)Lead, developer
Quote, Lead, developer
The BMW 116 was a piston aircraft engine developed by BMW in the 1930s.
Sources
1. BMW 116 (Wikipedia)
  • Specifications, general characteristics
    Type: V12
  • Specifications, cylinder layout
    Type: V12
  • Lead, developer
    The BMW 116 was a piston aircraft engine developed by BMW in the 1930s.
  • In Group: Piston Aero Engines, Lead
    The BMW 116 was a piston aircraft engine developed by BMW in the 1930s.
  • Of Make: BMW, Lead, make
    The BMW 116 was a piston aircraft engine developed by BMW in the 1930s.
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