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BMW 114

1930s German piston aircraft engine From Wikipedia, the free encyclopedia

BMW 114
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The BMW 114 was a nine-cylinder air-cooled radial engine intended for military aircraft use. Developed in 1935 from the BMW 132, with which it could be interchanged, work did not progress beyond experimental prototype engines. [1]

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Specifications (BMW 114)

Data from BMW Aero Engines

General characteristics

Components

  • Supercharger: Single speed supercharger
  • Cooling system: Air- and liquid-cooled

Performance

  • Power output: 510 HP

See also

Related development

Comparable engines

Related lists

References

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