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.

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

Notes

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Fred Jakobs, Robert Kröschel and Christian Pierer. "BMW Aero Engines". BMW Group Classic, 2009 ISBN 978-3-86852-214-3

External links