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]

BMW 114
Preserved BMW-Lanova 114 diesel engine
Type	Radial engine
Manufacturer	BMW
First run	1935
Developed from	BMW 132

Specifications (BMW 114)

Data from BMW Aero Engines

General characteristics

• Type: 9-cylinder radial engine
• Bore: 155.5 mm
• Stroke: 162 mm
• Displacement: 27.7 L

Components

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

Performance

• Power output: 510 HP

See also

Related development

• BMW 132
• Pratt & Whitney R-1690

Comparable engines

• Bristol Phoenix
• Packard DR-980

Related lists

• List of aircraft engines

References

Notes

Bibliography

External links

Wikimedia Commons has media related to BMW 114 aircraft engine.

• BMW 114 at BMW Group archives

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[de] BMW 114 (Flugmotor)

[it] BMW 114