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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
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