BMW 114
| BMW 114 | |
|---|---|
 Preserved BMW-Lanova 114 diesel engine | |
| Type | Radial engine |
| Manufacturer | BMW |
| First run | 1935 |
| Developed from | BMW 132 |
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
- 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
Comparable engines
Related lists
References
Notes
- ↑ Gunston 1989, p.25.
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
Wikimedia Commons has media related to BMW 114 aircraft engine.
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