| 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. [1]
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.
This page was last edited on 17 April 2021, at 03:48