BMW 114
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
Comparable engines
Related lists
References
    
    Notes
    
- Gunston 1989, p.25.
 
External links
    
| Wikimedia Commons has media related to BMW 114 aircraft engine. | 
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