BMW 116: Difference between revisions
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[[Category:BMW Aircraft engines]] |
[[Category:BMW Aircraft engines]] |
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[[Category:Aircraft piston engines 1930-1939]] |
[[Category:Aircraft piston engines 1930-1939]] |
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==References== |
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;Notes |
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;Bibliography |
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* Fred Jakobs, Robert Kröschel and Christian Pierer. "BMW aero engines". BMW Group Classic, 2009 ISBN 978-3-86852-214-3 |
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Revision as of 21:57, 3 March 2011
A piston aircraft engine derveloped by BMW in 1930s. Development work stopped in 1937 and BMW concentrated on air-cooled engines instead. The BMW 116 engine was initially known as BMW XII.
Specifications (BMW 116)
Data from de:BMW 116
General characteristics
- Type: V-12
- Bore: 130 mm
- Stroke: 130 mm
- Displacement: 20.7 L
- Length: 1637 mm
- Width: 740 mm
- Height: 915 mm
- Dry weight: 470kg
Components
- Supercharger: radial supercharger
- Fuel system: carburettor
- Cooling system: Liquid cooled
Performance
- Power output: 620 HP
- Compression ratio: 6.50
References
- Notes
- Bibliography
- Fred Jakobs, Robert Kröschel and Christian Pierer. "BMW aero engines". BMW Group Classic, 2009 ISBN 978-3-86852-214-3