Beardmore 120 hp
The Beardmore 120 hp was a British six-cylinder, water-cooled aero engine that first ran in 1914, it was built by William Beardmore and Company as a licensed-built version of the Austro-Daimler 6. The engine featured cast iron cylinders and mild steel concave pistons. Produced between August 1914 and December 1918, the design powered many World War I aircraft types.[1]
Applications
Specifications (120 hp)
Data from Lumsden[2]
General characteristics
- Type: 6-cylinder, inline, upright piston engine
- Bore: 5.12 in (130 mm)
- Stroke: 6.89 in (175 mm)
- Displacement: 851 cu in (13.145 L)
- Length: 57 in (1,148 mm)
- Width: 19.9 in (505 mm)
- Height: 31.9 in (810 mm)
- Dry weight: 545 lb (247 kg)
Components
Performance
See also
- Related development
- Comparable engines
- Related lists
References
Notes
- ^ Gunston 1989, p. 21.
- ^ Lumsden 2003, p. 83.
Bibliography
- Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
- Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
External links
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