词条 | Beardmore 120 hp | |||||||||||||
释义 |
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){{pistonspecs||ref=Lumsden[2] |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) |diameter= |width=19.9 in (505 mm) |height=31.9 in (810 mm) |weight=545 lb (247 kg) |valvetrain=Overhead valve |supercharger= |turbocharger= |fuelsystem= |fueltype=Petrol |oilsystem= |coolingsystem=Water-cooled |power=154 hp (115 kW) at 1,400 rpm (maximum power) |specpower=0.18 hp/cu in (8.74 kw/L) |compression=4.85:1 |fuelcon= |specfuelcon= |oilcon= |power/weight=0.28 hp/lb (0.46 kW/kg) |designer= |reduction_gear=Direct drive, right-hand tractor |general_other= |components_other= |performance_other= }} See also{{aircontent|see also= |related=
|similar aircraft= |lists=
|similar engines=
}} ReferencesNotes1. ^Gunston 1989, p. 21. 2. ^Lumsden 2003, p. 83. Bibliography{{refbegin}}
External links{{Commons category|Beardmore 120 hp}}{{Beardmore aeroengines}} 2 : Aircraft piston engines 1910–1919|Beardmore aircraft engines |
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