Benz Bz IIIb: Forskjell mellom revisjoner
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==Specifications (Benz Bz.IIIb)== | ==Specifications (Benz Bz.IIIb)== | ||
8-cylinder liquid-cooled 60° V engine | |||
bore=135 mm | |||
stroke=135 mm | |||
displacement=15.5 L | |||
length=1,300 mm | |||
width=860 mm | |||
height=850 mm | |||
weight=257 kg | |||
valvetrain= | |||
supercharger= | |||
turbocharger= | |||
fuelsystem=Carburetor | |||
fueltype= | |||
oilsystem= | |||
coolingsystem=Liquid-cooled | |||
power=maximum 200 hp at 1,750 rpm | |||
specpower= | |||
compression= | |||
fuelcon= | |||
specfuelcon= | |||
oilcon= | |||
power/weight= | |||
==See also== | ==See also== |
Revisjonen fra 27. mar. 2015 kl. 22:10
Mal:Infobox Aircraft Engine |}
The Benz Bz.IIIb was an eight-cylinder, water-cooled, V-engine developed in Germany for use in aircraft in 1918.
Design and development
Inspired by the Hispano-Suiza 8, some of which were captured and tested, the Benz Bz.IIIb was a fairly large engine, but its performance was disappointing. Despite not being accepted for service use a number of late World War I prototype German aircraft used the Bz.IIIb, the Benz IIIbo and the geared Benz IIIbm. The latter suffered from vibration problems.[1]
Fly med denne motoren
- AEG DJ.I
- AEG PE
- Albatros D.X
- Albatros Dr.II
- LFG Roland D.VII
- LFG Roland D.VIII
Specifications (Benz Bz.IIIb)
8-cylinder liquid-cooled 60° V engine bore=135 mm stroke=135 mm displacement=15.5 L length=1,300 mm width=860 mm height=850 mm weight=257 kg valvetrain= supercharger= turbocharger= fuelsystem=Carburetor fueltype= oilsystem= coolingsystem=Liquid-cooled power=maximum 200 hp at 1,750 rpm specpower= compression= fuelcon= specfuelcon= oilcon= power/weight=
See also
Notes
Mal:Reflist Mal:Refbegin Mal:Refend
References
Mal:Benz aeroengines Mal:Aviation lists Mal:Aeroengine-specs
- ↑ Green & Swanborough (1994) p.339