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{|{{Infobox aircraft begin
__NOTOC__
| name = Bz.III
The '''[[Benz]] Bz.III''' was a 6-cylinder, water cooled, inline engine developed in Germany for use in aircraft in [[1914 in aviation|1914]]. Developing 112 kW (150 hp) at 1,400 rpm from 875 cuin (14.3 L)<ref name="Smith 1981, p.53">Smith 1981, p.53.</ref>, it powered many German military aircraft during [[World War I]]. It was replaced in production by the unrelated [[Benz Bz.IIIa]] (140x190x6=17.55 L (1070.9cuin))<ref name="Smith 1981, p.53"/> and eventually the [[Benz Bz.IIIb]] (this latter engine a V-8).
| image =
| size =
| alt =
| caption =
}}
{{Infobox aircraft engine
|type =6-cylinder in-line water-cooled piston engine
<!-- The type of engine, eg: Air-cooled rotary, High-bypass turbofan -->
|national origin =[[Germany]]
<!-- The country where the engine was first manufactured. Use the main nation (ie. UK), not constituent country (England); don't use "EU". List collaborative programs of only 2 or 3 nations; for more than 3, use "Multi-national -->
|manufacturer =[[Benz & Cie.]]
<!-- The firm which manufactured the engine. -->
|designer =
<!-- The person or persons who designed the engine. Only appropriate for single designers, not project leaders -->
|first run =
<!-- The date that the engine was first run. If this hasn't happened, skip this field - don't speculate. -->
|major applications =
<!-- aircraft (or other vehicles) that were powered by this engine -->
|produced =
<!-- Years in production (eg. 1970-1999) if still in active use but no longer built -->
|number built =
|program cost =
<!-- Total program cost -->
|unit cost =
<!-- Incremental or flyaway cost for military or retail price for commercial aircraft -->
|developed from =
<!-- The engine which formed the basis for this engine -->
|variants with their own articles =
<!-- Variants OF this engine -->
|developed into=[[RBVZ-6]]}}
|}

The '''Benz Bz.III''' was a six-cylinder, [[water cooling|water-cooled]], [[Inline engine (aviation)|inline engine]] developed in Germany for use in aircraft in [[1914 in aviation|1914]]. Developing 112&nbsp;kW (150&nbsp;hp) at 1,400 rpm from 14.3 L (875 cu in),<ref name="Smith 1981, p.53">Smith 1981, p.53.</ref> it powered many German military aircraft during [[World War I]]. It was replaced in production by the unrelated [[Benz Bz.IIIa]].<ref>{{Cite web|url=http://www.aircraftinvestigation.info/airplanes/Benz_Bz.IIIa.html|title=Benz Bz.IIIa|website=aircraftinvestigation}}</ref><ref name="Smith 1981, p.53"/> and eventually the V-8 [[Benz Bz.IIIb]]. The Benz Bz.III was built under licence in [[Sweden]] by [[AB Thulinverken]], known as the '''Thulin E'''.


==Applications==
==Applications==
{{colbegin}}
* [[AEG C.I]]
* [[AEG C.I]]
* [[AEG C.II]]
* [[AEG C.II]]
* [[AEG C.III]]
* [[AEG C.III]]
* [[AEG C.IV]]
* [[AEG C.IV]]
* [[AEG G.II]]
* [[Albatros C.I]]
* [[Albatros C.I]]
* [[Albatros C.II]]
* [[Albatros C.II]]
* [[Albatros C.III]]
* [[Albatros C.III]]
* [[Albatros D.I]]
* [[Albatros D.I]]
* [[Albatros W.3]]
* [[Albatros G.II]]
* [[Albatros G.II]]
* [[Friedrichshafen FF.33]]
* [[Friedrichshafen FF.33]]
* [[Friedrichshafen FF.41]]
* [[Friedrichshafen FF.41]]
* [[Friedrichshafen G.I]]
* [[R-planes|R-Plane]] Germany's giant aircraft of WWI
* [[Gotha G.I]]
* [[Hansa-Brandenburg KDW]]
* [[Hansa-Brandenburg KDW]]
* [[Hansa-Brandenburg W.12]]
* [[Hansa-Brandenburg W.29]]
* [[Hansa-Brandenburg W.29]]
* [[LFG Roland D.VII]]
* [[Riesenflugzeug]]e – Germany's giant aircraft of WWI
{{colend}}

==Specifications==
{{pistonspecs|
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
<!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully formatted line with <li> -->
|ref=<ref name="Kyrill von Gersdorff 1981, p.19">Kyrill von Gersdorff 1981, p.19.</ref>
|type=[[Straight six|Six-cylinder]], [[Inline engine (aeronautics)|inline piston]] engine
|bore={{convert|130|mm|in|abbr=on|3}}
|stroke={{convert|180|mm|in|abbr=on|3}}
|displacement={{convert|14.3|L|cuin|abbr=on|0}}
|length=
|diameter=
|width=
|height=
|weight={{convert|270|kg|lb|abbr=on|0}}
|valvetrain=One [[camshaft]] in the engine block, driving one [[inlet valve|inlet]] and one [[exhaust valve]] per cylinder via pushrods and rocker arms ([[Overhead valve engine|overhead valve]]).
|supercharger=
|turbocharger=
|fuelsystem=
|fueltype=
|oilsystem=
|coolingsystem=[[Water cooling|Water-cooled]]
|power={{convert|112|kW|hp|abbr=on|0}} at 1,400 rpm
|specpower=8.4 kW/L
|compression=4.7
|fuelcon=
|specfuelcon=310 g/kWh
|oilcon=
|power/weight=

|designer=
|reduction_gear=

|general_other=
|components_other=
|performance_other=
}}

==See also==
{{aircontent
<!-- first, the related articles that do not fit the specific entries: -->
|see also=

<!-- designs which were developed into or from this aircraft or engine: -->
|related=

<!-- aircraft that are of similar role, era, and capability as this design: -->
|similar aircraft=

<!-- relevant lists that this aircraft appears in: -->
|lists=
* [[List of aircraft engines]]
<!-- For aircraft engine articles. Engines that are of similar to this design: -->
|similar engines=

<!-- See [[WP:Air/PC]] for more explanation of these fields. -->
}}


==References==
==References==
{{reflist}}
{{reflist}}
{{refbegin}}
* Smith, Herschel. ''Aircraft Piston Engines''. New York, New York: McGraw-Hill, 1981. ISBN 0-07-058472-9.
{{refend}}


==and==
==Bibliography==
{{cite book |last= Gunston |first= Bill |title=World Encyclopedia of Aero Engines |year=1986 |publisher=Patrick Stephens |location= Wellingborough |pages=22–23 }}
* {{cite book |last= Gunston |first= Bill |title=World Encyclopedia of Aero Engines |year=1986 |publisher=Patrick Stephens |location= Wellingborough |pages=22–23 }}
* Kyrill von Gersdorff, Kurt Grasmann. ''Flugmotoren und Strahltriebwerke'', Bernard & Graefe Verlag, 1981, {{ISBN|3-7637-5272-2}}
* Smith, Herschel. ''Aircraft Piston Engines''. New York: McGraw-Hill, 1981. {{ISBN|0-07-058472-9}}.

== External links ==
* {{cite web| title=Benz type FB, FD and FF aero engine manual | url=https://muzlot.nazwa.pl/digitalizacja/index.php?/category/1267 | date= | accessdate=21 September 2024 }}
* {{cite web| title=150 HP Benz aero engine manual 1917 | url=https://muzlot.nazwa.pl/digitalizacja/index.php?/category/851 | date=1917 | accessdate=21 September 2024 }}


{{Benz aeroengines}}
{{Benz aeroengines}}
{{Aviation lists}}


{{DEFAULTSORT:Benz Bz.Iii}}
{{DEFAULTSORT:Benz Bz.Iii}}
[[Category:Aircraft piston engines 1910-1919]]
[[Category:1910s aircraft piston engines]]
[[Category:Thulinverken]]

[[cs:Benz Bz.III]]
[[pl:Benz Bz.III]]

Latest revision as of 12:18, 21 September 2024

Bz.III
Type 6-cylinder in-line water-cooled piston engine
National origin Germany
Manufacturer Benz & Cie.
Developed into RBVZ-6

The Benz Bz.III was a six-cylinder, water-cooled, inline engine developed in Germany for use in aircraft in 1914. Developing 112 kW (150 hp) at 1,400 rpm from 14.3 L (875 cu in),[1] it powered many German military aircraft during World War I. It was replaced in production by the unrelated Benz Bz.IIIa.[2][1] and eventually the V-8 Benz Bz.IIIb. The Benz Bz.III was built under licence in Sweden by AB Thulinverken, known as the Thulin E.

Applications

[edit]

Specifications

[edit]

Data from [3]

General characteristics

Components

Performance

See also

[edit]

Related lists

References

[edit]
  1. ^ a b Smith 1981, p.53.
  2. ^ "Benz Bz.IIIa". aircraftinvestigation.
  3. ^ Kyrill von Gersdorff 1981, p.19.

Bibliography

[edit]
  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 22–23.
  • Kyrill von Gersdorff, Kurt Grasmann. Flugmotoren und Strahltriebwerke, Bernard & Graefe Verlag, 1981, ISBN 3-7637-5272-2
  • Smith, Herschel. Aircraft Piston Engines. New York: McGraw-Hill, 1981. ISBN 0-07-058472-9.
[edit]