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Benz Bz.IV
| Field | Value |
|---|---|
| name | Bz.IV |
| image | Benz BZ 4S Aircraft Engine.jpg |
| caption | A Benz Bz.IV at the National Air and Space Museum's Udvar-Hazy Center (2017) |
| engine_type | Inline piston engine |
| national_origin | Germany |
| manufacturer | Benz |
| first_run | c. 1916 |
| number_built | 6,400 |
| developed_from | Benz Bz.III |
The Benz Bz.IV was a German six-cylinder, water-cooled, inline engine developed for aircraft use. Deliveries began in 1916, and some 6,400 were produced.
Design and development
The Bz.IV was a dual-camshaft design, with two intake and two exhaust valves per cylinder. The cylinders were cast iron surrounded by a sheet metal cooling jacket. The crankcase was aluminium and pistons were initially steel but later versions had aluminium pistons. A high compression version of the engine (Bz IVsü) was produced from 1917 onwards. In February 1918, pistons from a Bz.IV were the first captured aluminium pistons to be examined by the British Ministry of Munitions.{{Cite journal
Variants
;IV : (1916) Main production variant produced by Benz & Cie.
;IVmarta : (1916) Licensed production of the Benz Bz.IV in Austria-Hungary by Magyar Automobil Részvény Társaság Arad (MARTA). The Marta produced version was heavier and had a lower compression ratio than the German original.
;IVsü : (1917) Overcompressed version producing 275 hp at altitudes above 2000 m. Also known as the IVs, IVü or IVaü. The "ü" in the model description stands for überverdichtet (German: "overcompressed”) while the "s" denotes the use of steel cylinder liners.
Applications
- AEG C.VI
- AEG J.I
- AGO C.IV
- Albatros C.VII
- Albatros C.XIV
- Albatros J.I
- Chitty 2 (racing car)
- DFW C.V
- Dobi-II
- Friedrichshafen FF.49
- Friedrichshafen G.II
- Halberstadt C.III
- Halberstadt C.V
- Junkers J.I
- LFG Roland C.III
- LVG C.VI
- NAVO RK-P4/220
- Pfalz D.XII
- Pfalz D.XIV
- Siemens-Schuckert R.III
- Siemens-Schuckert R.IV
- Siemens-Schuckert R.V
- Siemens-Schuckert R.VI
- Zeppelin-Staaken R.IV
- Zeppelin-Staaken R.XVI
Specifications
| and start a new, fully-formatted line with -- |power/weight= 0.3796 kW/kg (0.231 hp/lb)
References
Bibliography
- Kroschel, Gunter and Helmust Stützer. (1977) Die deutschen Militarflugzeuge 1910-1918 Wilhelmshaven: Lohse-Eissing Mittler.
References
- Düsing, Michael. (2022). "German & Austro-Hungarian Aero Engines of WW1". Aeronaut Books.
- Grey, C.G.. (1969). "Jane's All the World's Aircraft 1919". David & Charles (Publishing) Limited.
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