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Benz Bz.IV


FieldValue
nameBz.IV
imageBenz BZ 4S Aircraft Engine.jpg
captionA Benz Bz.IV at the National Air and Space Museum's Udvar-Hazy Center (2017)
engine_typeInline piston engine
national_originGermany
manufacturerBenz
first_runc. 1916
number_built6,400
developed_fromBenz 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

  1. Düsing, Michael. (2022). "German & Austro-Hungarian Aero Engines of WW1". Aeronaut Books.
  2. Grey, C.G.. (1969). "Jane's All the World's Aircraft 1919". David & Charles (Publishing) Limited.
Info: Wikipedia Source

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