Jump to content

Benz Bz.II

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Cydebot (talk | contribs) at 00:47, 8 May 2019 (Robot - Moving category Aircraft piston engines 1910–1919 to Category:1910s aircraft piston engines per CFD at Wikipedia:Categories for discussion/Log/2019 April 19.). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Bz.II
Type 6-cyl. water-cooled in-line piston engine
National origin Germany
Manufacturer Benz & Cie

The Benz Bz.II was a six-cylinder, water-cooled, inline engine developed in Germany for use in aircraft in 1913. With a displacement of 14.3 L (875 cu in), it developed 75 kW (100 hp) at 1,200 rpm. It had cast-iron cylinders and the valves were operated by dual camshafts.[1]

Applications

Specifications (variant)

General characteristics

  • Type: 6-cyl. water-cooled in-line piston engine
  • Displacement: 14.34 L (875.1 cu in)

Performance

  • Power output: 75 kW (101 hp) at 1,200 rpm

References

  1. ^ Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 22–23.

Bibliography

  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 22–23.