Benz Bz.II
The Benz Bz.II was a 6-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.
Applications
References
Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 22–23. {{cite book}}: Cite has empty unknown parameter: |1= (help)