Hiero 6

Hiero 6
	Hiero 6 engine of an Austro-Hungarian Phönix J.1 fighter biplane in a Swedish museum
Type	6-cyl water-cooled in-line piston engine
National origin	Austria
Manufacturer	Hiero / Laurin & Klement Automobile Works
Designer	Otto Hieronimus

In 1914 Otto Hieronimus manufactured the six-cylinder Hiero E, also known as the Hiero 6 engine which was derived from earlier 4-cylinder engines. The Hiero engine like the Austro-Daimler powered many of Austria's World War I aircraft. Hiero aircraft engines were designed by Otto Hieronimus, a famous Austrian auto racer of the early 1900s. His initial designs were liquid-cooled inline engines built by the Laurin & Klement Automobile Works of Austria.

Design and development

The Hiero E had a 135 mm x 180 mm bore/stroke (15.46L / 943.4cuin) and delivered 200-230 hp. The engine had the typical features of an inline vertical 6-cylinder: aluminum crankcase, cast iron cylinders, one inlet and one exhaust valve per cylinder controlled by bars and rockers, as part of a "SOHC" (single overhead camshaft) valvetrain like the Mercedes D-series aviation engines of the German Empire, and dual ignition with two Bosch magnetos. During World War I, the highly regarded Hiero engines were built under license by Essler, Warschalowski & Company of Vienna and the Breitfeld-Daněk company of Czechoslovakia. A point of recognition of Hiero engines compared with other Central Powers OHC inlines is that the intake was on the right and the exhaust on the left. After World War I, production was continued by the Avia company and powered a number of their early aircraft.

Variants

Hiero 145 hp: 145 hp (108.1 kW) (probably designated Hiero B or Hiero C )
Hiero 185 hp: 185 hp (138.0 kW) (probably designated Hiero D)
Hiero B
Hiero C
Hiero D
Hiero E: 200 hp (149.1 kW) - 230 hp (171.5 kW)
Hiero L
Hiero N: 230 hp (171.5 kW)

Applications

Specifications (Hiero E)

Data from World Encyclopaedia of Aero Engines.^[1]

General characteristics

Type: 6-cyl in-line Water-cooled
Bore: 135 mm (5.31 in)
Stroke: 180 mm (7.09 in)
Displacement: 15,459 cc (943.4 cu in)
Designer: Otto Hieronimus

Components

Valvetrain: overhead-cam
Cooling system: water

Performance

Power output: 200 - 230 hp (149 - 172 hp)

References

^ Gunston, Bill (2006). World Encyclopaedia of Aero Engines (5th ed.). Stroud. ISBN 0-7509-4479-X.{{cite book}}: CS1 maint: location missing publisher (link)