Walter Minor

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Type Inline piston engine
National origin Czechoslovakia
Manufacturer Walter Aircraft Engines
First run 1929



The Walter Minor is a family of four, six and twelve-cylinder inverted inline air-cooled engine used on light aircraft. First produced in 1929, the Minor engines have steel cylinders, aluminum heads and overhead valves, with identical bore and stroke of 105 mm (4.1 in) and 115 mm (4.5 in), respectively. Typical power ratings varied from 105 hp to 160 hp.[1] Today Avia continues to produce the Minor.

Variants

Minor Sc.
Minor M 337
Minor 4-I
Minor 4-II
Minor 4-III
Minor 6-I
Minor 6-II
Minor 6-III
Minor 12 1-MR
[2]

Applications

Specifications (Minor 4-cylinder)

Walter Minor 4-III

Data from: Oldengine.org [3]

General characteristics

  • Type: 4-cylinder inverted inline air-cooled
  • Bore: 105mm (4.14 in)
  • Stroke: 115mm (4.53 in)
  • Displacement: 4 Liter (244 cu in)
  • Length: 1,119mm (44.09 in)
  • Width: 440mm (17.32 in)
  • Height: 630mm (24.80 in)
  • Dry weight: 93kg (205 lb)

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cyclinder
  • Fuel system: 1 claudel carburetor
  • Fuel type: 68 octane
  • Cooling system: air-cooled

Performance

See also


Comparable engines
Related lists

References

  1. Gunston 1989, p.174.
  2. http://www.enginehistory.org/Museums/national_technical_museum.shtml. Retrieved 8 July 2013.  Missing or empty |title= (help)
  3. Oldengine.org

External links

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