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Vaxell 80i

From Wikipedia, the free encyclopedia

80i
TypeAircraft engine
National originPoland
ManufacturerVaxell

The Vaxell 80i is a Polish aircraft engine, designed and produced by Vaxell of Bydgoszcz for use in ultralight and homebuilt aircraft.[1]

Design and development

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The Vaxell 80i engine is a four-cylinder four-stroke, horizontally opposed, 1,900 cc (115.9 cu in) displacement, air-cooled, direct-drive, petrol engine design. It employs dual electronic ignition, electronic, multipoint fuel injection and produces 80 hp (60 kW) at 3100 rpm.[1]

Specifications (80i)

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Data from Tacke[1]

General characteristics

  • Type: Four-cylinder, four-stroke aircraft engine
  • Displacement: 1,900 cc (115.9 cu in)
  • Length: 670 mm (26.4 in)
  • Width: 770 mm (30.3 in)
  • Height: 380 mm (15.0 in)
  • Dry weight: 73.5 kg (162.0 lb) dry weight

Components

  • Fuel system: electronic, multipoint fuel injection
  • Fuel type: petrol
  • Cooling system: air
  • Reduction gear: none

Performance

  • Power output: 80 hp (60 kW) at 3100 rpm

See also

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Related lists

References

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  1. 1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
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