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Vaxell 100i

From Wikipedia, the free encyclopedia

100i
Type Aircraft engine
National origin Poland
Manufacturer Vaxell

The Vaxell 100i is a Polish aircraft engine, designed and produced by Vaxell of Bydgoszcz for use in ultralight and homebuilt aircraft.[1]

Design and development

The Vaxell 100i engine is a four-cylinder four-stroke, horizontally-opposed, 2,300 cc (140.4 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs dual electronic ignition, electronic, multipoint fuel injection and produces 90 hp (67 kW) at 3100 rpm.[1]

Specifications (80i)

Data from Tacke[1]

General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Displacement: 2,300 cc (140.4 cu in)
  • Length: 670 mm (26.4 in)
  • Width: 770 mm (30.3 in)
  • Height: 380 mm (15.0 in)
  • Dry weight: 74.85 kg (165.0 lb) dry weight

Components

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

Performance

  • Power output: 90 hp (67 kW) at 3100 rpm

See also

Related lists

References

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

External links

This page was last edited on 6 January 2022, at 00:11
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