VIJA J-16Ti

The VIJA J-16Ti is a French aircraft engine, designed and produced by VIJA Aircraft Engines of Toulouse for use in ultralight and homebuilt aircraft.[1]

J-16Ti
Type Aircraft engine
National origin France
Manufacturer VIJA Aircraft Engines
Produced 2010-2015

The company was founded in 2004 and went out of business in about 2015, ending production.[2][3]

Design and development

The engine is a turbocharged, four-cylinder four-stroke, in-line, 1,186 cc (72.4 cu in) displacement, 16 valve, air-cooled, fuel injected motorcycle conversion, gasoline engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.55:1. It employs electronic ignition and produces 160 hp (119 kW) at 7000 rpm.[1]

Specifications (J-16Ti)

Data from Tacke[1]

General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 80 mm (3.1 in)
  • Stroke: 58 mm (2.3 in)
  • Displacement: 1,186 cc (72.4 cu in)
  • Length: 585 mm (23.0 in)
  • Width: 610 mm (24.0 in)
  • Height: 570 mm (22.4 in)
  • Dry weight: 88 kg (194.0 lb)

Components

Performance

  • Power output: 160 hp (119 kW) at 7000 rpm

See also

Related lists

References

  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. "Moteur Vija J-12Si". ulmag.fr. Retrieved 25 April 2018.
  3. "Internet Archive Wayback Machine". archive.org. Retrieved 25 April 2018.
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