| J-16Ti | |
|---|---|
| Type | Aircraft engine |
| National origin | France |
| Manufacturer | VIJA Aircraft Engines |
| Produced | 2010-2015 |
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.
The company was founded in 2004 and went out of business in about 2015, ending production.
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, petrol 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.
Specifications (J-16Ti)
Data from Tacke
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
- Turbocharger: yes
- Fuel system: Fuel injection
- Fuel type: petrol
- Cooling system: air
- Reduction gear: mechanical gearbox, reduction ratio 2.55:1
Performance
- Power output: 160 hp (119 kW) at 7000 rpm
See also
Related lists
References
- ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- "Moteur Vija J-12Si". ulmag.fr. Retrieved 25 April 2018.
- "VIJA Engines". Internet Archive Wayback Machine. Retrieved 25 April 2018.
External links
| VIJA Aircraft Engines | |
|---|---|
| Aircraft engines | |