| AG-12Si | |
|---|---|
| Type | Aircraft engine |
| National origin | France |
| Manufacturer | VIJA Aircraft Engines |
The VIJA AG-12Si 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 four-cylinder four-stroke, in-line, 1,216 cc (74.2 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 120 hp (89 kW) at 7100 rpm, with a compression ratio of 11.5.
Variants
- AG-12Si
- Base model with a weight of 84 kg (185.2 lb).
- AG-12Sbi
- Model with a weight of 79 kg (174.2 lb).
Specifications (AG-12Si)
Data from Tacke
General characteristics
- Type: Four cylinder, four stroke aircraft engine
- Bore: 81 mm (3.2 in)
- Stroke: 59 mm (2.3 in)
- Displacement: 1,186 cc (72.4 cu in)
- Length: 585 mm (23.0 in)
- Width: 485 mm (19.1 in)
- Height: 565 mm (22.2 in)
- Dry weight: 84 kg (185.2 lb)
Components
- Fuel system: Fuel injection
- Fuel type: petrol
- Cooling system: air
- Reduction gear: mechanical gearbox, reduction ratio 2.55:1
Performance
- Power output: 120 hp (89 kW) at 7100 rpm
- Compression ratio: 11.5:1
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.
- ^ VIJA Aircraft Engines (25 April 2018). "Produits". vija-engines.com. Archived from the original on 2 January 2013. Retrieved 15 April 2018.
External links
| VIJA Aircraft Engines | |
|---|---|
| Aircraft engines | |