| Type | Aircraft engine |
|---|---|
| National origin | France |
| Manufacturer | Loravia |
The Loravia LOR 75 is a French aircraft engine, designed and produced by Loravia of Yutz for use in ultralight aircraft. It was introduced in 2009.
By March 2018, the engine was no longer advertised on the company website and seems to be out of production.
Design and development
The LOR 75 is a three-cylinder four-stroke, in-line, 998 cc (60.9 cu in) displacement, liquid-cooled, automotive conversion petrol engine design, with a toothed poly V belt reduction drive with reduction ratios of 2.46 and 3.72:1. It employs electronic ignition and produces 75 hp (56 kW) at 6000 rpm, with a compression ratio of 10.5.
Applications
Specifications (LOR 75)
Data from Tacke
General characteristics
- Type: Three-cylinder, four stroke aircraft engine
- Bore: 71 mm (2.8 in)
- Stroke: 84 mm (3.3 in)
- Displacement: 998 cc (60.9 cu in)
- Dry weight: 75 kg (165.3 lb)
Components
- Fuel type: petrol
- Cooling system: liquid
- Reduction gear: toothed poly V belt
Performance
- Power output: 75 hp (56 kW)
See also
Related lists
References
- ^ Loravia (22 April 2009). "LOR 75 : ça plane pour lui". www.ulmag.fr. Retrieved 20 March 2018.
- ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, pages 258–259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Loravia (2010). "Find Your Engine". loravia.com. Retrieved 20 March 2018.