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.[1][2]
| Type | Aircraft engine |
|---|---|
| National origin | France |
| Manufacturer | Loravia |
By March 2018, the engine was no longer advertised on the company website and seems to be out of production.[3]
Design and development edit
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.[2]
Applications edit
Specifications (LOR 75) edit
Data from Tacke[2]
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 edit
Related lists
References edit
- ^ a b c d Loravia (22 April 2009). "LOR 75 : ça plane pour lui". www.ulmag.fr. Retrieved 20 March 2018.
- ^ a b c 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.