Loravia LOR 75
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| Loravia LOR 75 | |
|---|---|
| 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.[1][2]
By March 2018, the engine was no longer advertised on the company website and seems to be out of production.[3]
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
Specifications (LOR 75)
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)