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Loravia LOR 75

From Wikipedia, the free encyclopedia

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]

Design and development

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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

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Specifications (LOR 75)

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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

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Related lists

References

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  1. ^ a b c d Loravia (22 April 2009). "LOR 75 : ça plane pour lui". www.ulmag.fr. Retrieved 20 March 2018.
  2. ^ 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
  3. ^ Loravia (2010). "Find Your Engine". loravia.com. Retrieved 20 March 2018.
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