Loravia LOR 75

{{Short description|French aircraft engine}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

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}}{{Infobox Aircraft Engine

|type=Aircraft engine

|manufacturer=Loravia

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|national origin=France

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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.{{cite web|url = http://www.ulmag.fr/actu2009/reagir.php?a=0904222350|title = LOR 75 : ça plane pour lui|accessdate = 20 March 2018|author=Loravia |work = www.ulmag.fr|date = 22 April 2009 }}Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, pages 258–259. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

By March 2018, the engine was no longer advertised on the company website and seems to be out of production.{{cite web|url = http://loravia.com/shop/en/find-your-engine|title = Find Your Engine|accessdate = 20 March 2018|author= Loravia|work =loravia.com|year=2010}}

Design and development

The LOR 75 is a three-cylinder four-stroke, in-line, {{convert|998|cc|cuin|1|abbr=on}} 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 {{convert|75|hp|kW|0|abbr=on}} at 6000 rpm, with a compression ratio of 10.5.

Applications

Specifications (LOR 75)

{{pistonspecs|

|ref=Tacke

|type=Three-cylinder, four stroke aircraft engine

|bore={{convert|71|mm|in|1|abbr=on}}

|stroke={{convert|84|mm|in|1|abbr=on}}

|displacement={{convert|998|cc|cuin|1|abbr=on}}

|length=

|diameter=

|width=

|height=

|weight={{convert|75|kg|lb|1|abbr=on}}

|valvetrain=

|supercharger=

|turbocharger=

|fuelsystem=

|fueltype=petrol

|oilsystem=

|coolingsystem=liquid

|power={{convert|75|hp|kW|0|abbr=on}}

|specpower=

|compression=

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=

|designer=

|reduction_gear=toothed poly V belt

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See also

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References

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