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Limbach L275E : ウィキペディア英語版 | Limbach L275E
The Limbach L275E is a German aircraft engine, designed and produced by Limbach Flugmotoren of Königswinter for use in UAVs.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 240-241. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The L275E is a twin cylinder horizontally-opposed two-stroke, air-cooled, direct-drive gasoline engine design, based upon the Volkswagen air-cooled engine. It employs a single magneto ignition, two carburettors, is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 for synthetic oil and produces at 7200 rpm.〔
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