| 词条 | Sodemo V2-1.2 | |||||||||||||||
| 释义 |
The Sodemo V2-1.2 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.[1] Design and developmentThe engine is a 90° V-twin-cylinder four-stroke, {{convert|1200|cc|cuin|1|abbr=on}} displacement, liquid-cooled, gasoline engine design, with a mechanical helical-gear gearbox reduction drive. It employs dual capacitor discharge ignition and produces {{convert|136|hp|kW|0|abbr=on}}.[1] Specifications (V2-1.2){{pistonspecs||ref=Tacke[1] |type=Twin cylinder, four stroke aircraft engine |bore= |stroke= |displacement={{convert|992|cc|cuin|1|abbr=on}} |length= |diameter= |width= |height= |weight= |valvetrain= |supercharger= |turbocharger= |fuelsystem= |fueltype=gasoline |oilsystem= |coolingsystem=liquid |power={{convert|136|hp|kW|0|abbr=on}} |specpower= |compression= |fuelcon= |specfuelcon= |oilcon= |power/weight= |designer= |reduction_gear= |general_other= |components_other= |performance_other= }} See also{{aircontent|see also= |related=*Sodemo V2-1.0 |similar aircraft= |lists= *List of aircraft engines }} References1. ^1 2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}} External links
3 : Sodemo aircraft engines|Liquid-cooled aircraft piston engines|Aircraft piston engines 2010–2019 |
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