词条 | GEN 125 | |||||||||||||||
释义 |
The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.[1] Design and developmentThe engine is a twin cylinder two-stroke, horizontally-opposed, air-cooled, {{convert|124|cc|cuin|1|abbr=on}}, direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces {{convert|8|hp|kW|0|abbr=on}} at 8500 rpm. The engine weighs {{convert|3|kg|lb|1|abbr=on}}.[1] The engine was designed specifically for the GEN H-4 helicopter, in which four of the engines are mounted to provide redundancy.[1] Variants
Base model producing {{convert|8|hp|kW|0|abbr=on}}[1]
Model producing {{convert|10|hp|kW|0|abbr=on}}[1] Applications
Specifications (GEN 125){{pistonspecs||ref=World Directory of Leisure Aviation 2011-12[1] |type=Twin cylinder, two stroke aircraft engine |bore= |stroke= |displacement={{convert|124|cc|cuin|1|abbr=on}} |length= |diameter= |width= |height= |weight={{convert|3|kg|lb|1|abbr=on}} |valvetrain= |supercharger= |turbocharger= |fuelsystem= |fueltype=gasoline |oilsystem= |coolingsystem=liquid or air |power={{convert|8|hp|kW|0|abbr=on}} at 8500 rpm |specpower= |compression= |fuelcon= |specfuelcon= |oilcon= |power/weight= |designer= |reduction_gear= |general_other= |components_other= |performance_other= }} See also{{aircontent|see also= |related= |similar aircraft= |lists= *List of aircraft engines }} References1. ^1 2 3 4 5 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 191 and 238-239. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X External links
3 : Two-stroke aircraft piston engines|Air-cooled aircraft piston engines|Aircraft piston engines 2010–2019 |
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