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Hexadyne P60 : ウィキペディア英語版 | Hexadyne P60
The Hexadyne P60 is an American aircraft engine, designed and produced by Hexatron Engineering of Salt Lake City, Utah for use in ultralight and homebuilt aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 238-241. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The engine is a twin cylinder four-stroke, horizontally-opposed, , air-cooled, gasoline engine design, with a mechanical gearbox spur gear reduction drive with a reduction ratio of 2.5:1. It employs electronic ignition and produces continuous at 5750 rpm. The engine management system is a six-sensor computer and the engine is optimized to drive a propeller.〔〔(【引用サイトリンク】title=Hexatron Product 2 )〕 The engine was initially displayed at AirVenture, Oshkosh, Wisconsin in 2001.〔
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