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Austro Engine GIAE110R : ウィキペディア英語版 | Austro Engine GIAE110R
The Austro Engine GIAE110R is an Austrian aircraft engine, designed and produced by Austro Engine of Wiener Neustadt for use in light aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 238-239. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 As of 2015 the engine is not listed as available on the company website and may not have been developed past prototype stage. ==Design and development== The engine is a twin rotor four-stroke, air and liquid-cooled, , gasoline Wankel engine design, with a mechanical gearbox reduction drive, employing a helical gear set, with reduction ratio of 2.96:1. It employs dual capacitor discharge ignition and produces at 7500 rpm.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Austro Engine GIAE110R」の詳細全文を読む
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