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Zanzottera MZ 301 : ウィキペディア英語版 | Zanzottera MZ 301
The Zanzottera MZ 301 is a three cylinder, in-line two-stroke, dual ignition aircraft engine designed for ultralight aircraft.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-10 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 The engine was originally designed and produced by Zanzottera Technologies of Italy, but the design was sold, along with the rest of the company's two-stroke ultralight aircraft engine line, to Compact Radial Engines of Surrey, British Columbia, Canada.〔 ==Development== The MZ 301 was developed first as a fuel injected lightweight competitor to the more expensive liquid-cooled four stroke Rotax 912. Later a carbureted version of the MZ 301 was developed with three Bing 54 carburetors and producing .〔〔 The MZ 301 has cylinder barrels that are Nikasil-coated. The bore and stroke are the same as the single cylinder MZ 34 engine and twin-cylinder MZ 201 and MZ 202 powerplants . The MZ 301 features electric starting and the RZ2 gearbox with optional reduction ratios of 2.18, 2.55, 2.88, 3.11 or 3.66 to 1.〔〔
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「Zanzottera MZ 301」の詳細全文を読む
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