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Sunbeam Matabele : ウィキペディア英語版 | Sunbeam Matabele
The Sunbeam Matabele was a British 12-cylinder aero engine that was first flown in 1918. The Matabele was the last iteration of one of Sunbeam's most successful aero engines, the Cossack. ==Design and development== The Cossack was a twin overhead camshaft V12, with four valves per cylinder. The Matabele fitted this with two of the blocks from the Saracen, using aluminium instead of the Cossack's cast iron. The Saracen's bore was slightly larger at 122 mm (from the Cossack's 110 mm) and with the same stroke of 160 mm this gave a capacity of 22.4 litres (1,370 cu in). Ignition was by four magnetos (two per bank), with twin sparkplugs. A propeller reduction gear of 1.63:1 was fitted.〔(【引用サイトリンク】url=http://www.localhistory.scit.wlv.ac.uk/Museum/Transport/planes/SunbeamEngines9.htm )〕
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「Sunbeam Matabele」の詳細全文を読む
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