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Siddeley Tiger : ウィキペディア英語版 | Siddeley Tiger
:''For the 1932 radial engine, see Armstrong Siddeley Tiger'' The Siddeley Tiger was an unsuccessful British aero engine developed shortly after the end of World War I by Siddeley-Deasy. Problems encountered during flight testing caused the project to be cancelled. ==Design and development== Developed using two modified cylinder banks from the Siddeley Puma, the Tiger was a liquid-cooled 60 degree V12 engine with the advanced feature of an electric starter motor protected by a friction clutch. A reduction gear arrangement was provided for the propeller drive with a ratio of 0.559:1. The company claimed a power output of 600 hp (447 kW) but this was regarded as optimistic.〔Gunston 1989, p.18.〕 Flight testing by a Royal Aircraft Establishment test pilot, Frank Courtenay, revealed problems and his opinion of the engine was low as the following quote shows:
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「Siddeley Tiger」の詳細全文を読む
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