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翻訳と辞書　辞書検索 [ 開発暫定版 ] スポンサード リンク Rolls-Royce Olympus ： ウィキペディア英語版 Rolls-Royce Olympus The Rolls-Royce Olympus (originally the Bristol B.E.10 Olympus) was the world's first two-spool axial-flow turbojet aircraft engine design dating from November 1946,〔Baxter 2012, p. 16〕〔http://www.flightglobal.com/pdfarchive/view/1955/1955%20-%201748.html〕 although not the first to run or enter service. It was originally developed and produced by Bristol Aero Engines. First running in 1950,〔Baxter 2012, p. 20〕 its initial use was as the powerplant of the Avro Vulcan V bomber. The design was further developed for supersonic performance as part of the BAC TSR-2 programme. Later it saw production as the Rolls-Royce/Snecma Olympus 593, the powerplant for Concorde SST. Versions of the engine were licensed to Curtiss-Wright in the US as the TJ-32 or J67 (military designation) and the TJ-38 'Zephyr'. The Olympus was also developed with success as marine and industrial gas turbines. Bristol Aero Engines (formerly Bristol Engine Company) merged with Armstrong Siddeley Motors in 1959 to form Bristol Siddeley Engines Limited (BSEL), which in turn was taken over by Rolls-Royce in 1966. As of 2012, the Olympus remains in service as both a marine and industrial gas turbine. It also powers the restored Avro Vulcan XH558. ==Background== 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「Rolls-Royce Olympus」の詳細全文を読む スポンサード リンク 翻訳と辞書 : 翻訳のためのインターネットリソース Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.