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Rolls-Royce RB.183 Tay
・ Rolls-Royce RB.203 Trent
・ Rolls-Royce RB.44 Tay
・ Rolls-Royce RB.50 Trent
・ Rolls-Royce RB106
・ Rolls-Royce RB108
・ Rolls-Royce RB145
・ Rolls-Royce RB162
・ Rolls-Royce RB211
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・ Rolls-Royce RB3011
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・ Rolls-Royce Rugby Football Club


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Rolls-Royce RB.183 Tay : ウィキペディア英語版
Rolls-Royce RB.183 Tay


The Rolls-Royce RB.183 Tay is a turbofan engine, developed from the RB183 Mk555 (Spey) core and using a fan scaled directly from the Rolls-Royce RB.211-535E4 to produce versions with a bypass ratio of 3.1:1 or greater. The IP compressor and LP turbine were designed using technology from the RB211 programme.〔"Developing the Rolls-Royce Tay' M.J.Wilson ASME-880051〕 The engine was first run in August 1984.〔Gunston 1989, p.153.〕 The Tay 650 had a new HP turbine which incorporated new technology which had been proven with the RB211-535E4. This engine also had a new combustor for improved durability.〔"Developing the Rolls-Royce Tay' M.J.Wilson ASME-880051〕
The Tay family is used on a number of airliners and larger business jets, including the Gulfstream IV family, Fokker 70 and Fokker 100, with a later version being used to re-engine Boeing 727-100s.
==Variants==


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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