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A wide chord fan engine is a term to describe a modern turbofan jet engine having a ducted fan with a specific blade geometry - In layman's terms, they would be described as having wider blades than other jet engines. The technology was pioneered by Rolls-Royce in the 1970s 〔http://civil.rolls-royce.com/wide-chord-jet-engine-fan-blades/〕 and development from a variety of manufacturers continues today. ==Overview== The main fan on a jet engine consists of a number of aerofoils mounted at the rotational center on the fan disk, and as the engine core rotates the fan blades accelerate an air mass and create the force to move forward which gives thrust (in accordance with Newton's Third Law). In theory the larger the fan diameter (the line from the tip of one fanblade to its opposite member) the greater the thrust. In practical applications, fan size is limited by the weight, the space available around the aircraft and by the increased drag (resistance) generated by the larger frontal area. In the race to achieve better fuel economy, more thrust and less weight & noise from jet engines, designers have refined the blade design and materials to extract more thrust for any given fan disk area. One significant improvement〔http://civil.rolls-royce.com/wide-chord-jet-engine-fan-blades Rolls Royce Plc, 2004〕 is to make blade chords wider and, more recently, alter the blade geometry to give it a scimitar-like shape. Further refinements include making the blades from a light material such as titanium and to manufacture them with a hollow cross-section. Modern jet engines such as the Rolls Royce Trent 900 and the Engine Alliance GP7000, which both power the Airbus A380, are examples of wide-chord fan engines. 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「Wide chord」の詳細全文を読む スポンサード リンク
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