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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0127710 (1998-07-30) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 16 인용 특허 : 7 |
A fan in an axial flow gas turbine engine includes a plurality of fan blades. Each fan blade includes an airfoil portion and a root portion with a platform disposed radially therebetween. The platform of each blade extends circumferentially from the blade and is dimensioned to define, with an adjace
[ What is claimed is:] [1.] An improved fan in an axial flow gas turbine engine disposed about an axis, the gas turbine engine including an axially directed flow path defining a passage for working medium gases, the fan including a plurality of fan blades with each of said plurality of fan blades ha
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