发明名称 ADVANCED BOOSTER SYSTEM
摘要 A compression stage [8] having a plurality of stator vanes [40] and rotor blades [14] coaxial with a longitudinal centerline axis [15], each stator vane haying an exit swirl angle distribution such that the exit swirl angle has a maximum value at an intermediate radius location and each rotor blade having a blade leading edge adapted to receive the flow from the stator vanes with the exit swirl angle distribution profile.
申请公布号 CA2918131(A1) 申请公布日期 2008.05.30
申请号 CA20072918131 申请日期 2007.11.15
申请人 GENERAL ELECTRIC COMPANY 发明人 WOOD, PETER JOHN;FALK, ERIC ANDREW;DAILEY, LYLE D.
分类号 F01D5/14;F01D9/02 主分类号 F01D5/14
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