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    • 1. 发明授权
    • Counterrotatable booster compressor assembly for a gas turbine engine
    • 用于燃气涡轮发动机的可逆增压压缩机组件
    • US06666017B2
    • 2003-12-23
    • US10154584
    • 2002-05-24
    • Ian Francis PrenticeDavid William CrallBruce Clark BusbeyChristopher Charles GlynnDonald Ray Bond
    • Ian Francis PrenticeDavid William CrallBruce Clark BusbeyChristopher Charles GlynnDonald Ray Bond
    • F02K3072
    • F01D5/022F02C3/067F02K3/072F04D19/024F04D25/04
    • A counterrotatable booster compressor assembly for a gas turbine engine having a counterrotatable fan section with a first fan blade row connected to a first drive shaft and a second fan blade row axially spaced from the first fan blade row and connected to a second drive shaft. The counterrotatable booster compressor assembly includes a first compressor blade row connected to the first drive shaft, a plurality of fan shaft extensions connected to the second drive shaft for driving the second fan blade row, and at least one compressor blade integral with each fan shaft extension so as to form a second compressor blade row interdigitated with the first compressor blade row. The counterrotatable booster compressor further includes a first platform member integral with each fan shaft extension at a first location so as to form a portion of an inner flowpath for the counterrotatable booster compressor and a second platform member integral with each fan shaft extension at a second location so as to form a portion of an outer flowpath for the counterrotatable booster compressor, where each compressor blade of the second compressor blade row is positioned between the first and second platform members.
    • 一种用于燃气涡轮发动机的可逆转增压压缩机组件,其具有可逆转风扇部分,其具有连接到第一驱动轴的第一风扇叶片排和与第一风扇叶片排轴向间隔开并连接到第二驱动轴的第二风扇叶片排。 可逆转增压压缩机组件包括连接到第一驱动轴的第一压缩机叶片排,与驱动第二风扇叶片排的第二驱动轴连接的多个风扇轴延伸部,以及与每个风扇轴延伸部一体的至少一个压缩机叶片 以形成与第一压缩机叶片排交叉的第二压缩机叶片排。 可逆转增压压缩机还包括在第一位置处与每个风扇轴延伸部一体形成的第一平台构件,以便形成用于可逆转增压压缩机的内部流路的一部分,以及在第二位置处与每个风扇轴延伸部一体形成的第二平台构件 以便形成用于可逆转增压压缩机的外部流路的一部分,其中第二压缩机叶片排的每个压缩机叶片位于第一和第二平台构件之间。