发明申请
US20120233982A1 GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT 有权
燃气涡轮发动机压缩机装置

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT
摘要:
A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four to eight (4-8) stages.
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