发明名称 GEARED TURBOMACHINE FAN AND COMPRESSOR ROTATION
摘要 A high-bypass ratio geared turbomachine comprises a compressor section of a high-bypass ratio geared turbomachine. The compressor section provides at least a low-pressure compressor and a high-pressure compressor, wherein a rotor of the low-pressure compressor rotates together with a rotor of a fan.
申请公布号 EP2807358(A4) 申请公布日期 2015.10.21
申请号 EP20130774928 申请日期 2013.01.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SHERIDAN, WILLIAM G.;MCCUNE, MICHAEL E.
分类号 F02C7/36;F02K3/06 主分类号 F02C7/36
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