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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|