| 发明名称 |
NON-AXISYMMETRIC FAN FLOW PATH |
| 摘要 |
A gas turbine engine propulsion system and method of assembling such is disclosed. The gas turbine engine propulsion system comprises a gas turbine engine that includes a fan flow path. The fan flow path may extend from the fan inlet to the rear exhaust outlet of the bypass flow path. A portion of the fan flow path, proximal to the fan, is non-axisymmetric. The non-axisymmetric portion may be upstream or downstream of the fan. |
| 申请公布号 |
EP3033497(A1) |
申请公布日期 |
2016.06.22 |
| 申请号 |
EP20140836522 |
申请日期 |
2014.04.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
FLOREA, RAZVAN, VIRGIL;TILLMAN, THOMAS, G.;COUSINS, WILLIAM, T. |
| 分类号 |
F01D17/00;B64C11/14;F01D5/14;F01D5/20;F01D25/24;F02C3/04;F02C7/04;F02C7/045;F02K3/06;F04D27/02;F04D29/32;F04D29/38;F04D29/40;F04D29/52;F04D29/54 |
主分类号 |
F01D17/00 |
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