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 |
WO2015023325(A1) |
申请公布日期 |
2015.02.19 |
申请号 |
WO2014US34494 |
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;F01D5/14;F01D25/24;F04D29/38;F04D29/40 |
主分类号 |
F01D17/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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