发明名称 |
HIGH TURNING FAN EXIT STATOR |
摘要 |
<p>A turbine engine includes a fan section that rotates about a longitudinal axis and a compressor section. The turbine engine also includes a fan exit stator located between the fan section and the compressor section, the fan exit stator including an airfoil. The airfoil defines an entrance angle with respect to a leading edge of the airfoil and a line parallel to the longitudinal axis, and the airfoil defines an exit angle with respect to a trailing edge of the airfoil and a line parallel to the longitudinal axis. A difference between the entrance angle and the exit angle is between about 45° and about 65°. The turbine engine also includes a turbine section, and a portion of the compressor section is driven by a portion of the turbine section.</p> |
申请公布号 |
EP2809929(A1) |
申请公布日期 |
2014.12.10 |
申请号 |
EP20130778582 |
申请日期 |
2013.01.28 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BRILLIANT, LISA I.;ROSE, BECKY E.;DONG, YUAN;BALAMUCKI, STANLEY J. |
分类号 |
F02K3/072;F02C7/36 |
主分类号 |
F02K3/072 |
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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