发明名称 |
ANTI-ICING STATOR ASSEMBLY FOR A GAS TURBINE |
摘要 |
A gas turbine engine is defined wherein the inlet guide vanes leading into a core engine flow path are sized and positioned such that flow paths positioned circumferentially intermediate the vane are sufficiently large that a hydraulic diameter of greater than or equal to about 1.5 is achieved. This will likely reduce the detrimental effect of icing. |
申请公布号 |
EP2809913(A4) |
申请公布日期 |
2015.10.28 |
申请号 |
EP20130775336 |
申请日期 |
2013.01.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
FEULNER, MATTHEW R.;LIAO, SHENGFANG |
分类号 |
F02C7/04;F01D9/04;F02C7/047;F28D15/02 |
主分类号 |
F02C7/04 |
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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