发明名称 |
AIRFOIL CONTOUR FOR LOW-LOSS ON-BOARDING OF COOLING AIR THROUGH AN ARTICULATING SPINDLE |
摘要 |
A turbine stator vane assembly for a gas turbine engine is disclosed and includes an airfoil rotatable about an axis transverse to an engine longitudinal axis. The airfoil includes outer walls defining an inner chamber between a pressure side and a suction side of the airfoil. At least one spindle supports rotation of the airfoil and includes a feed opening for communicating cooling air into the inner chamber. An inlet defines a passage between the feed opening and the inner chamber and includes a protrusion of the outer wall on at least one of the pressure side and suction side of the airfoil. |
申请公布号 |
EP3068977(A1) |
申请公布日期 |
2016.09.21 |
申请号 |
EP20140862100 |
申请日期 |
2014.11.03 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SLAVENS, THOMAS N.;GROVER, ERIC A.;TEIXEIRA, JOHN D. |
分类号 |
F01D9/02;F01D5/02;F01D5/12;F01D5/14;F01D9/04;F01D9/06;F01D17/14;F01D17/16;F01D25/12;F02C3/04;F02C7/18 |
主分类号 |
F01D9/02 |
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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