发明名称 |
TURBINE ENGINE VARIABLE AREA VANE |
摘要 |
A turbine engine stator vane is provided that rotates about an axis, and includes an airfoil, a flange and a shaft. The airfoil extends axially between a first airfoil end and a second airfoil end. The airfoil includes a concave side surface, a convex side surface and a cavity. The concave and the convex side surfaces extend between an airfoil leading edge and an airfoil trailing edge. The cavity extends axially into the airfoil from a cavity inlet in an end surface at the second airfoil end. The flange is connected to the second airfoil end. The flange extends circumferentially around at least a portion of the cavity inlet, and radially away from the concave and the convex side surfaces to a distal flange edge. The shaft extends along the axis, and is connected to the second airfoil end. |
申请公布号 |
WO2014011304(A3) |
申请公布日期 |
2014.04.10 |
申请号 |
WO2013US37618 |
申请日期 |
2013.04.22 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SPANGLER, BRANDON W.;PROPHETER-HINCKLEY, TRACY A. |
分类号 |
F02C9/20;F01D17/16;F02K3/00 |
主分类号 |
F02C9/20 |
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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