发明名称 |
Gas turbine engine airfoil profile |
摘要 |
An airfoil for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an airfoil body including a leading edge and a trailing edge joined by a pressure side and a suction side spaced apart from the pressure side to provide an external airfoil surface extending in a radial direction from at least one platform. The external airfoil surface is formed in substantial conformance with multiple cross-sectional profiles of the airfoil described by a set of Cartesian coordinates set forth in Table 1. The Cartesian coordinates are provided by an axial coordinate scaled by a local axial chord, a circumferential coordinate scaled by a local axial chord, and a span location. The local axial chord corresponds to a width of the airfoil between the leading edge and the trailing edge at the span location, and the Cartesian coordinates in Table 1 have a tolerance relative to the specified coordinates of up to ±0.050 inches (±1.27 mm). |
申请公布号 |
US8979499(B2) |
申请公布日期 |
2015.03.17 |
申请号 |
US201213588056 |
申请日期 |
2012.08.17 |
申请人 |
United Technologies Corporation |
发明人 |
Allen-Bradley Eunice |
分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
代理机构 |
Carlson, Gaskey & Olds |
代理人 |
Carlson, Gaskey & Olds |
主权项 |
1. An airfoil for a gas turbine engine, comprising:
an airfoil body including a leading edge and a trailing edge joined by a pressure side and a suction side spaced apart from said pressure side to provide an external airfoil surface extending in a radial direction from at least one platform; and wherein said external airfoil surface is formed in substantial conformance with multiple cross-sectional profiles of the airfoil described by a set of Cartesian coordinates set forth in Table 1, said Cartesian coordinates provided by an axial coordinate scaled by a local axial chord, a circumferential coordinate scaled by a local axial chord, and a span location, wherein said local axial chord corresponds to a width of the airfoil between said leading edge and said trailing edge at said span location and said Cartesian coordinates in Table 1 have a tolerance relative to the specified coordinates of up to ±0.050 inches (±1.27 mm). |
地址 |
Hartford CT US |