Turbine vane airfoil profile
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United States of America Patent
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Dec 27, 2022
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N/A
app pub date -
Feb 4, 2022
filing date -
Feb 4, 2022
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Abstract
A turbine vane for a gas turbine engine has an airfoil including leading and trailing edges joined by spaced-apart pressure and suction sides to provide an external airfoil surface. The surface is formed in substantial conformance with multiple cross-sectional profiles of the airfoil defined by a set of Cartesian coordinates set forth in Table 1, the 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.
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