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US 2011/0236200 A1Published application
Gas turbine engine with non-axisymmetric surface contoured vane platform
AssigneeUnited Technologies Corporation
InventorsEric A. Grover, Thomas J. Praisner
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Abstract
A vane segment for a gas turbine engine according to an exemplary aspect of the present disclosure includes an inner vane platform relative an axis, the inner vane platform having a non-axisymmetric surface contour.
Claims13
A vane segment for a for a gas turbine engine comprising:
- an outer vane platform relative an axis;
- an inner vane platform relative said axis, said inner vane platform having a non-axisymmetric surface contour;
- and
- a vane which extends between said outer vane platform and said inner vane platform.
1 more element
Dependencies are inferred from the claim text.