INSERT AND STANDOFF DESIGN FOR A GAS TURBINE ENGINE VANE

摘要

A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform, an airfoil that extends from the platform, and an insert positioned such that a first portion of the insert extends relative to a surface of the platform and a second portion extends inside the airfoil. A standoff supports the insert above the surface.

主权项

1. A component for a gas turbine engine, comprising:
a platform; an airfoil that extends from said platform; an insert positioned such that a first portion of said insert extends relative to a surface of said platform and a second portion extends inside said airfoil; and a standoff that supports said insert above said surface.