Invention Application
US20070098548A1 VANE ASSEMBLY WITH IMPROVED VANE ROOTS 有权
VANE组装改进的VANE ROOTS

VANE ASSEMBLY WITH IMPROVED VANE ROOTS
Abstract:
A vane for a vane assembly of a gas turbine engine includes a vane root connected to the airfoil portion opposite a tip thereof. The vane root includes a platform and a button portion interconnecting the platform and the airfoil position. The button portion has relatively blunt leading and trailing ends which respectively protrude beyond leading and trailing edges of the airfoil portion.
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