Invention Application
US20160208629A1 ANTI-ROTATION VANE 审中-公开
防旋转风扇

ANTI-ROTATION VANE
Abstract:
A vane for a gas turbine engine includes a radially inner platform and a radially outer platform. At least two airfoils extend between the radially inner platform and the radially outer platform. At least two anti-rotation tabs extend axially from the radially outer platform.
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