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US09279335B2 Vane assembly for a gas turbine engine 有权
燃气轮机的叶片组件

Vane assembly for a gas turbine engine
Abstract:
A vane assembly for a gas turbine engine includes a first platform, a second platform, and an airfoil that extends radially across an annulus between the first platform and the second platform. The airfoil is centered relative to a centerline axis of the second platform and is offset relative to a centerline axis of the first platform.
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