Invention Grant
US08834125B2 Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine 有权
具有用于燃气涡轮发动机的陶瓷基体复合翼型的混合转子盘组件

Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine
Abstract:
A Ceramic Matrix Composite (CMC) airfoil for a gas turbine engine includes a CMC root section which extends to form a CMC airfoil section, the CMC root section defines a bore along a non-linear axis.
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