Invention Application
US20120301314A1 HYBRID ROTOR DISK ASSEMBLY WITH A CERAMIC MATRIX COMPOSITE AIRFOIL FOR A GAS TURBINE ENGINE
有权
用于气体涡轮发动机的陶瓷基体复合材料的混合转子盘组件
- Patent Title: HYBRID ROTOR DISK ASSEMBLY WITH A CERAMIC MATRIX COMPOSITE AIRFOIL FOR A GAS TURBINE ENGINE
- Patent Title (中): 用于气体涡轮发动机的陶瓷基体复合材料的混合转子盘组件
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Application No.: US13116188Application Date: 2011-05-26
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Publication No.: US20120301314A1Publication Date: 2012-11-29
- Inventor: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Applicant: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Main IPC: F01D5/14
- IPC: F01D5/14
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.
Public/Granted literature
- US08834125B2 Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine Public/Granted day:2014-09-16
Information query
