Invention Application
US20120301317A1 HYBRID ROTOR DISK ASSEMBLY WITH CERAMIC MATRIX COMPOSITES PLATFORM FOR A GAS TURBINE ENGINE
有权
混合转子盘组件与陶瓷基体复合材料平台用于气体涡轮发动机
- Patent Title: HYBRID ROTOR DISK ASSEMBLY WITH CERAMIC MATRIX COMPOSITES PLATFORM FOR A GAS TURBINE ENGINE
- Patent Title (中): 混合转子盘组件与陶瓷基体复合材料平台用于气体涡轮发动机
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Application No.: US13116173Application Date: 2011-05-26
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Publication No.: US20120301317A1Publication 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) platform for an airfoil of a gas turbine engine includes a CMC platform segment which at least partially defines an airfoil profile.
Public/Granted literature
- US08936440B2 Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine Public/Granted day:2015-01-20
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