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
- Patent Title: Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine
- Patent Title (中): 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
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Application No.: US13116188Application Date: 2011-05-26
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Publication No.: US08834125B2Publication Date: 2014-09-16
- Inventor: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Applicant: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/28 ; F01D5/22 ; C04B37/00
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
- US20120301314A1 HYBRID ROTOR DISK ASSEMBLY WITH A CERAMIC MATRIX COMPOSITE AIRFOIL FOR A GAS TURBINE ENGINE Public/Granted day:2012-11-29
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