Invention Application
US20120301313A1 CERAMIC MATRIX COMPOSITE CONTINUOUS "I"-SHAPED FIBER GEOMETRY AIRFOIL FOR A GAS TURBINE ENGINE
有权
陶瓷基复合材料连续式“I”型用于气体涡轮发动机的光纤几何式
- Patent Title: CERAMIC MATRIX COMPOSITE CONTINUOUS "I"-SHAPED FIBER GEOMETRY AIRFOIL FOR A GAS TURBINE ENGINE
- Patent Title (中): 陶瓷基复合材料连续式“I”型用于气体涡轮发动机的光纤几何式
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Application No.: US13116156Application Date: 2011-05-26
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Publication No.: US20120301313A1Publication Date: 2012-11-29
- Inventor: Gabriel L. Suciu , Ioannis Alvanos
- Applicant: Gabriel L. Suciu , Ioannis Alvanos
- Main IPC: F01D5/14
- IPC: F01D5/14 ; B65H81/00
Abstract:
A Ceramic Matrix Composites (CMC) airfoil for a gas turbine engine includes at least one CMC ply which defines a suction side, an outer platform, a pressure side and an inner platform with a continuous “I”-shaped fiber geometry.
Public/Granted literature
- US09011085B2 Ceramic matrix composite continuous “I”-shaped fiber geometry airfoil for a gas turbine engine Public/Granted day:2015-04-21
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