Invention Grant
US09011085B2 Ceramic matrix composite continuous “I”-shaped fiber geometry airfoil for a gas turbine engine
有权
用于燃气涡轮发动机的陶瓷基复合连续“I”形纤维几何翼型
- Patent Title: Ceramic matrix composite continuous “I”-shaped fiber geometry airfoil for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的陶瓷基复合连续“I”形纤维几何翼型
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Application No.: US13116156Application Date: 2011-05-26
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Publication No.: US09011085B2Publication Date: 2015-04-21
- Inventor: Gabriel L. Suciu , Ioannis Alvanos
- Applicant: Gabriel L. Suciu , Ioannis Alvanos
- 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: F01D9/04
- IPC: F01D9/04 ; F01D25/24 ; F01D5/28 ; F01D11/00
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
- US20120301313A1 CERAMIC MATRIX COMPOSITE CONTINUOUS "I"-SHAPED FIBER GEOMETRY AIRFOIL FOR A GAS TURBINE ENGINE Public/Granted day:2012-11-29
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