Invention Application
US20120301303A1 HYBRID CERAMIC MATRIX COMPOSITE VANE STRUCTURES FOR A GAS TURBINE ENGINE
有权
用于气体涡轮发动机的混合陶瓷基体复合材料结构
- Patent Title: HYBRID CERAMIC MATRIX COMPOSITE VANE STRUCTURES FOR A GAS TURBINE ENGINE
- Patent Title (中): 用于气体涡轮发动机的混合陶瓷基体复合材料结构
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Application No.: US13116144Application Date: 2011-05-26
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Publication No.: US20120301303A1Publication Date: 2012-11-29
- Inventor: Ioannis Alvanos , Gabriel L. Suciu
- Applicant: Ioannis Alvanos , Gabriel L. Suciu
- Main IPC: F01D5/22
- IPC: F01D5/22 ; B21K25/00
Abstract:
A vane structure for a gas turbine engine includes a multiple of CMC airfoil sections integrated between a CMC outer ring and a metal alloy inner ring.
Public/Granted literature
- US08770931B2 Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine Public/Granted day:2014-07-08
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