Invention Grant
US08770931B2 Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine
有权
混合陶瓷基体用于燃气涡轮发动机的复合叶片结构
- Patent Title: Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine
- Patent Title (中): 混合陶瓷基体用于燃气涡轮发动机的复合叶片结构
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Application No.: US13116144Application Date: 2011-05-26
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Publication No.: US08770931B2Publication Date: 2014-07-08
- Inventor: Ioannis Alvanos , Gabriel L. Suciu
- Applicant: Ioannis Alvanos , Gabriel L. Suciu
- 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
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
- US20120301303A1 HYBRID CERAMIC MATRIX COMPOSITE VANE STRUCTURES FOR A GAS TURBINE ENGINE Public/Granted day:2012-11-29
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