Invention Grant
US08905711B2 Ceramic matrix composite vane structures for a gas turbine engine turbine
有权
用于燃气涡轮发动机涡轮机的陶瓷基体复合叶片结构
- Patent Title: Ceramic matrix composite vane structures for a gas turbine engine turbine
- Patent Title (中): 用于燃气涡轮发动机涡轮机的陶瓷基体复合叶片结构
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Application No.: US13116053Application Date: 2011-05-26
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Publication No.: US08905711B2Publication Date: 2014-12-09
- Inventor: Gabriel L. Suciu , Ioannis Alvanos , Brian D. Merry , Christopher M. Dye
- Applicant: Gabriel L. Suciu , Ioannis Alvanos , Brian D. Merry , Christopher M. Dye
- 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: F04D29/54
- IPC: F04D29/54 ; F01D9/04 ; F01D5/28 ; F01D25/24 ; F01D5/14 ; F01D11/00
Abstract:
A vane structure for a gas turbine engine according includes a multiple of CMC airfoil sections integrated between a CMC outer ring and a CMC inner ring.
Public/Granted literature
- US20120301285A1 CERAMIC MATRIX COMPOSITE VANE STRUCTURES FOR A GAS TURBINE ENGINE TURBINE Public/Granted day:2012-11-29
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