Invention Grant
US09045990B2 Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
有权
用于燃气涡轮发动机的集成陶瓷基体复合转子盘几何形状
- Patent Title: Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的集成陶瓷基体复合转子盘几何形状
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Application No.: US13116102Application Date: 2011-05-26
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Publication No.: US09045990B2Publication Date: 2015-06-02
- 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: F01D11/00
- IPC: F01D11/00 ; F01D5/28 ; F01D5/34 ; F01D5/06
Abstract:
A CMC disk for a gas turbine engine includes a CMC hub defined about an axis and a multiple of CMC airfoils integrated with the CMC hub.
Public/Granted literature
- US20120297790A1 INTEGRATED CERAMIC MATRIX COMPOSITE ROTOR DISK GEOMETRY FOR A GAS TURBINE ENGINE Public/Granted day:2012-11-29
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