Invention Grant
- Patent Title: Turbine vane assembly with ceramic matrix composite airfoil and friction fit metallic attachment features
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Application No.: US15607744Application Date: 2017-05-30
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Publication No.: US10260362B2Publication Date: 2019-04-16
- Inventor: Bruce E. Varney
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D9/00
- IPC: F01D9/00 ; F01D5/00 ; F01D9/04 ; F01D5/28 ; F01D5/14 ; C04B37/02
Abstract:
A turbine vane for a gas turbine engine incorporating a ceramic matrix composite airfoil is disclosed in this paper. The turbine vane includes an attachment unit configured to mount the ceramic matrix composite airfoil to other metallic components of the turbine vane.
Public/Granted literature
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