- Patent Title: Composite turbine vane with three-dimensional fiber reinforcements
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Application No.: US15462230Application Date: 2017-03-17
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Publication No.: US10767502B2Publication Date: 2020-09-08
- Inventor: Tara G. Schetzel , Ted J. Freeman , Jun Shi , Jeffrey A. Walston , Steven Clarke , Sean Kroszner
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis US IN Indianapolis US CA Cypress
- Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.,Rolls-Royce High Temperature Composites Inc.
- Current Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.,Rolls-Royce High Temperature Composites Inc.
- Current Assignee Address: US IN Indianapolis US IN Indianapolis US CA Cypress
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D5/28 ; F01D25/00 ; F01D5/18
Abstract:
A turbine vane made from ceramic matrix composite material and adapted for use in a gas turbine engine. The turbine vane is made from ceramic matrix composite materials with three-dimensionally woven or braided reinforcing tows and includes an inner band, an outer band, and an airfoil that extends between the inner band and the outer band.
Public/Granted literature
- US20180179906A1 COMPOSITE TURBINE VANE WITH THREE-DIMENSIONAL FIBER REINFORCEMENTS Public/Granted day:2018-06-28
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