Invention Grant
- Patent Title: Turbine blade with three-dimensional CMC construction elements
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Application No.: US15340684Application Date: 2016-11-01
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Publication No.: US10577939B2Publication Date: 2020-03-03
- Inventor: Daniel K. Vetters , David J. Thomas
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis US IN Indianapolis
- Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D5/28
- IPC: F01D5/28 ; F01D5/14 ; F01D5/30 ; F04D29/38
Abstract:
An ceramic matrix composite blade for use in a gas turbine engine is disclosed. The ceramic matrix composite blade includes a root, an airfoil, and a platform located between the root and the airfoil.
Public/Granted literature
- US20180119549A1 TURBINE BLADE WITH THREE-DIMENSIONAL CMC CONSTRUCTION ELEMENTS Public/Granted day:2018-05-03
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