Invention Grant
- Patent Title: Turbine section assembly with ceramic matrix composite vane
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Application No.: US16391936Application Date: 2019-04-23
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Publication No.: US10975708B2Publication Date: 2021-04-13
- Inventor: Michael J. Whittle , Anthony G. Razzell , Roderick M. Townes , David J. Shepherd , Duncan Forbes
- Applicant: Rolls-Royce plc
- Applicant Address: GB London
- Assignee: Rolls-Royce plc
- Current Assignee: Rolls-Royce plc
- Current Assignee Address: GB London
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D5/14 ; F01D5/28 ; F01D9/04 ; F01D11/00 ; F01D25/00 ; F01D25/24 ; F01D25/28
Abstract:
A turbine assembly adapted for use in a gas turbine engine is disclosed in this paper. The turbine assembly includes a turbine vane comprising ceramic matrix composite materials configured for use in high temperature environments. The turbine assembly further includes a vane-stage support for holding the turbine vane and other components in place relative to a turbine case.
Public/Granted literature
- US20200340365A1 TURBINE SECTION ASSEMBLY WITH CERAMIC MATRIX COMPOSITE VANE Public/Granted day:2020-10-29
Information query
