Invention Grant
- Patent Title: Turbine section assembly with ceramic matrix composite vane
-
Application No.: US16391811Application Date: 2019-04-23
-
Publication No.: US10954802B2Publication Date: 2021-03-23
- 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: F01D25/28
- IPC: F01D25/28 ; F01D11/00 ; F01D9/04 ; F01D5/28
Abstract:
A turbine assembly adapted for use in a gas turbine engine with a turbine vane comprising ceramic matrix composite materials. The turbine vane is configured to redirect air moving through a primary gas path of the gas turbine engine. The turbine assembly includes a vane-stage support for holding the turbine vane in place relative to a turbine case.
Public/Granted literature
- US20200340363A1 TURBINE SECTION ASSEMBLY WITH CERAMIC MATRIX COMPOSITE VANE Public/Granted day:2020-10-29
Information query
