Invention Grant
- Patent Title: Turbine vane assembly incorporating ceramic matrix composite materials and cooling
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Application No.: US16665638Application Date: 2019-10-28
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Publication No.: US11268392B2Publication Date: 2022-03-08
- Inventor: Roderick M. Townes , Andrew T. Holt , Michael J. Whittle
- 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: F01D9/04
- IPC: F01D9/04 ; F01D5/18 ; F01D5/28 ; B33Y10/00
Abstract:
A turbine vane assembly adapted for use with a gas turbine engine includes an airfoil and a spar. The airfoil is formed to define a cavity that extends into the airfoil. The spar is located in the cavity to define a cooling passage that extends around the spar between the spar and the airfoil. The turbine vane assembly includes cooling features to aid heat transfer of the turbine vane assembly during operation in the gas turbine engine.
Public/Granted literature
- US20210123352A1 TURBINE VANE ASSEMBLY INCORPORATING CERAMIC MATRIX COMPOSITE MATERIALS AND COOLING Public/Granted day:2021-04-29
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