Invention Grant
- Patent Title: Turbine engine assembly with ceramic matrix composite components and end face seals
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Application No.: US16409231Application Date: 2019-05-10
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Publication No.: US11078802B2Publication Date: 2021-08-03
- Inventor: Anthony G. Razzell , Michael J. Whittle , Steven Hillier
- 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: F01D11/00
- IPC: F01D11/00 ; F16J15/3284
Abstract:
A gas turbine engine assembly includes a first component, a second component, and a seal. The first component is spaced apart from the second component to form a gap between the first component and the second component. The seal is configured to block gases from flowing in the gap between the first component and the second component.
Information query
