Turbine shroud assembly with pinned attachment supplements for ceramic matrix composite component mounting
US11326474B2 · kind B2 · utility
1Cited by
8References
6Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Dec 4, 2019 |
| Grant date | May 10, 2022 |
| Priority date | — |
| Expiry date | Feb 23, 2040 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes a turbine shroud assembly with a carrier and a plurality of turbine shroud segments. Each turbine shroud segment includes a blade track segment and a mount assembly. The carrier is arranged to extend circumferentially at least partway around an axis. The blade track segment includes a shroud wall and a mount post that extends radially away from the shroud wall. The mount assembly is configured to couple the blade track segment with the carrier.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.