Turbine shroud assembly with inter-segment damping
US12215593B1 · kind B1 · utility
0Cited by
160References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 30, 2024 |
| Grant date | Feb 4, 2025 |
| Priority date | — |
| Expiry date | May 30, 2044 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/55
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbine shroud assembly includes a first shroud segment, a second shroud segment, and a seal assembly. The first shroud segment includes a first carrier segment arranged circumferentially at least partway around a central axis and a first blade track segment supported by the first carrier segment. The second shroud segment is arranged circumferentially adjacent the first shroud segment about the central axis. The seal assembly is configured to block gases from escaping the gas path radially between the first shroud segment and the second shroud segment.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.