Turbine shroud segments with strip seal assemblies having dampened ends
US12152499B1 · kind B1 · utility
1Cited by
159References
19Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 4, 2023 |
| Grant date | Nov 26, 2024 |
| Priority date | — |
| Expiry date | Dec 4, 2043 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/14
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbine shroud assembly for use with a gas turbine engine includes a first shroud segment, a second shroud segment, and a damping strip seal assembly. The first shroud segment has 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. The damping strip seal assembly includes an axial seal member, a forward seal, and an aft seal member.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.