Turbine shroud with tubular runner-locating inserts
US10012100B2 · kind B2 · utility
4Cited by
57References
20Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Jan 6, 2016 |
| Grant date | Jul 3, 2018 |
| Priority date | — |
| Expiry date | Jan 4, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbine shroud for a gas turbine engine includes a carrier and a blade track. The blade track includes an annular runner and a plurality of inserts that extend radially outward away from the annular runner. The inserts extend through the carrier to couple the annular runner with the carrier.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.