Turbine shroud segment with buffer air seal system
US10094234B2 · kind B2 · utility
12Cited by
22References
20Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Jan 22, 2016 |
| Grant date | Oct 9, 2018 |
| Priority date | — |
| Expiry date | Nov 12, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbine shroud adapted for use in a gas turbine engine includes a plurality of metallic carrier segments and a plurality of blade track segments mounted to corresponding metallic carrier segments. Cooling air is directed onto the blade track segments to cool the blade track segments when exposed to high temperatures in a gas turbine engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.