Ceramic matrix composite component assembly and seal
US10718226B2 · kind B2 · utility
18Cited by
65References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 21, 2017 |
| Grant date | Jul 21, 2020 |
| Priority date | — |
| Expiry date | Apr 8, 2038 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine assembly adapted to separate a high pressure zone from a low pressure zone includes a seal configured to block gasses from passing through the interface of two adjacent components. The seal assembly includes a strip seal.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.