Combustor liner with gasket for gas turbine engine
US10941937B2 · kind B2 · utility
2Cited by
32References
9Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 20, 2017 |
| Grant date | Mar 9, 2021 |
| Priority date | — |
| Expiry date | Feb 7, 2040 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gasket for installation within a cavity between a support shell and a liner panel of a combustor wall assembly, the support shell having a multiple of impingement holes, and the liner panel having a multiple of film holes, the gasket including a multiple of cells arranged with respect to the multiple of impingement holes and the multiple of film holes, wherein at least one of the multiple of cells segregate a respective subset of the multiple of impingement holes and a subset of the multiple of film holes.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.