Dilution passage arrangement for gas turbine engine combustor
US10655856B2 · kind B2 · utility
0Cited by
31References
18Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 19, 2014 |
| Grant date | May 19, 2020 |
| Priority date | — |
| Expiry date | Nov 8, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a major dilution passage having a lip and a first seal boss. The liner panel also includes a minor dilution passage having a second seal boss adjacent the first seal boss.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.