Combustor liner with reduced cooling dilution openings
US9335049B2 · kind B2 · utility
4Cited by
24References
15Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 7, 2012 |
| Grant date | May 10, 2016 |
| Priority date | — |
| Expiry date | Mar 12, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/03045
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A combustor liner is arcuate in shape and defines an axis and a circumferential direction. The combustor liner includes a first row of dilution openings and a second row of dilution openings. The first row runs in the circumferential direction. The second row runs parallel to the first row and is axially spaced from the first row. Each dilution opening of the second row overlaps in an axial direction a portion of each of two adjacent dilution openings of the first row.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.