Combustor liner with decreased liner cooling
US9217568B2 · kind B2 · utility
6Cited by
24References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 7, 2012 |
| Grant date | Dec 22, 2015 |
| Priority date | — |
| Expiry date | Oct 23, 2034 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/03045
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A shell for a combustor liner includes a cold side, a hot side, a row of cooling holes and a jet wall. The jet wall projects from the hot side for creating a wall shear jet of increased velocity cooling flow in a tangential direction away from the row of cooling holes and along an adjacent heat shield cold side wall.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.