Dilution air hole in a gas turbine combustion chamber with combustion chamber tiles
US7059133B2 · kind B2 · utility
34Cited by
7References
24Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Mar 28, 2003 |
| Grant date | Jun 13, 2006 |
| Priority date | — |
| Expiry date | May 23, 2023 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/03041
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine combustion chamber includes combustion chamber tiles 3 attached to a supporting structure 6 of the gas turbine combustion chamber, with each tile possessing at least one dilution air hole 4 which is flush with a dilution air hole of the supporting structure 6, wherein a diameter of the dilution air hole of the supporting structure 6 is considerably larger than a diameter 14 of the dilution air hole 4 of the combustion chamber tile 3.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.