Premix Burner for operating a combustion chamber with a liquid and/or gaseous fuel
US6098406A · kind A · utility
15Cited by
7References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 17, 1997 |
| Grant date | Aug 8, 2000 |
| Priority date | — |
| Expiry date | Dec 17, 2017 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23D2209/10
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
A premix burner for a gas turbine engine having a pair of partial conical bodies stacked inside each other to form a conical interior chamber is disclosed. The conical bodies are offset laterally to form tangential air flow openings. The width of the openings is varied in a prescribed manner to induce rotational disorder.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.