Combustion chamber of a gas turbine with pre-mixing and pre-evaporation elements
US4408461A · kind A · utility
113Cited by
3References
15Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 20, 1980 |
| Grant date | Oct 11, 1983 |
| Priority date | — |
| Expiry date | Oct 20, 2000 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23D2209/10
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A combustion chamber for a gas turbine which is equipped with a number of tubular-shaped elements, within which there occurs between the fuel and the compressed air a pre-mixing/pre-evaporation process. Each tubular element is closed at its end at the side of its combustion space by a flame baffle provided with one or a number of openings, so that the combustion first can occur downstream of the flame baffle, whereby there is appreciably reduced the emissivity of noxious substances from the combustion process.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.