Method for minimizing thermoacoustic oscillations in gas turbine combustion chambers
US6460341B1 · kind B1 · utility
17Cited by
8References
7Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Aug 25, 1999 |
| Grant date | Oct 8, 2002 |
| Priority date | — |
| Expiry date | Aug 25, 2019 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/00014
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
In a method for minimizing thermoacoustic oscillations in gas turbine combustion chambers, an inert gas (N2, CO2, H2O) is additionally mixed with the stream of fuel.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.