Diffuser combustor
US6508061B2 · kind B2 · utility
21Cited by
6References
14Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Apr 25, 2001 |
| Grant date | Jan 21, 2003 |
| Priority date | — |
| Expiry date | Apr 25, 2021 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/34
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A combustion system for a power generating gas turbine engine which includes at least a combustion chamber with a annular fuel manifold at one end of the combustion chamber and a passageway having a narrow throat downstream of the fuel manifold whereby air passes around the fuel manifold and mixes with fuel and is diffused through the passageway into the burn zone defined in the combustion chamber in an ultimate location.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.