Combustion chamber of a gas turbine
US5154059A · kind A · utility
Assignee
Inventor
Key dates
| Filing date | Mar 16, 1992 |
| Grant date | Oct 13, 1992 |
| Priority date | — |
| Expiry date | Mar 16, 2012 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23C2900/07002
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
In a combustion chamber (A) of the form of an annular combustion chamber, a row of large and small premixed burners (B, C) are arranged along the annular front wall (10). The large premixed burners (B), which are the main burners of the combustion chamber (A), and the small premixed burners (C), which are the pilot burners of the combustion chamber (A), follow each other alternately and regularly along the front wall (10) where they also emerge into the combustion space of the combustion chamber (A). A plurality of air nozzles (D), whose injection is directed into the combustion space of the combustion chamber (A), are placed between the large premixed burners (B) and the small premixed burners (C).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.