Variable-throat gas-turbine combustion chamber
US6263663A · kind A · utility
Assignees
Inventors
Key dates
| Filing date | Jun 11, 1999 |
| Grant date | Jul 24, 2001 |
| Priority date | — |
| Expiry date | Jun 11, 2019 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/26
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The present invention relates to a gas-turbine combustion chamber comprising at least a zone (11) referred to as pilot combustion zone into which at least a first pilot fuel injection means (3) and an associated first oxidizer injection means (4) open; a main combustion zone (12) into which at least a second main fuel injection means (7) and an associated second oxidizer injection means (8) open, all of it being maintained under a pressure P1 inside an enclosure (14). According to the invention, said chamber further comprises a mechanical means (15-19) for controlling the second flow of oxidizer, which reacts to the pressure difference between the inside (P1) and the atmospheric pressure (Po) outside enclosure (14), said pressure difference being directly linked with the engine speed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.