Main combustion system and combustion process
Abstract
Abstract IMPROVED CONSTRUCTION FOR THE COMBUSTION OF FUELS IN A COMBUSTION SYSTEM, AS FOR EXAMPLE A GAS TURBINE, IS DESCRIBED WHEREIN MEANS ARE PROVIDED FOR ACCURATELY METERING THE INCOMING PRIMARY AIR FLOW IN RELATION TO CHANGES IN METERED FUEL IMPUTS WHEREBY A REALTIVELY CONSTANT EQUIVALENCE RATIO FOR THE FUEL-PRIMARY AIR MIXTURE MAY BE MAINTAINED, AND WHEREIN SECONDARY AIR IS ISOLATED IN RIBBON-LIKE RADIALLY-DIRECTED FLOWS PARALLEL TO AND INTERLEAVED WITH THE PRIMARY AIR-FUEL MIXTURE FOR CONTROLLED COOLING OF THE TURBINE NOZZLE PARTITIONS AND/OR OF THE COMBUSTION PRODUCTS. THE METERING MEANS FOR THE PRIMARY AIR FLOW AUTOMATICALLY CONTROL THE AMOUNT OF AIR IN THE PRIMARY AIR STREAMS IN INVERSE RELATION TO THE AMOUNT OF AIR IN THE SECONDARY AIR STREAMS.
Inventors
- 👤 Paul H Kydd
Bibliographic Details
Claims Analysis
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| 7.5 Years (Year 8) | 1978-11-08 | 1979-05-10 | 1979-11-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1982-11-08 | 1983-05-10 | 1983-11-09 | $7700.00 | Window Closed / Lapsed |