FIELD: machine building.
SUBSTANCE: device consists of facilities for gaseous fuel supply, of facilities for supply of oxidant, and of fuel combustion facilities utilising oxidant for partial combustion of first part of fuel with products of partial combustion including intermediate combustion products. Also, products of partial combustion are mixed with the rest part of fuel, partially not combusted, thus facilitating production of modified fuel. Partial combustion is controlled to ensure output of intermediate combustion products required for production of preliminary specified modified fuel.
EFFECT: increased stability of combustion process.
23 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| INLET DEVICE OF ANNULAR COMBUSTION CHAMBER | 2023 |
|
RU2802903C1 |
| GAS TURBINE ENGINE COMBUSTION CHAMBER ASSEMBLY WITH A STRUCTURAL ELEMENT THAT PROVIDES A CAPTURED VORTEX | 2018 |
|
RU2748110C1 |
| METHOD FOR BURNING FUEL IN A LOW-EMISSION COMBUSTION CHAMBER | 2020 |
|
RU2753202C1 |
| ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE AND METHOD OF WORKING PROCESS IMPLEMENTATION | 2016 |
|
RU2624682C1 |
| FUEL COMBUSTION METHOD AND DEVICE | 2001 |
|
RU2215941C2 |
| AIR-COOLED HEAD OF SWIRL ATOMISER | 2009 |
|
RU2472070C2 |
| COMBUSTION CHAMBER OF GAS TURBINE UNIT WITH COMBUSTION IN COUNTERCURRENT SWIRLING FLOW | 2023 |
|
RU2806421C1 |
| METHOD FOR BURNING FUEL IN A LOW-EMISSION COMBUSTION CHAMBER | 2020 |
|
RU2753203C1 |
| ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 2018 |
|
RU2696519C1 |
| FUEL COMBUSTION DEVICE | 2019 |
|
RU2708011C1 |
