FIELD: gas turbine engines.
SUBSTANCE: invention relates to a method and a control system for a combustion system of a gas turbine engine (10). The gas turbine engine (10) has a combustion chamber (28) with a primary combustion zone (110) wherefor the condition in the primary combustion zone (110) is determined by the primary zone control parameter. The method includes adjusting the primary zone control parameter (PZCP) to a substantially constant value in the range of values of the air temperature (T1) at the inlet of the compressor. Also disclosed are a gas turbine engine and a method for producing a control system for a combustion system of a gas turbine engine.
EFFECT: creation of a method and a control system for a combustion system of a gas turbine engine.
14 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR CONTROLLING GAS TURBINE ENGINE | 2018 |
|
RU2755957C1 |
| GAS TURBINE ENGINE CONTROL SYSTEM | 2014 |
|
RU2641786C2 |
| CONTROLLER FOR GAS TURBINE, GAS TURBINE, CONTROL METHOD OF GAS TURBINE AND MACHINE-READABLE DATA MEDIUM | 2018 |
|
RU2737489C1 |
| CONTROL METHOD OF GAS TURBINE ENGINE | 2019 |
|
RU2730568C1 |
| GAS TURBINE ENGINE COMBUSTION CHAMBER AND GAS TURBINE ENGINE | 2007 |
|
RU2444680C2 |
| SYSTEM OF GAS TURBINE ENGINE CONTROL | 2012 |
|
RU2501964C1 |
| GAS TURBINE ENGINE AND METHOD OF ITS OPERATION | 2011 |
|
RU2554367C2 |
| COMBUSTION CHAMBER FOR GAS TURBINE INSTALLATION | 2017 |
|
RU2672985C2 |
| GAS-TURBINE ENGINE CONTROL METHOD | 2006 |
|
RU2319025C1 |
| CONTROL METHOD OF GAS TURBINE ENGINE WITH AFTERBURNER COMBUSTION CHAMBER | 2018 |
|
RU2706518C1 |
