FIELD: fuel combustion devices.
SUBSTANCE: object of the present invention is to create a fuel injector for a combustion chamber of a gas turbine characterized by a long service life and high strength reliability. Solution of the problem is a fuel injector for a combustion chamber of a gas turbine, which is a fuel injector injecting fuel into the combustion chamber of a combustion chamber of a gas turbine, in which the fuel injector is metallurgically connected to a base that supports the fuel injector, surface between the fuel injector and the base includes surface on which the connection is made as a result of a fusion connection or a solder connection, and an inner portion on which the joint is made as a result of pressure welding. Variants of the combustion chamber of a gas turbine including a fuel injector, and a method of manufacturing a fuel injector are proposed.
EFFECT: long service life and high strength reliability.
15 cl, 19 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE COMBUSTION CHAMBER | 2017 |
|
RU2674819C1 |
| COMBUSTION CHAMBER OF A GAS TURBINE | 2021 |
|
RU2766495C1 |
| COMBUSTION CHAMBER OF GAS TURBINE AND GAS TURBINE | 2019 |
|
RU2727946C1 |
| COMBUSTION CHAMBER OF A GAS TURBINE AND METHOD FOR MANUFACTURING A BURNER PART | 2021 |
|
RU2763436C1 |
| COMBUSTION CHAMBER OF A GAS TURBINE AND METHOD FOR MANUFACTURING A FUEL NOZZLE | 2021 |
|
RU2766382C1 |
| GAS TURBINE COMBUSTION CHAMBER | 2017 |
|
RU2676496C1 |
| COMBUSTION CHAMBER AND GAS TURBINE ENGINE COMPRISING SUCH COMBUSTION CHAMBER | 2019 |
|
RU2738248C1 |
| GAS TURBINE COMBUSTION CHAMBER AND METHOD FOR OPERATION THEREOF | 2017 |
|
RU2674836C1 |
| GAS TURBINE COMBUSTOR | 2017 |
|
RU2669883C9 |
| COMBUSTION CHAMBER OF A GAS TURBINE | 2020 |
|
RU2757313C1 |
