FIELD: power industry.
SUBSTANCE: invention relates to power engineering. A gas turbine combustion chamber that has a burner insert that has a wall with cold and hot sides and an edge restricting the burner insert wall. The edge has an extreme rib at least partially enveloping and projecting above the cold side; besides, the extreme rib has holes along the whole edge. In the burner insert wall there is a hole for insertion of the burner into it. Besides, a gas turbine is presented, which contains the combustion chamber according to the invention.
EFFECT: invention allows creating an effective combustion chamber.
6 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE | 2017 |
|
RU2684157C2 |
| COMBUSTION CHAMBER OF GAS TURBINE AND GAS TURBINE | 2019 |
|
RU2727946C1 |
| BURNER OF GAS TURBINE, AND GAS TURBINE | 2007 |
|
RU2439433C2 |
| BURNER AND GAS TURBINE WITH SUCH BURNER | 2010 |
|
RU2541482C2 |
| COMBUSTION CHAMBER OF A GAS TURBINE | 2020 |
|
RU2757313C1 |
| GAS TURBINE COMBUSTION CHAMBER | 0 |
|
SU1835031A3 |
| AXIAL GAS TURBINE | 2010 |
|
RU2547351C2 |
| MODULAR VANE OR BLADE FOR GAS TURBINE AND GAS TURBINE WITH SUCH VANE OR BLADE | 2013 |
|
RU2563046C2 |
| GAS TURBINE COMBUSTION CHAMBER | 2017 |
|
RU2674819C1 |
| GAS TURBINE COMBUSTION CHAMBER | 1995 |
|
RU2133916C1 |
