FIELD: engines and pumps.
SUBSTANCE: annular combustion chamber of gas turbine engine includes inner and outer walls and chamber bottom that is located between walls in front part of the chamber. Chamber bottom is divided into many sectors. Each sector is attached to walls. Sectors have side edges; at that, side edges of two neighbouring sectors overlap each other. Each sector includes the ridge elongated along one of its side edges. Ridge protrudes relative to one surface of this sector and covers the side edge of the neighbouring sector.
EFFECT: reducing air leaks between sectors.
9 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE ENGINE RING COMBUSTION CHAMBER | 2007 |
|
RU2429418C2 |
| DIFFUSION CHAMBER OF GAS TURBINE ENGINE, COMBUSTION CHAMBER AND GAS TURBINE CONTAINING THEM | 2008 |
|
RU2461778C2 |
| TRANSITION CHANNEL BETWEEN TWO STAGES OF TURBINE AND GAS-TURBINE ENGINE | 2007 |
|
RU2455498C2 |
| GAS TURBINE ENGINE COMBUSTION CHAMBER | 2008 |
|
RU2498163C2 |
| GAS TURBINE ENGINE COMBUSTION CHAMBER AND GAS TURBINE ENGINE | 2007 |
|
RU2444680C2 |
| GAS TURBINE ENGINE MODULE | 2015 |
|
RU2700847C2 |
| SWIRLER, BURNER AND COMBUSTION SYSTEM FOR GAS TURBINE ENGINE | 2016 |
|
RU2690598C2 |
| GAS-TURBINE ENGINE WITH ANNULAR COMBUSTION CHAMBER | 2008 |
|
RU2471122C2 |
| CIRCULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 2008 |
|
RU2485405C2 |
| COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 2006 |
|
RU2382279C2 |
