FIELD: turbines.
SUBSTANCE: invention refers to gas turbine combustion chamber. Combustion chamber contains device of start-up burner, fuel injector (102) and unit (103) of the igniter. Device of start-up burner comprises starting housing (100) with starting surface (101), which faces the internal volume of the combustion chamber. Fuel injector (102) comprises outlet fuel for fuel injection into the inner volume. Unit (103) of the igniter has the possibility of ignition of fuel in internal volume, upon that unit (103) of the igniter is arranged at launching surface (101) so that fuel, which passes through the unit (103) of the igniter is flammable. Starting housing (100) contains cavity (501), fuel outlet is arranged inside the socket (501).
EFFECT: invention provides reliability of ignition.
16 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL INCLINED INJECTION INTO SWIRLER SLOT | 2012 |
|
RU2584385C2 |
| OIL AND WASTE OIL BURNER | 2020 |
|
RU2788014C1 |
| STEP SWIRLER FOR DYNAMIC CONTROL | 2009 |
|
RU2498161C2 |
| DOWNHOLE GAS GENERATOR AND ITS APPLICATION | 2011 |
|
RU2524226C2 |
| DAMPING DEVICE TO REDUCE PULSATION OF COMBUSTION CHAMBER | 2013 |
|
RU2568030C2 |
| COMBUSTOR BURNER ARRANGEMENT | 2015 |
|
RU2672216C2 |
| SWIRLER FOR MIXING FUEL WITH AIR IN COMBUSTION ENGINE | 2017 |
|
RU2716951C1 |
| GAS TURBINE PLANT COMBUSTION DEVICE | 2017 |
|
RU2660740C1 |
| DEVICE FOR EXTRACTION OF UNDERGROUND WATER AND SOIL RECLAMATION | 2010 |
|
RU2442859C1 |
| COMBUSTION ASSEMBLY FOR GAS TURBINE ENGINE | 2008 |
|
RU2478879C2 |
