FIELD: power industry.
SUBSTANCE: swirler (31, 131, 231) includes central fuel distributing element (37), external wall (39) enveloping the central fuel distributing element (37) and restricting axial combustion air flow passage (41), swirling blades (47) passing in radial direction to external wall (39) and providing the flowing combustion air with a tangential component of the flow, as well as enveloping central fuel distributing element (37), and partition wall (42, 142) located radially inside external wall (39) and dividing flow passage (41) into radially internal section (43) and radially external section (45); radially internal section (43) of the passage provides for combustion air flow without any provision of the tangential component of the flow. Fuel lines (49) pass through radially internal section (43) of the passage to swirling blades (47) in radially external section (45) of the passage.
EFFECT: invention allows preventing backfire in a burner.
13 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
SWIRLER, BURNER AND COMBUSTION SYSTEM FOR GAS TURBINE ENGINE | 2016 |
|
RU2690598C2 |
BURNER | 2010 |
|
RU2562900C2 |
STEP SWIRLER FOR DYNAMIC CONTROL | 2009 |
|
RU2498161C2 |
BURNER | 2009 |
|
RU2459146C2 |
BURNER WITH GAS AND AIR PRE-MIXING FOR GAS TURBINES AND CONVECTORS (EMBODIMENTS) | 2018 |
|
RU2716775C2 |
VORTEX BURNER FOR GAS TURBINE | 2016 |
|
RU2635958C1 |
LOW-EMISSIVE VORTEX BURNER | 2018 |
|
RU2693117C1 |
SWIRLER FOR MIXING FUEL WITH AIR IN COMBUSTION ENGINE | 2017 |
|
RU2716951C1 |
SWIRLER, COMBUSTION CHAMBER UNIT AND GAS TURBINE WITH IMPROVED FUEL/AIR MIXING | 2017 |
|
RU2715129C1 |
METHOD FOR CONTROLLING OPERATION OF LOW-TOXIC COMBUSTION CHAMBER MODULE OF GAS TURBINE ENGINE | 2017 |
|
RU2637164C1 |
Authors
Dates
2014-12-20—Published
2010-03-22—Filed