FIELD: machine building.
SUBSTANCE: device for injection cooling of wall includes injection sleeve and wall exposed to hot gas during operation. Injection sleeve is at least partially located in the pressure chamber and is located at a distance from the wall to form a cooling flow path between the wall and the injection hose so that the compressed gas injected from the pressure chamber through the first hole in the cooling hose blows the wall during operation and flows as a transverse flow towards the outlet at the outlet end of the cooling flow path. Flow deflection device is located in the flow path of the cooling flow downstream the first hole for deviation of the cross flow from the second hole and passes from the point between the first hole and the second hole in the direction of the cross flow over the second hole. First branch extends from one side of the second hole in the direction of transverse flow, and the second branch passes from the other side of the second hole in the direction of cross flow. Hole of injection cooling is absent in the first section of convective cooling of the wall, which is the wall section between the inlet end and the outlet end of the flow deflection device outside the section enclosed by the deviation device.
EFFECT: higher efficiency of injection cooling.
15 cl, 14 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBINE VANE WITH COOLED FILLET | 2015 |
|
RU2675433C2 |
TURBINE DESIGN AND METHOD TO COOL BAND INSTALLED NEAR TURBINE BLADE EDGE | 2008 |
|
RU2462600C2 |
BURNER ARRANGEMENT AND METHOD FOR OPERATING BURNER ARRANGEMENT | 2014 |
|
RU2665199C2 |
GAS TURBINE ENGINE (VERSIONS) | 2014 |
|
RU2639921C2 |
CONSEQUENT BURNING WITH THE DILUTION GAS MIXER | 2013 |
|
RU2627759C2 |
COOLED WALL OF TURBINE COMPONENT AND COOLING METHOD OF THIS WALL | 2016 |
|
RU2706211C2 |
COOLED WALL | 2013 |
|
RU2634986C2 |
STATOR THERMAL SHIELD FOR GAS TURBINE, GAS TURBINE WITH SUCH STATOR THERMAL SHIELD AND STATOR THERMAL SHIELD COOLING METHOD | 2016 |
|
RU2706210C2 |
METHOD FOR OPERATION OF COMBUSTION DEVICE FOR GAS TURBINE AND COMBUSTION DEVICE FOR GAS TURBINE | 2014 |
|
RU2686652C2 |
GAS-TURBINE ENGINE PROFILE PART COOLING DEVICE | 1997 |
|
RU2179246C2 |
Authors
Dates
2019-08-06—Published
2015-06-10—Filed