FIELD: turbine engineering. SUBSTANCE: blade has hollow feather with entrance and exit edges and longitudinal partition, installed in a spaced relation to feather periphery and abutting against blade root portion so that it divides blade interior into front and rear sections; made in front section on pan and wall sides are parallel fins inclined to blade axis in opposite directions contacting each other on tops at intersecting points to form channels; front section communicates with coolant source; exit edge has slots for discharging coolant; partition is intermittent structure made in the form of separated straps which cover part of interfin channels their other part being held open for passing coolant from front to rear section. EFFECT: improved cooling conditions for blade making it useful for operation at high temperatures. 4 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STEAM TURBINE STAGE WITH MOISTURE SEPARATORS | 1995 |
|
RU2126088C1 |
| COOLED WORKING BLADE OF TURBINE | 1992 |
|
RU2043508C1 |
| AIR COOLING PATH OF BLADE OF NOZZLE APPARATUS OF HIGH PRESSURE TURBINE OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2686430C1 |
| HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
| METHOD OF ASSEMBLY OF DOUBLE-TIER FLOW SECTION OF TURBINE CYLINDER AND UNIT OF CONNECTION OF DIAPHRAGM RIM WITH BAFFLE PLATE OF REAR INTER-TIER SEAL FOR REALIZATION OF THIS METHOD (VERSIONS) | 1996 |
|
RU2146006C1 |
| HIGH-SPEED MOISTURE SEPARATOR FOR STEAM LINES OF STEAM TURBINES | 1993 |
|
RU2067666C1 |
| GAS TURBINE WHEEL COOLING DEVICE | 2000 |
|
RU2183747C1 |
| COOLED DOWN BLADE OF THE GAS TURBINE | 2017 |
|
RU2647351C1 |
| COOLED BLADE OF GAS TURBINE | 2003 |
|
RU2251622C2 |
| TURBOMACHINE COOLED BLADE | 1996 |
|
RU2117768C1 |
