FIELD: engines and pumps.
SUBSTANCE: stage of gas turbine with holes for dust concentrate discharge from cooling system comprises working and nozzle cooled blades that make the turbine wheel space, swirling apparatus with holes to fee cooling air to turbine components cooling system. Swirling apparatus has at least one extra dust concentrate discharge hole made at 0°<α<90° in working wheel rotation direction and at 0°<β<60° from engine axis. Dust concentrate discharge hole is located radially above cooling air feed holes in meridional plane at spacing larger than one cooling air feed hole diameter.
EFFECT: higher turbine reliability.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR COOLING HIGH-PRESSURE TURBINE NOZZLE ASSEMBLY (TNA) OF GAS TURBINE ENGINE (GTE) AND NOZZLE DEVICE OF GTE TNA (EMBODIMENTS) | 2018 |
|
RU2688052C1 |
| COOLING SYSTEM OF GAS-TURBINE ENGINE IMPELLER | 2012 |
|
RU2490473C1 |
| METHOD OF COOLING THE ROTOR OF A HIGH PRESSURE TURBINE (HPT) OF GAS TURBINE ENGINE (GTE), HPT ROTOR AND HPT ROTOR BLADE COOLED BY THIS METHOD, KNOT OF THE DEVICE OF TWISTING OF AIR OF HPT ROTOR | 2018 |
|
RU2684298C1 |
| METHOD OF COOLING AND REGULATING RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR ITS IMPLEMENTATION | 2020 |
|
RU2731781C1 |
| COOLED TURBINE OF GAS TURBINE ENGINE | 2001 |
|
RU2196233C1 |
| METHOD OF COOLING AND REGULATING RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2732653C1 |
| GAS TRANSFER UNIT | 2020 |
|
RU2735040C1 |
| CONTROL METHOD OF RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2738523C1 |
| GAS TRANSFER UNIT | 2020 |
|
RU2735881C1 |
| HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
