FIELD: manufacture of turbomachines. SUBSTANCE: end seal includes fixed grate 4 and rotary grate 5 and labyrinth sections 6, 7 located in series in way of leakage of working medium. Vane cascade is made in the form of turbine stage with nozzle grate 4 and working grate 5. EFFECT: reduced leakage and reduced sizes of seal. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STEAM TURBINE LOW-PRESSURE CYLINDER END SEAL | 1996 |
|
RU2107824C1 |
| AXIAL-FLOW TURBINE STAGE | 1996 |
|
RU2135780C1 |
| END-SEAL ASSEMBLY FOR STEAM-TURBINE CYLINDER | 1999 |
|
RU2174606C2 |
| TURBOMACHINE | 1992 |
|
RU2042835C1 |
| TURBOMACHINE AXIAL-RADIAL STAGE RUNNER | 1998 |
|
RU2153077C2 |
| COMBINED-CYCLE PLANT | 1997 |
|
RU2144994C1 |
| STEAM TURBINE OVERSHROUD SEAL | 2001 |
|
RU2210673C2 |
| REGULATING ORIFICE PLATE | 1996 |
|
RU2136898C1 |
| HONEYCOMB SEAL FOR TURBOMACHINE RADIAL CLEARANCE | 1998 |
|
RU2153112C2 |
| MULTI-STAGE CONTACTLESS SEALING DEVICE | 1996 |
|
RU2106556C1 |
Authors
Dates
1997-08-10—Published
1994-05-19—Filed