FIELD: turbine and compressor engineering. SUBSTANCE: stage of turbomachine has case 1 with ring grooves 17, passages 18 and hollow 19, guide apparatus 2 with deflectors set on their top shelves, ring grooves 14 and passages 16,15, porous bushing 3 with locator 7 for bearing and porous bushings 4 of thrust bearings, working vane rim 5 with axial grooves 6 provided on the inner shelf and ring grooves 25 provided on faces of inner and outer shelves, ring force shelf 8 of disk 9 with keys 10, bearing and stop sealing spring- loaded porous bushings 11,12 with ring locator 13, spring-loaded ring tabs 24, keys-locators 20, flexible washers 21, pins 22, axial gaps 23, and radial gaps. EFFECT: enhanced efficiency. 2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOMACHINE STAGE | 1990 |
|
RU2018697C1 |
TURBO-JET ENGINE | 1991 |
|
RU2027054C1 |
POWER PLANT | 1990 |
|
RU2011852C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614709C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
TURBINE MACHINE WITH BUILT-IN STARTER-GENERATOR | 2003 |
|
RU2321755C2 |
TURBO-ALTERNATOR TO PRODUCE ELECTRIC POWER | 2007 |
|
RU2380547C2 |
ROTOR FORTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING | 2016 |
|
RU2630919C1 |
TURBOJET LOW-PRESSURE COMPRESSOR THIRD STAGE DISC | 2014 |
|
RU2565140C1 |
METHOD OF OPERATION OF SUBMERSIBLE MULTI-STAGE CENTRIFUGAL PUMP WITH POLYMER IMPELLERS AND DESIGN FOR ITS IMPLEMENTATION | 2023 |
|
RU2810186C1 |
Authors
Dates
1994-01-15—Published
1989-05-06—Filed