FIELD: machine building.
SUBSTANCE: group of inventions relates to turbomachines. Impeller (1) of turbomachine comprises hub (3) having axis (A-A) of rotation, covering disc (13), blades (5; 5A, 5B), located between hub (3) and covering disc (13), and flow channels (11). Each channel (11) is limited by hub (3) covering disk (13) and adjacent working blades (5; 5A, 5B) and has inlet and outlet. Each flow channel (11) passes inside in radial direction from its inlet in direction of the most internal in radial direction part of the specified channel and from the specified most internal in radial direction part to output of the specified channel.
EFFECT: inventions are aimed at reduction of oscillation amplitudes at approach to critical speed and increase in stiffness of rotor.
17 cl, 21 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| IMPELLER OF AXIAL TURBOMACHINE | 2019 |
|
RU2793173C2 |
| TURBO MACHINE TURBINE MANUFACTURING BY TUBULAR COMPONENTS ASSEMBLY | 2015 |
|
RU2719193C2 |
| LIQUID TOLERANT IMPELLER FOR CENTRIFUGAL COMPRESSORS | 2014 |
|
RU2680018C2 |
| TURBOMACHINE DOUBLE-FLOW WHEEL | 2006 |
|
RU2307253C1 |
| TURBO MACHINE IMPELLER VANE AND TURBO MACHINE | 2009 |
|
RU2488001C2 |
| ROTOR IMPELLER OF LP COMPRESSOR OF JET TURBINE ENGINE (VERSIONS) | 2014 |
|
RU2565091C1 |
| COOLING IMPELLER OF CENTRIFUGAL COMPRESSOR | 2013 |
|
RU2620620C2 |
| 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 |
| IMPELLER WHEEL OF FIRST STAGE OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VARIANTS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING | 2016 |
|
RU2630918C1 |
| SECOND STAGE IMPELLER WHEEL OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VARIANTS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING | 2016 |
|
RU2636998C1 |
