FIELD: turbines or turbomachines.
SUBSTANCE: device (1) for balancing rotor (2) of turbomachine comprises main part (3) made with possibility of coaxial attachment to rotor (2) and drive, and at least three balancing tools (4), which are located on main part (3) and each of which sets appropriate balancing direction (B) along radial direction of main part (3), wherein each balancing tool (4) comprises load (5) configured to move in the balance direction (B), wherein balancing directions (B) pass with uniform angular spacing, wherein main part (3) is configured to transmit torque from drive to rotor (2) of turbomachine.
EFFECT: enabling balancing of rotor without its stopping.
16 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COUPLING FOR ROTOR BALANCING | 2010 |
|
RU2550716C2 |
| AUTOMATIC BALANCING DEVICE | 0 |
|
SU1352270A1 |
| METHOD USED TO COMPENSATE FOR UNBALANCE POSITION CORRECTION AND TO CORRECT DEGREE OF UNBALANCE ON BALANCING MACHINE | 2002 |
|
RU2294046C2 |
| METHOD AND GEAR FOR DYNAMIC BALANCING OF GIMBAL DRIVE | 2002 |
|
RU2225603C2 |
| METHOD OF REPLACEMENT OF AXIAL-FLOW COMPRESSOR MOVING BLADES | 1992 |
|
RU2013568C1 |
| ROTOR WITH OUT-OF-BALANCE COMPENSATOR | 2012 |
|
RU2516722C1 |
| PASSIVE DYNAMIC INERTIAL ROTOR BALANCE SYSTEM FOR TURBOMACHINERY | 2013 |
|
RU2597722C2 |
| DEVICE FOR OBJECT BALANCING | 1999 |
|
RU2147733C1 |
| SPLIT TURBOCHARGER BEARING ASSEMBLY | 2015 |
|
RU2637607C2 |
| METHOD OF REPLACING ASSEMBLY OF WORKING VANES OF TURBINE STAGE OF GAS-TURBINE ENGINE | 1995 |
|
RU2099541C1 |
