FIELD: instrument making.
SUBSTANCE: balancing mechanism is normally incorporated with the disk of rotors furnished with a rim. The proposed mechanism comprises seats made in aforesaid rim, balancing weights fitted in the said seats. Note here that the seats are closed by lock ring. The mechanism is used in rotor including one-piece blade disks.
EFFECT: simplified balancing mechanism.
22 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET TURBINE ROTOR | 2012 |
|
RU2493371C1 |
| COMPRESSOR ROTOR OF GAS TURBINE ENGINE | 2000 |
|
RU2188339C2 |
| HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
| DEVICE FOR BALANCING OF ROTARY PART, IN PARTICULAR TURBOJET ENGINE ROTOR | 2005 |
|
RU2361090C2 |
| GAS TURBINE ENGINE LOW-PRESSURE TURBINE (LPT) (VERSIONS), ROTOR SHAFT CONNECTION UNIT WITH LPT DISC, LPT ROTOR AIR COOLING PATH AND AIR FEEDING APPARATUS FOR COOLING LPT ROTOR BLADES | 2018 |
|
RU2684355C1 |
| 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 |
| FIRST STAGE COMPRESSOR DISC CONFIGURED FOR BALANCING THE COMPRESSOR ROTOR ASSEMBLY | 2013 |
|
RU2650237C2 |
| FIRST STAGE DISC OF TURBOJET ENGINE LOW-PRESSURE COMPRESSOR ROTOR SHAFT (VERSIONS) | 2015 |
|
RU2603217C1 |
| METHOD OF MAKING TURBINE DISC AND TURBINE | 2011 |
|
RU2581296C2 |
| METHOD OF PRODUCING ROTOR OR BLADED MACHINE, MACHINE TOOL FOR GRINDING AND DEVICE FOR AUTOMATIC CONTROL | 1996 |
|
RU2179502C2 |
