FIELD: energetics.
SUBSTANCE: invention relates to power engineering. Device for locking in axial direction of the sealing ring, made of abradable material and being in contact with periphery of module rotor of aircraft turbine machine. Device comprises support with the support hole, axial locking part, the device design provides the possibility of rotation of the locking part around axis between axial locking position for a packing ring and between the position for extraction of the above ring through the passage for extraction. Invention also discloses aircraft turbomachine module and aircraft turbomachine containing locking device.
EFFECT: invention allows to ensure a non-performance retainer sealing ring of the first stage of turbomachine module.
10 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBINE MODULE FOR GAS TURBINE ENGINE WITH MONOBLOCK ROTOR | 2005 |
|
RU2377417C2 |
| COMPRESSOR OUTER HOUSING OF AXIAL TURBOMACHINE WITH SEAL | 2015 |
|
RU2710458C2 |
| SEALING DEVICE BETWEEN ROTOR AND STATOR OF GAS TURBINE ENGINE | 2018 |
|
RU2762016C2 |
| OPEN AIR PROPELLER FOR TURBINE MACHINE | 2011 |
|
RU2558411C2 |
| ROTOR RING SEAL IN TURBINE STAGE | 2008 |
|
RU2476710C2 |
| TURBOMACHINE MODULE EQUIPPED WITH RADIAL GAP IMPROVEMENT DEVICE | 2008 |
|
RU2472000C2 |
| CONTROL OF GAP AT HEAD OF BLADES IN HIGH PRESSURE TURBINE OF TURBOMACHINE | 2008 |
|
RU2472001C2 |
| TURBINE MODULE FOR GAS TURBINE ENGINE | 2005 |
|
RU2377421C2 |
| AXIAL TURBINE MACHINE STATOR BLADES RETAINING RING AND AXIAL TURBOMACHINE | 2015 |
|
RU2614302C2 |
| SECTOR DISTRIBUTOR, LOW-PRESSURE TURBINE AND TURBO MACHINE INCORPORATING SAID DISTRIBUTOR | 2008 |
|
RU2484261C2 |
