FIELD: machine building.
SUBSTANCE: turbomachine rotor support containing a bearing, which internal ring is installed on the shaft, a casing with lid, in which a bearing race and raceway are installed, at that between the casing and race a bushing is installed, it is made out of two rings, and is spring-loaded at one end in axial direction, and by the another end is in contact with the lid, at that the contacting ends of the adjacent rings are made cone relatively to the shaft longitudinal central line.
EFFECT: invention simplifies design of the support of the turbine machine rotor, reduces wear of the rings, and heat generation in the support, resulting in increased service life and reliability.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RESILIENT DAMPING SUPPORT OF TURBOMACHINE ROTOR | 2014 |
|
RU2563952C1 |
| END SEAL OF TURBOMACHINE ROTOR | 2013 |
|
RU2525378C1 |
| TURBINE MACHINE ROTOR | 2014 |
|
RU2563955C1 |
| CONTACT GRAPHITE SEALING OF TURBINE MACHINE ROTOR | 2014 |
|
RU2561809C1 |
| CONTACT RADIAL-BUTT GRAPHITE SEALING OF THE TURBO MACHINE ROTOR | 2017 |
|
RU2663368C1 |
| DEVICE FOR MEASUREMENT OF AXIAL FORCE OF TURBINE MACHINE ROTOR | 2015 |
|
RU2601513C1 |
| END CONTACT SEAL OF TURBOMACHINE ROTOR | 2016 |
|
RU2634510C1 |
| TURBOMACHINE ROTOR SUPPORT | 2014 |
|
RU2555599C1 |
| SUPPORT OF LOW-PRESSURE COMPRESSOR OF TURBOMACHINE | 2015 |
|
RU2596899C1 |
| COMBINATION SEAL OF TURBOMACHINE | 2016 |
|
RU2614910C1 |
