FIELD: engines and pumps.
SUBSTANCE: nut includes threaded part facing the inner race of bracket and lead-in part opposite to it, which has lead-in chamfer along outer surface, middle cylindrical part, installation cone and rear cylindrical part which is equal as to diametre to outer diametre of inner race of roller bearing. On inner side of lead-in part of the nut there made are radial protrusions forming the slots between each other to arrange axial locks which are rectangular in cross section. Slots are connected through radial holes to outer surface of middle cylindrical part of the nut. In the shaft there are mating slots for rectangular locks; at that, locks are provided with axial shanks arranged in mating slots of the shaft under the nut thread and fixed in axial direction with expansion elastic ring installed on inner side of lead-in part. During the operation of the support, rectangular locks of increased mechanical strength shall secure the nut in circumferential direction relative to the shaft. Since during the assembly of rotor there is no plastic deformation of locks, then in case there are no mechanical damages, locks can be used for many times.
EFFECT: improving reliability of the support owing to excluding the damage to the bearing rollers during the assembly of support and by increasing mechanical strength of the lock.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
FREE POWER TURBINE | 2016 |
|
RU2659694C2 |
GAS-TURBINE ENGINE | 2001 |
|
RU2204042C2 |
GAS TURBINE ENGINE SUPPORT | 2011 |
|
RU2459966C1 |
ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), CASING OF ROTOR SHAFT REAR BEARING, ROTOR SHAFT COMPONENT, POLYFUNCTIONAL EXTERNAL TIGHTENING COMPONENT OF ROTOR SHAFT, CONNECTION COMPONENT OF ROTOR SHAFT, CASING OF BEARING OF ROTOR SHAFT REAR BEARING | 2016 |
|
RU2614029C1 |
ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), CYLINDER CONSTITUENT OF ROTOR SHAFT, EXTERNAL TIGHTENING COMPONENT OF ROTOR SHAFT | 2016 |
|
RU2614018C1 |
TURBOJET ENGINE ROTOR SHAFT GARTER SEAL, TURBOJET ENGINE ROTOR SHAFT SEALING GARTER, JET TURBINE ENGINE GARTER SEAL CONTACT BUSHING, TURBOJET ENGINE ROTOR SHAFT SUPPORT | 2015 |
|
RU2603387C1 |
ELASTIC DAMPER ROTOR SUPPORT TURBOMACHINERY | 2014 |
|
RU2579646C1 |
ASSEMBLY OF JOINT BETWEEN GAS TURBINE ENGINE COMPRESSOR AND TURBINE ROTORS | 2009 |
|
RU2405955C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614709C1 |
Authors
Dates
2011-02-10—Published
2009-08-31—Filed