FIELD: machine building.
SUBSTANCE: resilient support of a turbomachine rotor comprises a radial bearing set on a shaft with the bearing housing being connected to a stator element, and the stator element is fitted by slits with girders located between them and oriented in the radial direction in respect to the support axis.
EFFECT: invention allows for the reduction of axial dimensions and weight at keeping the required stiffness and reliability.
2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBO MACHINE ROTOR ELASTICALLY DAMPING BEARING ASSEMBLY | 2013 |
|
RU2514527C1 |
RESILIENT SUPPORT OF TURBOMACHINE ROTOR | 2014 |
|
RU2574945C1 |
TURBOMACHINE ROTOR SUPPORT | 2014 |
|
RU2551452C1 |
RESILENT DAMPING SUPPORT WITH ADJUSTABLE RIGIDITY | 2016 |
|
RU2634512C1 |
ROTARY MACHINE RESILIENT-DAMPING SUPPORT | 2005 |
|
RU2303143C1 |
RESILIENT DAMPING SUPPORT OF TURBOMACHINE ROTOR | 2013 |
|
RU2525373C1 |
SHAFT ELASTIC SUPPORT DEVICE AND METHOD OF THE SHAFT OSCILLATIONS CONTROL | 2017 |
|
RU2656936C1 |
TURBOJET ENGINE ROTOR SHAFT SUPPORT (VERSIONS), TURBOJET ENGINE ROTOR SHAFT SUPPORT GARTER SEAL, TURBOJET ENGINE ROTOR SHAFT SUPPORT SEALING GARTER ASSEMBLY, TURBOJET ENGINE ROTOR SHAFT SUPPORT GARTER SEAL RING SECTION | 2015 |
|
RU2603389C1 |
ELASTICITY-DAMPER SUPPORT WITH ADJUSTABLE STIFFNESS | 2016 |
|
RU2623703C1 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614709C1 |
Authors
Dates
2014-09-27—Published
2013-06-06—Filed