FIELD: turbo-machine.
SUBSTANCE: turbo-machine containing at least one shaft and at least one bearing guiding in rotation the said shaft around the turbomachine axis; a bearing containing the first internally located in radial direction ring and the second externally located in radial direction ring, between which moving elements are arranged; a turbo-machine, in which the first ring is installed floating on the said shaft by means of a damping thin fluid layer.
EFFECT: technical result is the increase of reliability by excluding deformation of the shaft with the bearing.
9 cl, 10 dwg
| Title |
Year |
Author |
Number |
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2015 |
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|
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2014 |
|
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2014 |
|
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- Bujer Filipp
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|
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2011 |
|
RU2575512C2 |
| JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR |
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|
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2011 |
|
RU2578264C2 |
| TURBOMACHINE WITH GEARBOX FOR AIRCRAFT |
2018 |
- Bekule, Zhyulen, Faben, Patrik
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- Pomme, Nikolya, Ogyust, Marsel
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|
RU2774134C2 |
| LUBRICATING DEVICE FOR LUBRICATION OF TURBO-MACHINE ELEMENTS AND TURBOJET ENGINE |
2005 |
- Prestel' Sebast'En
- Renon Oliv'E
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|
RU2358132C2 |
| RESILIENT DAMPING SUPPORT OF ROTOR HEAVY TURBO-MACHINE |
2014 |
|
RU2592664C2 |
