FIELD: machine building.
SUBSTANCE: in an elastic damper support of a turbomachine with inner and outer elastic bushings installed on a stator casing, a support ring, also flanges that limit an oil cavity, according to the invention, the inner and outer elastic bushings are made as a whole and are connected with a C-shaped elastic element, on the outer bushing there is a box-like circular casing with outer and inner circular air cavities separated with a cylindrical wall, in the box-like circular body there are radial channels of supply and discharge of oil and breathing of the oil cavity, and in the cylindrical wall - axial channels for bolt connection of the support ring and flanges with the outer elastic bushing, besides, the specified body is installed between the bushing and the support ring.
EFFECT: higher reliability of the elastic damper support due to reduction of heat supply to the oil cavity and higher durability of elastic bushings.
4 dwg
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|---|---|---|---|
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 | RU2414613C1 | 
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 | RU2572444C1 | 
| RESILIENT DAMPING SUPPORT OF TURBINE | 2017 | 
 | RU2644003C1 | 
| ELASTIC-DAMPER SUPPORT OF TURBOJET ENGINE | 2013 | 
 | RU2534686C1 | 
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 | RU2614017C1 | 
| 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 | 
| ELASTIC DAMPER ROTOR SUPPORT TURBOMACHINERY | 2014 | 
 | RU2579646C1 | 
Authors
Dates
2012-04-10—Published
2010-12-16—Filed