FIELD: engines and pumps.
SUBSTANCE: set of invention relates to joint between screw-rotor compressor (2) with drive (3) and screw-rotor compressor with flange (1). Said flange (1) comprises central bore (4) for shaft (5) and/or bearing (6) to be fitted therein and first ring-like surface (7) to abut on compressor (2) casing (8) and second ring-like surface (9) fitting in casing (10) of drive (3). Flange (1) comprises seal (11) with axial force for sealing relative to casing (8) and seal (12) with radial force of sealing relative to shaft (5). Note here that exposed casing (8) can be closed and sealed at fitting the flange (1) in place. Flange (1) is shaped to bowl to confine cavity (20) to locate coupling (21) to abut on casing (8) and drive (3) casing (10) which couples compressor (2) shaft (5) with drive (3) shaft (22).
EFFECT: lower production and assembly costs, multifunctional flange.
12 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
COMPRESSOR ROTOR SEAL | 2013 |
|
RU2643269C2 |
SCREW COMPRESSOR | 2016 |
|
RU2689237C2 |
SCREW COMPRESSOR | 2009 |
|
RU2446314C2 |
SCREW COMPRESSOR | 0 |
|
SU1714200A1 |
SCREW COMPRESSOR | 2017 |
|
RU2733501C1 |
ROTOR SHAFT BEARING OF LOW-PRESSURE COMPRESSOR OF TURBOJET ENGINE (VERSIONS), SEALING SPOOL OF ROTOR SHAFT BEARING, ROTOR SHAFT BEARING BLOCK, CONTACT HUB OF ROTOR SHAFT BRACELET SEALING, OIL-CONTROL RING OF ROTOR SHAFT | 2016 |
|
RU2614017C1 |
SCREW COMPRESSOR | 2012 |
|
RU2587015C2 |
SCREW COMPRESSOR | 1998 |
|
RU2212564C2 |
SCREW COMPRESSOR | 2012 |
|
RU2642944C1 |
TURBOJET ENGINE ROTOR SHAFT SUPPORT (VERSIONS), TURBOJET ENGINE ROTOR SHAFT SUPPORT BODY, JET TURBINE ENGINE ROTOR SHAFT SUPPORT ROLLER BEARING HOUSING, TURBOJET ENGINE ROTOR SHAFT SUPPORT SEALING STAGES | 2015 |
|
RU2603386C1 |
Authors
Dates
2015-08-27—Published
2011-04-13—Filed