FIELD: machine building.
SUBSTANCE: invention relates to compressor engineering and can be used to prevent the transfer of oil from the frame to the cylinder cavity by a rod. An oil remover comprises a cover and a casing that are fitted by drain holes, a deflector is fixed on the casing and split oil scraper rings clamped by band springs are set in the casing, the deflector is made from a polymer material and is attached to the casing by screws with their diameter being less than the diameter of the deflector holes.
EFFECT: prevention of the deflector breakdown providing for the longer service life of the oil remover.
5 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| OIL REMOVER WITH SEALING ELEMENTS (VARIANTS) | 2018 |
|
RU2776837C2 |
| AIR COMPRESSOR STATION ON THE OPPOSITE BASE | 2022 |
|
RU2784159C1 |
| 0 |
|
SU418674A1 | |
| PACKING GLAND FOR GAS COMPRESSORS | 2013 |
|
RU2561960C2 |
| OIL REFLECTOR | 2013 |
|
RU2581341C2 |
| PISTON ROD | 2012 |
|
RU2497024C1 |
| SEALING DEVICE OF ROD SEAL | 2016 |
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RU2657026C2 |
| 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 |
| SUPPORT AND SEALING UNIT | 2014 |
|
RU2568370C1 |
| PISTON COMPRESSOR ON OPPOSITE BASES | 2016 |
|
RU2645885C2 |
