FIELD: pump production. SUBSTANCE: fluid viscosity is determined and gaps "b" are set between the disks. The gap is determined on the base of relationship as follows: 
, where τ is time to grow up boundary layer on the disks equal to 0.5 s; n is fluid kinematic viscosity coefficient; D is height of disk corrugations; d is height of disk riffling. EFFECT: improved efficiency and flowability. 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR SEPARATING DISSOLVED GASES FROM PUMPED FLUID AND DEVICE FOR ITS IMPLEMENTATION (VERSIONS) | 2016 |
|
RU2636732C1 |
| DISC-TYPE PUMP | 2012 |
|
RU2518716C2 |
| DISC-TYPE FRICTION PUMP FOR PUMPING LIQUIDS | 2016 |
|
RU2631854C1 |
| HORIZONTAL DISC-SHAPED HEAT- AND MASS-TRANSFER APPARATUS | 2008 |
|
RU2379096C2 |
| GRINDING TACKING FOR DISK MILL | 2009 |
|
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| DISK PUMP | 0 |
|
SU1681057A1 |
| PLACE OF MOUNTING OF WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION; BOOSTER ROTOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIRST GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF SWALLOWTAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES; METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR | 2016 |
|
RU2662755C2 |
| DISK PUMP | 0 |
|
SU1765525A1 |
| DISC PUMP | 0 |
|
SU1071807A1 |
| PLACE OF MOUNTING OF WORKING BLADES AND LOW AND HIGH PRESSURE COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION, ROTOR OF LOW PRESSURE COMPRESSOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIFTH GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF DOVETAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES, METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF ROTORS AND COMPRESSOR | 2017 |
|
RU2686353C2 |
