NO20150383A1 - JET PUMP - Google Patents

JET PUMP

Info

Publication number
NO20150383A1
NO20150383A1 NO20150383A NO20150383A NO20150383A1 NO 20150383 A1 NO20150383 A1 NO 20150383A1 NO 20150383 A NO20150383 A NO 20150383A NO 20150383 A NO20150383 A NO 20150383A NO 20150383 A1 NO20150383 A1 NO 20150383A1
Authority
NO
Norway
Prior art keywords
nozzle
fluid
jet pump
inlet
pump according
Prior art date
Application number
NO20150383A
Other languages
Norwegian (no)
Inventor
Mir Mahmood Sarshar
Mirza Najam Ali Beg
Original Assignee
Caltec Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Caltec Ltd filed Critical Caltec Ltd
Publication of NO20150383A1 publication Critical patent/NO20150383A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • F04F5/463Arrangements of nozzles with provisions for mixing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/42Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow characterised by the input flow of inducing fluid medium being radial or tangential to output flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/02Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid
    • F04F5/10Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid displacing liquids, e.g. containing solids, or liquids and elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/14Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid
    • F04F5/24Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing liquids, e.g. containing solids, or liquids and elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/54Installations characterised by use of jet pumps, e.g. combinations of two or more jet pumps of different type

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Mechanical Treatment Of Semiconductor (AREA)

Description

JET PUMP
The present invention relates to a jet pump and in particular, but not exclusively, to a jet pump for use in the oil and gas industries.
Jet pumps or eductors are passive devices that use energy from a high pressure (HP) fluid source to boost the pressure of a low pressure (LP) fluid. The terms jet pump, eductor, ejector and gas jet compressor are used in various industries and refer to the same general type of device. The HP and LP fluids may each consist of liquids, gases or a mixture of liquids and gases.
Figures 1 and 2 show the key features of a typical jet pump. HP fluid from a HP source passes through a HP inlet 4 to a jet pump 6, where it passes through constriction known as a nozzle 8 that increases the velocity of the fluid. In this way part of the potential (pressure) energy of the HP fluid is converted to kinetic energy (high velocity fluid). As a result, the pressure of the fluid in a nozzle discharge zone 10 in front of the nozzle 8 drops significantly.
LP fluid from a LP source passes through a LP inlet 12 and is introduced into the jet pump at the nozzle discharge zone 10, where it is entrained in the flow of fluid emerging from the nozzle 8. The mixture of fluids then passes through a mixing tube 14 where momentum and energy are exchanged between the fluids. The mixture finally passes through an expanding diffuser 16 where the velocity of flow normalises and pressure recovery takes place. The pressure at the outlet 18 of the jet pump will be at an intermediate value between the pressures of the HP and LP fluids and the inlets 4, 12. In some jet pumps the nozzle 8 and the mixing tube/diffuser 14, 16 comprise replaceable components that are mounted within a housing 20.
Jet pumps have been used successfully in a variety of applications onshore or near the bottom of oil or gas wells. In such situations the HP fluid may be gas or a high pressure liquid such as oil or water. The LP fluid could be gas, or liquid (oil and/or water), or a mixture of gas and liquid.
In some applications, particularly when the HP fluid is a liquid and the LP fluid is predominantly a gas, complete mixing of the HP and LP fluids may not take place. This can adversely affect the operational efficiency of the jet pump.
It is an object of the present invention to pro vide a jet pump that mitigates one or more of the aforesaid disadvantages.
According to one aspect of the present invention there is provided a jet pump including a HP inlet vent, a nozzle connected to the HP inlet vent via a HP fluid conduit and configured to discharge a first fluid flowing through the HP inlet into a nozzle discharge zone, a LP inlet vent, a LP fluid conduit connected to the LP inlet vent and configured to discharge a second fluid flowing through the LP inlet vent into the nozzle discharge zone, a mixing tube downstream of the nozzle discharge zone for mixing the first and second fluids and an outlet vent downstream of the mixing tube for discharging a mixture of the first and second fluids from the jet pump, wherein the jet pump includes a spinner mechanism upstream of the nozzle discharge zone for causing spinning rotation of at least one of the first and second fluids about a longitudinal axis of the nozzle.
We have found that by spinning at least one of the first and second fluids about a longitudinal axis of the nozzle, the mixing of the fluids in the mixing tube can be significantly improved. This applies in all situations, including even a situation where the HP first fluid is a liquid and the LP second fluid is predominantly a gas. Complete mixing of the HP and LP fluids can thus be ensured, thereby significantly improving the operational efficiency of the jet pump.
Advantageously, the spinner mechanism includes a LP inlet chamber connected to receive the second fluid from the LP fluid conduit, the LP inlet chamber comprising a fluid passageway that extends circumferentially around the nozzle to cause rotation of the second fluid around the longitudinal axis of the nozzle.
The LP inlet chamber may include a curved wall that extends at least partly around the nozzle. The LP inlet chamber may be substantially involute in shape, being defined by a curved wall that has a decreasing radius of curvature from its upstream end to its downstream end. Alternatively, the LP inlet chamber may be substantially cylindrical in shape.
Advantageously, the LP inlet chamber has a tangential inlet port connected to the LP inlet vent.
Advantageously, the LP inlet chamber has an annular outlet port configured to discharge the second fluid into the nozzle discharge zone.
Advantageously, the spinner mechanism includes a spinner device located within the HP fluid conduit, which is configured to cause rotation of the first fluid around the longitudinal axis of the nozzle. A spinner device may also be provided within the LP inlet chamber.
The spinner device preferably includes at least one helical blade configured to cause rotation of the first fluid as it flows through the HP fluid conduit.
Certain embodiments of the invention will now be described by way of example with reference to the accompanying drawings, in which: Figure 1 is a sectional side view of a known jet pump; Figure 2 is a sectional isometric view of a known jet pump; Figure 3 is a sectional side view of a jet pump assembly according to a first embodiment of the invention; Figure 4 is a cross-sectional view on live IV-IV of figure 3; Figure 5 is a sectional side view of a jet pump assembly according to a second embodiment of the invention;
Figure 6 is a cross-sectional view on live VI-VI of figure 5; and
Figure 7 is a sectional side-view of a nozzle assembly of a jet pump according to a third embodiment of the invention. Figures 3 and 4 show a jet pump according to a first embodiment of the invention. The jet pump includes a HP inlet 104 and an HP fluid conduit comprising an inlet tube 106 håving a nozzle 108 at one end. A HP first fluid flowing through the inlet tube 106 is discharged through the nozzle 108 into a low pressure nozzle discharge zone 110 in front of the nozzle 108. The nozzle 108 is constricted to increase the velocity of the fluid as it is discharged from the nozzle 108. In this way the potential (pressure) energy of the HP first fluid is converted to kinetic energy as the fluid emerges from the nozzle 108. This reduces the pressure at the low pressure nozzle discharge zone 110.
A low pressure second fluid from a LP source passes through an LP inlet 112 and is introduced into an involute inlet chamber 114 that encircles the inlet tube 106 and is positioned just upstream of the nozzle 108 and the low pressure nozzle discharge zone 110. The involute chamber 114 is defined by a curved wall 116 of decreasing radius that curves around the nozzle 108. The involute chamber 114 is defined between the curved wall 116 and the circular wall of the inlet tube 106. This chamber 114 has a cross-sectional area that decreases from the inlet end to the outlet end of the chamber.
The LP second fluid flowing through the LP inlet 112 into the involute inlet chamber 114 is guided by the curved wall 116 so that it rotates around the inlet tube 106 as shown in Figure 4. The speed of the rotating second fluid increases as it flows through the chamber 114 as a result of the decreasing cross-sectional area of the involute inlet chamber 114.
The rotating second fluid exits the involute inlet chamber 114 through an annular gap 117 that surrounds the inlet tube 106. The rotating LP second fluid is then combined in the nozzle discharge zone 110 with the first fluid emerging from the nozzle 108 and the first and second fluids are mixed within the mixing tube 118 downstream of the nozzle 108. The spinning motion of the LP second fluid causes the first and second fluids to mix thoroughly within the mixing tube 118. The mixture of fluids then passes through an expanding diffuser 120 where the velocity of the flow normalises as pressure recovery takes place. Finally, the mixture of fluids exits the jet pump 102 at outlet 122. The pressure of the fluid mixture at the outlet 122 will be at an intermediate value between the pressures of the first and second fluids at the HP and LP inlets 104, 112.
In this embodiment the inlet tube 106 and the mixing tube/diffuser 118, 120 are replaceable components that are mounted within a housing 124. Alternatively, the nozzle 108, the mixing tube 118 and the diffuser 120 may be permanently mounted within or formed integrally with the housing 124.
Figures 5 and 6 depict a jet pump according to a second embodiment of the invention. This embodiment is similar to the first embodiment described above, except that the low pressure inlet chamber 124 has a different cross-sectional shape.
The second jet pump shown in Figures 5 and 6 includes a HP inlet 104 and an inlet tube 106 that has a nozzle 108 at its downstream end. The nozzle 108 is arranged to discharge a first fluid emerging from the nozzle into a LP nozzle discharge zone 110 downstream of the nozzle. The discharged fluid then flows through a mixing tube 118 and a diffuser 120 towards an outlet vent 122.
In the embodiment of figures 5 and 6 the LP inlet chamber 124 is cylindrical and is defined by a curved wall 126 that encircles the inlet tube 106 upstream of the nozzle 108. The LP inlet 112 is connected tangentially to the LP inlet chamber 124, to feed a LP second fluid tangentially into the LP inlet chamber 124. As a result, the LP second fluid rotates around the nozzle 108 before flowing into the LP nozzle discharge zone 110 downstream of the nozzle 108 through an annular opening 127. The rotational movement of the LP second fluid aids mixing of the second fluid with the high velocity first fluid emerging from the nozzle 108, thereby improving the operational efficiency of the jet pump.
The two fluids are mixed within the mixing tube 118 and the mixture then flows through the diffuser 120 towards the outlet 122. As before, the mixture of fluids emerging from the outlet 122 will have a pressure that is intermediate between the pressures of the first and second fluids at the HP and LP inlets 104, 112.
Optionally, the HP inlet tube 106 may include a mechanical static spinner device 130 located within the HP inlet tube 106 upstream of the nozzle 108, as shown in figure 7. This spinner device 130 may for example take the form of helical blades provided on the inner wall of the HP inlet tube 106, which cause the HP first fluid flowing through the HP inlet tube to rotate about the axis of the tube. The spinning motion of the fluid will be maintained as the fluid emerges from the nozzle 108, thereby enhancing mixing of the first and second fluids in the LP nozzle discharge zone 110 downstream of the nozzle 108 and in the mixing tube 118. This spinner device 130 may be combined with either of the LP inlet chambers 114, 124 of the first and second embodiments described above and shown in Figures 3-6 so that both fluid streams are spinning as they enter the mixing tube 118. Alternatively the spinner device 130 may be used on its own with a conventional LP inlet arrangement as depicted in Figures 1 and 2, in which case spinning motion will be imparted only to the HP first fluids.

Claims (9)

1. A jet pump including a HP inlet vent, a nozzle connected to the HP inlet vent via a HP fluid conduit and configured to discharge a first fluid flowing through the HP inlet into a nozzle discharge zone, a LP inlet vent, a LP fluid conduit connected to the LP inlet vent and configured to discharge a second fluid flowing through the LP inlet vent into the nozzle discharge zone, a mixing tube downstream of the nozzle discharge zone for mixing the first and second fluids and an outlet vent downstream of the mixing tube for discharging a mixture of the first and second fluids from the jet pump, wherein the jet pump includes a spinner mechanism upstream of the nozzle discharge zone for causing spinning rotation of at least one of the first and second fluids about a longitudinal axis of the nozzle.
2. A jet pump according to claim 1, wherein the spinner mechanism includes a LP inlet chamber connected to receive the second fluid from the LP fluid conduit, the LP inlet chamber comprising a fluid passageway that extends circumferentially around the nozzle to cause rotation of the second fluid around the longitudinal axis of the nozzle.
3. A jet pump according to claim 2, wherein the LP inlet chamber includes a curved wall that extends at least partly around the nozzle.
4. A jet pump according to claim 3, wherein the LP inlet chamber is substantially involute in shape.
5. A jet pump according to claim 3, wherein the LP inlet chamber is substantially cylindrical in shape.
6. A jet pump according to any one of claims 2 to 5, wherein the LP inlet chamber has a tangential inlet port connected to the LP inlet vent.
7. A jet pump according to any one of claims 2 to 6, wherein the LP inlet chamber has an annular outlet port configured to discharge the second fluid into the nozzle discharge zone.
8. A jet pump according to any one of the preceding claims, wherein the spinner mechanism includes a static spinner device located within the HP fluid conduit, which is configured to cause rotation of the first fluid around the longitudinal axis of the nozzle.
9. A jet pump according to claim 8, wherein the static spinner device includes at least one helical blade configured to cause rotation of the first fluid as it flows through the HP fluid conduit.
NO20150383A 2014-04-04 2015-03-27 JET PUMP NO20150383A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1406059.4A GB2524820A (en) 2014-04-04 2014-04-04 Jet pump

Publications (1)

Publication Number Publication Date
NO20150383A1 true NO20150383A1 (en) 2015-10-05

Family

ID=50776806

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20150383A NO20150383A1 (en) 2014-04-04 2015-03-27 JET PUMP

Country Status (3)

Country Link
US (1) US20150285271A1 (en)
GB (1) GB2524820A (en)
NO (1) NO20150383A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9494166B1 (en) * 2015-12-22 2016-11-15 Syphon Energy, LLC Jet-gas lift system and method for pumping well fluids
FR3050778B1 (en) * 2016-04-27 2020-02-14 Safran Aircraft Engines JET PUMP FOR A TURBOMACHINE, INCLUDING A BLADE FOR ROTATING ACTIVE FLUID
GB2558627B (en) * 2017-01-11 2020-02-26 Transvac Systems Ltd Ejector device
CN106975379A (en) * 2017-04-08 2017-07-25 深圳欧威奇科技有限公司 A kind of jet mixer of air inlet biasing
JP7243096B2 (en) * 2018-09-14 2023-03-22 富士電機株式会社 Ejector
NO20220710A1 (en) * 2022-06-21 2023-12-22 Norrde As A multi-stage venturi-type apparatus, liquid treatment system, aquafarm, and method for treating liquid in a tank

Family Cites Families (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US718683A (en) * 1902-04-07 1903-01-20 George C Wiedenmayer Carbonating device.
US1517467A (en) * 1920-09-29 1924-12-02 Westinghouse Electric & Mfg Co Steam-actuated ejector
US1619808A (en) * 1923-04-13 1927-03-08 Curtis B Camp Suction-producing means for fuel-feeding systems
US1612838A (en) * 1925-04-09 1927-01-04 Centrifix Corp Draft-inducing means
GB575024A (en) * 1944-07-18 1946-01-30 Wilfred Reginald Holloway Improvements in air ejectors
US3099965A (en) * 1958-01-02 1963-08-06 Krantz H Fa Jet conveyors
US3007322A (en) * 1961-04-03 1961-11-07 Adiel Y Dodge Low pressure exhauster
US3134338A (en) * 1961-08-07 1964-05-26 A Y Dodge Co Jet pump
US3131645A (en) * 1961-11-28 1964-05-05 A Y Dodge Co Vortex jet pump
US3667069A (en) * 1970-03-27 1972-06-06 Univ Minnesota Jet pump cardiac replacement and assist device and method of at least partially replacing a disabled right heart
SU545776A1 (en) * 1975-04-09 1977-02-05 Куйбышевский политехнический институт им.В.В.Куйбышева Swirl Ejector
US4245961A (en) * 1978-09-08 1981-01-20 Martin Marietta Corporation Ejector utilizing a vortex flow
US4834132A (en) * 1986-09-25 1989-05-30 Nissan Motor Company, Limited Fuel transfer apparatus
JP2598091B2 (en) * 1988-07-15 1997-04-09 日産自動車株式会社 Fuel suction device for fuel tank
JPH0745856B2 (en) * 1988-12-23 1995-05-17 日産自動車株式会社 Fuel suction device for fuel tank
FR2646213A1 (en) * 1989-04-20 1990-10-26 Marzin Georges Marcel Jose Ejector (jet pump) for volumetric induction and compression
US5160610A (en) * 1990-11-13 1992-11-03 Smith & Loveless, Inc. Radial header for dissolved air flotation systems
RU2052671C1 (en) * 1992-03-02 1996-01-20 Нефтегазодобывающее управление "Ласьеганнефть" Hydraulic vortex compressor
DE4234538C1 (en) * 1992-10-14 1994-04-14 Herbst Bremer Goldschlaegerei Device for extracting gases, especially those containing dust
GB9817073D0 (en) * 1997-11-04 1998-10-07 Bhr Group Ltd Phase separator
FR2787838B1 (en) * 1998-12-23 2002-01-11 Inst Francais Du Petrole JET PUMPING DEVICE
DE10016924A1 (en) * 2000-04-05 2001-07-12 Voith Paper Patent Gmbh Jet pump has two fluid feeds to be mixed for delivery where the jet tube has an axial adjustment against the mixer tube which can be set and varied while the pump is operating
US6491064B2 (en) * 2000-12-06 2002-12-10 Juergen Kampe Apparatus for charging a liquid medium with a gas
GB0410961D0 (en) * 2004-05-17 2004-06-16 Caltec Ltd A separation system for handling and boosting the production of heavy oil
FR2883601B1 (en) * 2005-03-22 2007-10-05 Melchior Jean F DEVICE FOR ACCELERATING A TURBOCOMPRESSION GROUP AT LOW REGIMES OF AN ALTERNATIVE MOTOR AND ALTERNATIVE MOTOR COMPRISING SUCH A DEVICE
GB2440726B (en) * 2006-08-12 2011-05-18 Caltec Ltd Cyclonic separator and a method of separating fluids
DE102006045088A1 (en) * 2006-09-21 2008-03-27 Basf Ag Mixing a liquid or suspension beneath a gas space in a closed container comprises supplying a stream of the liquid or suspension as a drive jet for a submerged ejector which aspirates gas from the gas space
GB2453586B (en) * 2007-10-12 2012-04-11 Caltec Ltd Apparatus for and method of separating multi-phase fluids
KR101278529B1 (en) * 2010-03-18 2013-06-25 삼성전자주식회사 A Vacuum Pump Ejector and A Vacuum Pump Having the Same
US10928101B2 (en) * 2011-06-10 2021-02-23 Carrier Corporation Ejector with motive flow swirl
JP5999071B2 (en) * 2012-12-27 2016-09-28 株式会社デンソー Ejector
JP6056596B2 (en) * 2013-03-27 2017-01-11 株式会社デンソー Ejector
JP2014224626A (en) * 2013-05-15 2014-12-04 株式会社デンソー Ejector
JP6115344B2 (en) * 2013-06-18 2017-04-19 株式会社デンソー Ejector
JP6115345B2 (en) * 2013-06-18 2017-04-19 株式会社デンソー Ejector
JP6003844B2 (en) * 2013-08-09 2016-10-05 株式会社デンソー Ejector
GB2521172A (en) * 2013-12-11 2015-06-17 Caltec Ltd Commingling device
JP6176127B2 (en) * 2014-01-21 2017-08-09 株式会社デンソー Ejector

Also Published As

Publication number Publication date
GB201406059D0 (en) 2014-05-21
GB2524820A (en) 2015-10-07
US20150285271A1 (en) 2015-10-08

Similar Documents

Publication Publication Date Title
US20150285271A1 (en) Jet pump
JP4426612B2 (en) Fine bubble generation nozzle
WO2016088725A1 (en) Gas-liquid separation device
US10578110B2 (en) Centrifugal pump with coalescing effect, design method and use thereof
TW201827121A (en) Device and system for generating gas-liquid containing microbubbles
WO2010041565A1 (en) Microbubble generating pump, microbubble generating pump rotor blade and microbubble generating pump stator blade
US8721168B2 (en) Homogenizer device having a rotor and an advance wheel (inducer screw) that can rotate opposite to the rotor and a counter-current rotor that can rotate opposite to the rotor
US7153097B2 (en) Centrifugal impeller and pump apparatus
US20210213400A1 (en) Gas-liquid mixing device
CN107820544B (en) Self-aspirating pump assembly
WO1999054629A1 (en) Liquid-gas jet apparatus and variants
RU173966U1 (en) VORTEX GAS SEPARATOR
JP6663269B2 (en) Compressor
US3185107A (en) Vortex jet pump
RU158649U1 (en) PUMP - DISPERSANT
RU2518769C1 (en) Turbopump for two fluids
RU2361118C2 (en) Pump-jet unit
RU2398638C1 (en) Vortex cavitation device
RU2260147C2 (en) Vortex injector
RU2776733C2 (en) Centrifugal rotor
RU2660002C1 (en) Pneumatic swirl atomizer
RU2433314C1 (en) Radial-flow pump two-flow hydraulic discharge device
RU2390656C2 (en) Centrifugal fan
RU2181853C1 (en) Axial centrifugal pump
RU2638100C1 (en) Vortex pump

Legal Events

Date Code Title Description
FC2A Withdrawal, rejection or dismissal of laid open patent application