GB2524820A - Jet pump - Google Patents

Jet pump Download PDF

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Publication number
GB2524820A
GB2524820A GB1406059.4A GB201406059A GB2524820A GB 2524820 A GB2524820 A GB 2524820A GB 201406059 A GB201406059 A GB 201406059A GB 2524820 A GB2524820 A GB 2524820A
Authority
GB
United Kingdom
Prior art keywords
nozzle
fluid
inlet
jet pump
fluids
Prior art date
Legal status (The legal status 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 status listed.)
Withdrawn
Application number
GB1406059.4A
Other versions
GB201406059D0 (en
Inventor
Mirza Najam Ali Beg
Mir Mahmood Sarshar
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caltec Ltd
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
Priority to GB1406059.4A priority Critical patent/GB2524820A/en
Publication of GB201406059D0 publication Critical patent/GB201406059D0/en
Priority to NO20150383A priority patent/NO20150383A1/en
Priority to US14/674,216 priority patent/US20150285271A1/en
Publication of GB2524820A publication Critical patent/GB2524820A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46—Arrangements of nozzles
    • F04F5/463—Arrangements of nozzles with provisions for mixing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/42—Jet 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/02—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid
    • F04F5/10—Jet 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/14—Jet 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
    • F04F5/24—Jet 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46—Arrangements of nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/54—Installations characterised by use of jet pumps, e.g. combinations of two or more jet pumps of different type

Abstract

A jet pump comprising an HP inlet 104, a nozzle 108 connected to the HP inlet, via an HP conduit 106, configured to discharge a first fluid into a nozzle discharge zone 110, an LP inlet 112, an LP conduit connected to the LP inlet configured to discharge a second fluid into the nozzle discharge zone, a mixing tube 118, an outlet 122 and a spinner mechanism 114 located upstream of the nozzle discharge zone for causing rotation of at least one of the fluids about a longitudinal axis of the nozzle. The spinner mechanism may be in the form of an involute or cylindrical LP inlet chamber extending circumferentially around the nozzle or a static spinner device, for example a device comprising at least one helical blade, located within the HP conduit. The pump provides significantly improved mixing of the two fluids, thus providing significantly improved operational efficiency.

Description

JET PUMP
The present invention relates to a jet pump and in particular, hut not exclusively, to a jet puinp for use in the oil and gas indusu-ies.
Jet pumps or eductors are passive devices that use energy from a high pressure (UP) fluid source to boost the pressure of a low pressure (LP) tluid. 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 tluid from a HP source passes through a UP inlet 4 to ajet 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 froni 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 sonic jet punips 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 thc HP fluid may bc 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 whcn thc 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 provide 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 UP inlet vent, a nozzle connected to the HP inlet vent via a UP 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 iiito 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 dischargc zonc 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 eircumlèrentially 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 upsutani end to its downsfteani 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 intation of the first fluid as it tiows 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 lisa 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; FigureS is a sectional side view of ajet pump assembly according to a second embodiment of the invention; Figure 6 is a cross-sectional view on live VI-VI of figureS; 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 having a nozzle 108 at one end. A HP first fluid tiowing 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 1-Il' 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 inhoduced 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 I 14 is defined between the curved wall 1 16 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 1 14 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 arc mixed within the fluxing tube I 18 downstream of the nozzle 108.
The spinning motion of the LP second fluid causes the first and second tluids 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 norrnalises as pressure recovery takes place. Finally, the mixture of tluids exits the jet pump 102 at outlet 122. The pressure of the fluid mixture at the outlet 122 will he 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 1 22.
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 Ilowing 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 UP 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 lIP 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 downsueam 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 IlK 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 ease spinning motion will be imparted only to the HP first fluids.

Claims (9)

  1. CLAIMSA 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. 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 circumtèrentially around the nozzle to cause rotation of the second fluid around the longitudinal axis of the nozzle.
  3. 3. A jet pump accoiding to claim 2, wherein the LP inlet chamber includes a curved wall that extends at least partly around the nozzle.
  4. 4, A jet pump according to claim 3, wherein the LP inlet chamber is substantially involute in shape.
  5. 5. A jet pump according to claim 3, wherein the LI' inlet chamber is substantially cylindrical in shapc.
  6. 6. A jet pump according to any one of claims 2 to 5, wherein the LI' inlet chamber has a tangential inlet port connected to the LP inlet vent.
  7. 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 disehargc zone.
  8. 8. A jct pump according to any one of the preceding claims, whcrcin t& spinner mechanism includes a static spinner device located within the H P fluid conduit, which is configured to cause rotation of the first fluid around the longiwdinal axis of the nozzle.
  9. 9. Ajet pump according to claim 8, wherein the static spinner device includes at least onc helical blade configured to cause rotation of the first fluid as it flows through the HP fluid conduit.
GB1406059.4A 2014-04-04 2014-04-04 Jet pump Withdrawn GB2524820A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB1406059.4A GB2524820A (en) 2014-04-04 2014-04-04 Jet pump
NO20150383A NO20150383A1 (en) 2014-04-04 2015-03-27 JET PUMP
US14/674,216 US20150285271A1 (en) 2014-04-04 2015-03-31 Jet pump

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
GB201406059D0 GB201406059D0 (en) 2014-05-21
GB2524820A true GB2524820A (en) 2015-10-07

Family

ID=50776806

Family Applications (1)

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

Country Status (3)

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

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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

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WO2013002872A2 (en) * 2011-06-10 2013-01-03 Carrier Corporation Ejector with motive flow swirl

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GB575024A (en) * 1944-07-18 1946-01-30 Wilfred Reginald Holloway Improvements in air ejectors
SU545776A1 (en) * 1975-04-09 1977-02-05 Куйбышевский политехнический институт им.В.В.Куйбышева Swirl Ejector
FR2646213A1 (en) * 1989-04-20 1990-10-26 Marzin Georges Marcel Jose Ejector (jet pump) for volumetric induction and compression
RU2052671C1 (en) * 1992-03-02 1996-01-20 Нефтегазодобывающее управление "Ласьеганнефть" Hydraulic vortex compressor
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
WO2013002872A2 (en) * 2011-06-10 2013-01-03 Carrier Corporation Ejector with motive flow swirl

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Publication number Publication date
US20150285271A1 (en) 2015-10-08
NO20150383A1 (en) 2015-10-05
GB201406059D0 (en) 2014-05-21

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