WO2012175915A1 - Pump assembly comprising a plurality of jet pumps - Google Patents

Pump assembly comprising a plurality of jet pumps Download PDF

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Publication number
WO2012175915A1
WO2012175915A1 PCT/GB2012/000533 GB2012000533W WO2012175915A1 WO 2012175915 A1 WO2012175915 A1 WO 2012175915A1 GB 2012000533 W GB2012000533 W GB 2012000533W WO 2012175915 A1 WO2012175915 A1 WO 2012175915A1
Authority
WO
WIPO (PCT)
Prior art keywords
zone
inlet
outlet
jet
pump
Prior art date
Application number
PCT/GB2012/000533
Other languages
English (en)
French (fr)
Inventor
Mir Mahmood Sarshar
Mirza Najam Ali Beg
Raja Kishore Nalukurthy
Original Assignee
Caltec Limited
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 Limited filed Critical Caltec Limited
Priority to BR112013032509A priority Critical patent/BR112013032509A2/pt
Priority to GB1320575.2A priority patent/GB2505586A/en
Priority to US14/128,934 priority patent/US20140255218A1/en
Publication of WO2012175915A1 publication Critical patent/WO2012175915A1/en
Priority to NO20131706A priority patent/NO20131706A1/no

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
    • F04F5/54Installations characterised by use of jet pumps, e.g. combinations of two or more jet pumps of different type
    • 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
    • F04F5/44Component 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
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • F04F5/466Arrangements of nozzles with a plurality of nozzles arranged in parallel

Definitions

  • the present invention relates to a pump assembly and in particular, but not exclusively, to a pump assembly using jet pumps 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.
  • HP high pressure
  • LP low pressure
  • jet pump, eductor, ejector and gas jet compressor are used in various industries and refer to the same general type of device.
  • FIG. 1 shows the key features of a typical jet pump.
  • HP fluid from a HP source 2 passes through a conduit 4 to a jet pump 6, where it passes through constriction known as a nozzle 8 that increases its velocity.
  • a nozzle 8 that increases its velocity.
  • part of the potential (pressure) energy of the HP fluid is converted to kinetic energy (high velocity fluid).
  • LP fluids from a LP source 10 pass through a conduit 12 and are introduced at this point and entrained in the flow.
  • the mixture of fluids then passes through a mixing tube 14 where momentum and energy are exchanged between the HP and LP 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 sources 2, 10. Jet pumps have been used successfully in a variety of applications onshore or near the bottom of oil or gas wells.
  • the HP flow is gas or a high pressure liquid such as oil or water.
  • the LP flow could be gas, or liquid (oil and water), or a mixture of the two.
  • Jet pumps with interchangeable internals have been designed and supplied.
  • An example is shown in figure 2.
  • This jet pump 6 includes a housing 20 with a HP inlet 22, a LP inlet 24 and an outlet 26.
  • Mounted within the housing 20 are a nozzle assembly 28 and a separate mixer/diffuser tube 30.
  • a multi-nozzle pump assembly has been proposed, as shown in figure 3.
  • a single housing 32 is provided, which accommodates a plurality of nozzles 34.
  • the housing has a LP inlet 36 and a single mixing tube/diffuser 38 for receiving the mixture of HP and LP fluids.
  • Each nozzle 34 has a valve 40 to switch it on or off, so as to supply the desired total amount of HP fluid through feed lines 42.
  • This increases the size of the pump assembly because of the need for a valve for each nozzle, and this is not usually welcomed by the industry.
  • the efficiency of the pump assembly is limited by the provision of a single mixing tube/diffuser, which prevents it from operating efficiently over a wide range of flow rates.
  • Subsea production systems may consist of a variety of components such as manifolds, valves and in some cases booster pumps and separators, all of which are located on the sea bed to avoid the need for costly offshore platforms. All equipment that is installed subsea for any function needs to be highly reliable, with little to no maintenance requirement or changes to design requiring retrieval of the unit to surface, as the cost of retrieving such units for maintenance, repair, or modification is very high, especially in deep water applications. It is also desirable in many offshore platforms to minimise maintenance work, and to minimise the need to isolate and de-pressurise the jet pump and replace its internal components.
  • apump assembly comprising a housing and a plurality of jet pumps arranged within the housing, wherein the housing includes a HP inlet, a LP inlet and an outlet and is divided internally by partitions into a HP zone, a LP zone and an outlet zone, said partitions comprising a first partition between the HP zone and the LP zone, and a second partition between the LP zone and the outlet zone, said LP zone being located longitudinally between the HP zone and the outlet zone, and each jet pump includes a nozzle assembly, a mixing tube and a diffuser and comprises an elongate tubular body having an HP inlet at a first end of the body, an outlet at a second end of the tubular body and a LP inlet between the first and second ends, wherein each jet pump is mounted within the housing with the HP inlet located in the HP zone, the LP inlet located in the LP zone, and the outlet located in the outlet zone, and each jet pump extends through and is sealed to the first and
  • each jet pump includes a nozzle assembly, a mixing tube and a diffuser, it is capable of efficient operation, as the nozzle assembly may be matched specifically to the mixing tube and the diffuser design.
  • the pump assembly can also be modularised, consisting of a number of standard, off-the- shelf, components that can be selected according to specific production conditions including, for example, the flow rate, pressure and flow regime of the produced fluids. These components can then be assembled relatively quickly and easily, allowing a custom- designed pump assembly to be supplied quickly and at relatively low cost.
  • each jet pump is sealed to the partitions, for example by means of O-ring seals or by welding.
  • the housing is T-shaped, having a longitudinal axis and a transverse axis, the HP inlet being located at one end of the longitudinal axis, the outlet being located at the opposite end of the longitudinal axis and the LP inlet being located on the transverse axis.
  • the housing comprises a T-section pipe.
  • the jet pumps Preferably, at least some of the jet pumps have common external dimensions. More preferably, all the jet pumps have common external dimensions, or they all have "standard" external dimensions, selected for example from two or more alternative sets of dimensions.
  • At least one of the jet pumps is substantially cylindrical having a HP inlet at one end, an outlet at an opposite end and a LP inlet in a side thereof.
  • the pump assembly includes isolation means for isolating at least one of the jet pumps. This allows individual jet pumps to be turned on or off, thereby adapting the system to changes in operating conditions.
  • the isolation means preferably comprises means for stopping the HP inlet, the LP inlet and/or the outlet of at least one of the jet pumps.
  • the isolation means comprises means for stopping two of the three inlet and outlet vents.
  • the pump assembly preferably includes an actuator for actuating the isolation means to isolate individual jet pumps, allowing the system to be adapted to changes in operating conditions from a remote location.
  • the actuator comprises a hydraulically-driven valve.
  • the invention provides a modularised, multi-jet pump unit, which allows the operator to use any number of standard jet pump units as needed, depending on the field conditions, without having to isolate the system, remove the old internals and introduce new sets of internals.
  • Each jet pump unit consists of the same key components of a nozzle, a mixing tube and a diffuser.
  • the multiple jet pump units are housed in a containment pressure vessel or pipe section for ease of handling and for isolating the system against exposure to subsea environment, or in the case of offshore platforms achieve the full pressure rating of the total jet pump system. The key features of the new system are described below.
  • Figure 1 is a schematic representation of a first known jet pump system
  • Figure 2 is a sectional isometric view of a second known jet pump system
  • Figure 3 is a sectional side view of a third known multi-nozzle jet pump system
  • Figure 4 is a sectional side view of a pump assembly according to an embodiment of the invention.
  • Figure 5 is a cross-sectional view on live IV-IV of figure 4.
  • Figure 6 is a sectional side view of a jet pump comprising part of the pump assembly of figure 4, and
  • Figure 7 is a partial sectional view of another jet pump having hydraulically-activated valve.
  • the pump assembly shown in Figures 4, 5 and 6 comprises a housing 50 and a plurality of jet pumps 52 arranged within the housing 50.
  • the housing 50 comprises a T-section pipe is T-shaped having a longitudinal axis and a transverse axis.
  • An HP inlet 54 is located at one end of the longitudinal axis
  • an outlet 56 is located at the opposite end of the longitudinal axis
  • a LP inlet 58 is located on the transverse axis.
  • the HP and LP inlets 54, 58 and the outlet 56 are each provided with flanges 60 for connection to external pipelines (not shown).
  • the housing 50 is divided internally into a HP zone 62, a LP zone 64 and an outlet zone 66 by two partition walls 68, 70 the LP zone being located longitudinally between the HP zone and the outlet zone.
  • the first partition wall 68 is located between the HP zone 62 and the LP zone 64
  • the second partition wall 70 is located between the LP zone and the outlet zone.
  • Each of these partition walls 68, 70 includes a plurality of apertures 72 for receiving the individual jet pumps 52. In the embodiment shown in Figures 4 to 6 nine apertures 72 are provided in each wall 68, 70, eight of these being arranged in a circle around the ninth aperture. These numbers may vary depending on field conditions and expectations of the extent of changes during the service life of the system.
  • Each jet pump 52 is substantially cylindrical comprising an elongate tubular body 73 having a HP inlet 74 at a first end of the body, an outlet 76 at a second end of the body and a LP inlet vent 78 in a side of the body between the first and second ends thereof. It is supported by the partition walls 68, 70 so that the HP inlet 74 is located in the HP zone 62, the LP inlet 78 is located in the LP zone 64 and the outlet 76 is located in the outlet zone 66.
  • each jet pump 52 includes a nozzle assembly 80, a mixing tube 82 and a diffuser 84.
  • O-ring seals 86 are provided on the external cylindrical surface of the jet pump 52 to form a hermetic seal with the two partition walls 68, 70.
  • the jet pumps 52 may be welded permanently to the partition walls 68, 70.
  • each jet pump 52 may be provided with plugs 88 that can be screwed into the HP inlet 74 and the outlet 76 to prevent any flow of fluid, thereby isolating the jet pump 52.
  • Sealing rings 90 are provided to ensure a tight seal between the plug 88 and the end of the jet pump 52. By inserting or removing these plugs 88, the number of operational jet pumps 52 in the pump apparatus can be changed, thus allowing the pump apparatus to be adapted to different flow conditions, without changing the structure of the pump apparatus.
  • plugs 88 can be fitted to any two of the three inlets and outlet vents 74, 76, 78, or to all three vents.
  • jet pumps 52 are identical, the capacity of the pump apparatus can be adjusted by increasing or decreasing the number of isolated jet pumps.
  • jet pumps 52 with different flow capacities can be fitted to provide a wider range of flow capacity, or different types of jet pump can be used so that the pump apparatus can be adapted to different flow regimes (for example, different amounts of gas and liquid).
  • the jet pumps 52 all have identical external dimensions (even if they have different flow capacities or are of different types), so that they can be supplied as standard "off the shelf products, which can then be selected and fitted into a standard housing, according to the requirements of the application for which they are intended, including for example the flow rate, pressure and flow regime of the produced fluids.
  • plugs 88 are fitted manually, for example by screwing them into the ends of the jet pump 52, it will be necessary first to depressurise and isolate the pump apparatus, so as to provide access to the jet pumps. Although this is a somewhat time-consuming process, it is nevertheless considerably quicker and less expensive than adapting or removing and replacing a conventional jet pump.
  • a pump apparatus intended for use in this situation may therefore be provided with actuator-operated plugs for isolating individual jet pumps. These plugs may for example be hydraulically actuated.
  • Figure 7 shows such a plugging arrangement using a hydraulically-driven valve.
  • a piston 95 is provided at the HP inlet end of the jet pump unit 52.
  • the regions of the jet pump body on either side of the piston 95 are isolated by ring seals 98. These seals 98 isolate fully the small gap between the outer surface of the piston 95 and the inner surface of the jet pump 52.
  • the piston 95 can slide along the inner body of the jet pump to expose or to isolate a port 96, which comprises the HP inlet through which HP fluid enters the jet pump.
  • a spring 94 pushes the piston 95 to a position which exposes the port 96 and opens the flow passage into the jet pump.
  • hydraulic fluid is injected via a line 92 into a pressure chamber 93 between the piston 95 and a removable screwed end cap 91. This pressure pushes the piston 95 against the spring 94 and closes the port 96.
  • the multi-jet pump assembly consists of several small standardised jet pumps assembled to operate in parallel.
  • the number can be any, varying from two to several, depending on the application.
  • the system is designed so that at any time any number of jet pump units can be operational to match the operating conditions of that time. All units can be of identical external design to minimise cost, or if needed they can consist of two or more groups of similar size.
  • each jet pump is always of optimum design as it always handles the flow for which it was designed, even if the total HP or LP flow changes significantly.
  • the overall length of the unit is significantly less than that of a single jet pump performing the same duty as the combined jet pumps.
  • the total length of each jet pump is equal to a multiplier of its mixing tube and diffuser diameter. Therefore for small mixing tube diameters of the modularised jet pumps the total length is reduced significantly.
  • Typical multiplier for the length of a jet pump is 20 to 40 times the diameter of the mixing tube, depending on applications.
  • the arrangement can also be used for onshore or offshore applications with benefits such as using standard single sized units which can be manufactured in advance and used whenever needed, without having to wait for the manufacture of new internals.
  • the system therefore consists in a preferred embodiment of the following key features as shown in figures 4, 5 and 6:
  • a containment vessel 50 which houses the group of jet pump units 52;
  • the containment vessel 50 consists of a Tee section to provide the inlet point 58 for the LP flow.
  • the two other end flanged sections are allocated to HP flow inlet 54 and the common outlet point 56.;
  • the vessel is divided into three separate pressure zones 62, 64, 66 comprising the HP, LP and the discharge sections;
  • Each pressure zone 62, 64, 66 acts as a manifold to feed the HP and LP inlets 74, 78 and the discharge points 76 of the jet pumps;
  • isolation plates 68, 70 which are welded to the main containment vessel.
  • the individual jet pump units 52 pass through each isolation plate 68, 70 and are welded to the isolating plates 68, 70 or are equipped with sealing rings 86 or equivalent as they pass through each isolation plate, to ensure the operating pressure of the HP, LP and discharge manifold is maintained and each part is isolated from the neighbouring part;
  • the system is equipped with a set of two isolation valves or plugs 88 at each end of each jet pump.
  • This feature is shown in figure 6, showing the plug arrangement.
  • the plug 88 is screwed into the HP inlet 74 and the discharge end 76.
  • a piston valve similar to that shown in figure 7 can be hydraulically pushed in or out of each end of the jet pump to achieve the isolation or functioning of each jet pump without interrupting production. Only two out of the three inlet and outlet vents needs to be plugged to isolate the jet pump. If isolation plugs are used, each plug is equipped with sealing rings to plug and isolate the relevant section effectively.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
PCT/GB2012/000533 2011-06-23 2012-06-19 Pump assembly comprising a plurality of jet pumps WO2012175915A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BR112013032509A BR112013032509A2 (pt) 2011-06-23 2012-06-19 conjunto de bombas compreendendo uma carcaça e uma pluralidade de bombas a jato
GB1320575.2A GB2505586A (en) 2011-06-23 2012-06-19 Pump assembly comprising a plurality of jet pumps
US14/128,934 US20140255218A1 (en) 2011-06-23 2012-06-19 Pump assembly comprising a plurality of jet pumps
NO20131706A NO20131706A1 (no) 2011-06-23 2013-12-19 Pumpesammenstilling inneholdende et flertall jetpumper

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1110692.9A GB2492153A (en) 2011-06-23 2011-06-23 Multiple parallel jet pump apparatus
GB1110692.9 2011-06-23

Publications (1)

Publication Number Publication Date
WO2012175915A1 true WO2012175915A1 (en) 2012-12-27

Family

ID=44485069

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2012/000533 WO2012175915A1 (en) 2011-06-23 2012-06-19 Pump assembly comprising a plurality of jet pumps

Country Status (5)

Country Link
US (1) US20140255218A1 (pt)
BR (1) BR112013032509A2 (pt)
GB (2) GB2492153A (pt)
NO (1) NO20131706A1 (pt)
WO (1) WO2012175915A1 (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107023530A (zh) * 2016-02-01 2017-08-08 朱建林 一种圆管用多通道射流器
US20180038515A1 (en) * 2016-08-05 2018-02-08 Baker Hughes, A Ge Company, Llc Method and apparatus for flooding a subsea pipeline
GB201916064D0 (en) * 2019-11-05 2019-12-18 Transvac Systems Ltd Ejector device
US20220282739A1 (en) * 2021-03-05 2022-09-08 Honeywell International Inc. Mixture entrainment device
US11828223B2 (en) 2021-05-28 2023-11-28 Honeywell International Inc. Variable jet pump

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US1536180A (en) * 1922-12-27 1925-05-05 Electric Water Sterilizer & Oz Eductor
US1804569A (en) * 1929-01-26 1931-05-12 Westinghouse Electric & Mfg Co Air ejector
US6224042B1 (en) * 1997-12-15 2001-05-01 Serguei A. Popov Liquid-gas ejector
US6276903B1 (en) * 1998-01-27 2001-08-21 Evgueni D. Petroukhine Liquid-gas ejector

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US636953A (en) * 1899-09-05 1899-11-14 Watson & Mcdaniel Company Ejector.
US1071875A (en) * 1911-02-01 1913-09-02 Heinrich Buschei Gas-purifying apparatus.
US1421843A (en) * 1914-09-14 1922-07-04 Westinghouse Electric & Mfg Co Fluid-translating device
US3061179A (en) * 1960-11-08 1962-10-30 Vac U Max Suction creating apparatus
DE1503706C3 (de) * 1965-06-19 1971-09-02 Siemens Ag Einer vakuumpumpe vorschaltbare strahlsaugeraggregate
US4468172A (en) * 1983-03-08 1984-08-28 General Electric Company Jet pump plug
US5628623A (en) * 1993-02-12 1997-05-13 Skaggs; Bill D. Fluid jet ejector and ejection method
RU2142070C1 (ru) * 1998-03-02 1999-11-27 Попов Сергей Анатольевич Жидкостно-газовый эжектор
GB2447677B (en) * 2007-03-21 2011-11-16 Honeywell Normalair Garrett Jet pump apparatus
FR2929663B1 (fr) * 2008-04-03 2012-10-05 Coval Generateur de vide autoregule.

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1536180A (en) * 1922-12-27 1925-05-05 Electric Water Sterilizer & Oz Eductor
US1804569A (en) * 1929-01-26 1931-05-12 Westinghouse Electric & Mfg Co Air ejector
US6224042B1 (en) * 1997-12-15 2001-05-01 Serguei A. Popov Liquid-gas ejector
US6276903B1 (en) * 1998-01-27 2001-08-21 Evgueni D. Petroukhine Liquid-gas ejector

Also Published As

Publication number Publication date
GB201320575D0 (en) 2014-01-08
GB201110692D0 (en) 2011-08-10
US20140255218A1 (en) 2014-09-11
BR112013032509A2 (pt) 2017-03-01
GB2505586A (en) 2014-03-05
GB2492153A (en) 2012-12-26
NO20131706A1 (no) 2013-12-19

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