AU739662B2 - Three-phase rotary separator - Google Patents

Description

THREE-PHASE ROTARY SEPARATOR BACKGROUND OF THE INVENTION This invention relates generally to separation of three fluid phases--gas, oil and water, and more particularly concerns achieving such separation using rotating separator apparatus. In addition, the invention concerns methods of operating rotary separator apparatus in relation to scoop means immersed in a liquid ring on the rotary separator. Solids entrained in the flow must also be separated.

In existing non-rotary methods, a large gravity separation tank is required to be used, and only partial separation of oil and water phases is achievable. Therefore, additional treatment is required for separating those constituents. Secondary treatment methods require. expenditure of large amounts of power, as for example via high speed centrifuges.

Another advantage is the size and weight of the required vessels. For offshore oil and gas productions, the large separation vessels require large, expensive structures to support their weight.

From US-A-4 087 261 there is known a rotating separator apparatus which shows scoops fully submerged in the apparatus to remove separated liquids. As shown, the flowrate from a fully submerged scoop is fixed by the liquid velocity and the scoop inlet area. Increases in flowrate would cause the liquid entering a particular submerged scoop to overflow it and go into another scoop. Decreases in flowrate would cause the scoop to take in addition liquid from another zone.

There is need for improved means to efficiently achieve separation of the three phases--gas, oil and water; further, there is need to achieve such separation in a mixture of such fluids passed through a nozzle, as in a jet stream.

SUMMARY OF THE INVENTION The present invention seeks to provide a simple, effective method and apparatus meeting the above needs.

This is sought to be met by operating rotating separator apparatus to which fluid, including gas and liquids (as for example oil and water mixed together) is supplied in a fluid jet, as via a nozzle, the steps of the basic method including: a) separating the liquids for the gas in the stream, at a first zone within the Srotating apparatus, and 3 5 b) separating the liquids into liquids of differing density at a second zone within Jihe apparatus, P:\W PDOCS\RET spcci\7465848.doc- 14A8/IO I -2characterised by c) said separating including providing a scoop immersed in at least one of said liquids travelling relative to the scoop.

As will appear, the fluid jet has momentum which is utilised by transfer of energy from the jet to the rotating separator apparatus. Power may also be transferred from an external source to the rotating separator.

The present invention also seeks to provide method and apparatus to achieve complete separation of gas, oil, water, and solids. It operates either by the two-phase fluid energy or by a supplementary motor drive. It has a self-regulating feature to handle widely varying ratios of gas, oil and water with no external controls.

Further, the present invention concerns removal from the fluid jet of entrained solid particles, the method including providing a solids removal passage in the rotating-separator apparatus, and including separating the particles which are separated by transfer to the passage.

The present invention also includes provision at the rotating separator apparatus of a passage for receiving a liquid A of higher density, providing at the apparatus an outlet for liquid B of lesser density, the liquids A and B having a stable interface location determined by the relative locations of the outlets and passage, such that substantially complete separation of flowing liquids A and B occurs for a relatively wide range of flows. At least one of the outlets may advantageously be in the form of a scoop immersed in at least one of the liquids flowing as in a liquidous ring relative to the scoop. A movable inlet barrier may be provided in association with the scoop to block entry of gas into the scoop.

The present invention also includes supporting the barrier for movement in response to changes in force anppliedt to the brrier by at least one of the liquids flowing relative to the scoop.

The present invention also includes providing one or more of the outlets at the rotating separator apparatus to have the form of an open weir, and flowing liquid via that weir to a passage leading to a liquid nozzle, as will be described.

The present invention also seeks to provide for liquid leaving the nozzle in the form of a jet producing thrust, and including transferring the thrust to the rotating separator apparatus.

These and other features and advantages of the invention, as well as the details of an illustrative embodiment, will be more fully understood from the following specification and drawings, in which: DRAWING DESCRIPTION Fig. 1 is a sectional view, an axial radial plane, of three-phase rotary apparatus incorporating the invention; Fig. la is a view like fig. 1; Fig. 2 is a fragmentary section-showing details of a scoop having an entrained immersed in a rotating ring of liquids, and taken in a plane normal to the axis of separator rotation; Fig. 3 is a fragmentary section taken on lines 3-3 of fig. 2; Fig. 4 is a view like fig. 2 showing a modification; Fig. 5 is a view taken on lines 5-5 of fig. 4; and Fig. 6 is a fragmentary section showing an open weir outlet to a liquid nozzle.

DETAILED DESCRIPTION Fig. 1 shows a version of the three-phase rotary separator structure 32. A mixture of oil, gas and water is expanded in a nozzle 17. The resulting gas and liquid jet 1 is well collimated. The jet impinges generally tangentially onto a moving (rotating) surface 2. See in this regard the disclosure in U.S. Patent 5 385 446, incorporated herein by reference. In the case shown, the surface is solid with holes 3, to permit drainage of the liquids and solids. Surface 2 is defined by the inner side of a rotating separator annulus 2a connected as by rotor 8 and structure 31 to a rotating shaft 19 of structure 32. Shaft bearings are shown at locations 19a. The moving surface may alternatively be comprised of the separated liquid, in which case no 1;A o- 4 flf I 4 n The centrifugal force field acting on the gas and liquid jet, when it impacts the moving surface, causes an immediate radially inward separation of the gas from the liquids. The separated gas flows through gas blades 9 in the rotor 8, transferring power to the rotor and shaft 19. The gas leaves through an exit port 18. Blades 9 are spaced about the rotor axis 19b.

The oil and water, and any particulate solids, flow into the space between the outer wall 20 and the separating surface 2, in the centrifugal force field. The greater density of water causes it to acquire a radial outward velocity and separate from the oil flow 4. Separated water is indicated at 5. The separating oil and water flow axially through slots at location 8a in the rotor, toward the oil outlet 10, and toward the water outlet 13, respectively.

If the tangential velocity of the gas and liquid jet 1 impinging on the separating surface 2 is greater than the rotating surface speed, the liquids will be slowed by frictional forces transferring power to the separating surface and hence to the rotor and shaft. If the tangential velocity of the jet is lower than the desired rotating surface speed, external power must be transferred to the shaft, and hence rotor and separating surface, to drag the slower liquids up to the speed of the rotating surface. The power can be transferred, for example by a motor, or by the shaft of another rotary separator.

The solids, being heavier than the water, are thrown to the inner side of the wall 20. The solids are collected at the farthest radial position 6 of that wall, and flow at 21 with a small amount of water into a volute 22 from which they are discharged.

A barrier 12 to the balance of the water and oil flowing rightwardly forces the water to flow through structure-defined passages 23 located below (outwardly of) the water-oil interface 7, formed by the centrifugal force field.

The relative placement of the oil outlet 10 in the oil collection zone 10 O and the water outlet 13, in the water collection zone 13a beyond barrier 12 causes the oilwater interface 7a to form at a location radially outward of both the oil outlet and the water outlet, but which is radially inward from the water passages 23. This location of the rotating interface at 7a effects separation of the oil and water. Note that interface 7a intersects barrier 12, and that zones 10 Oa and 13a are at opposite axial sides of barrier 12. The interface radial location is determined by the following relation, listing dimensions as shown in fig. la: p 0 w(r 2 i-r 2 0 po(r 2 i-r.) where Pa oil density p, water density co rpm of surface 2 ri radius to oil water interface r 0 radius to oil outlet radius to water outlet The interface location is independent of the relative amounts of water and oil, so long as the pressure drop of liquid in flowing from the interface location to the outlets is small compared to the large centrifugally-induced head from the rotating liquids. The liquid outlets are typically open scoops of the type shown in figs. 2, 3, 4 and In fig. 2, a rotary separator is shown at 110 and having an annular portion 111 with a surface 11 la facing radially inwardly toward the separator axis 112 of rotation (the same as axis 19b in fig. A liquid film or layer builds up as a ring 113 on the rotating surface and is shown to have a thickness Such liquid may typically be supplied in a jet, as from a two-phase nozzle. The nozzle, jet and separator elements are schematically shown in fig. 5. See also U.S. Patent 5 385 446, incorporated herein by reference, and wherein the momentum of the jet is transferred to the separator at its inner surface 11 a, inducing rotation.

A scoop or diffuser structure is provided at 114 for removing liquid in the ring 113.

The scoop has an entrance 115 defined by radially separated inner and outer lips I115a and 115b presented toward the relatively oncoming liquid in the ring. Lip 1 5b is immersed in the liquid ring; and lip 115a is located radially inwardly of the inner surface 1 13a of the liquid ring. Ring liquid at 113b, radially inwardly of the scoop lip 115b, enters the scoop at 11 and flows via a passage 116 in the scoop toward outlet 117. The scoop is normally non-rotating, fixed, or it may rotate, but at a slower rate than the separator.

Gas that has separated from the liquid that builds up as layer 113 collects in the separator interior, as at 118. Since lip 1 15a lies inwardly of the liquid ring inner surface 113a, there is a tendency for separated gas to enter the scoop at region 120, due to the drag effect of the rotating liquid ring upon the gas adjacent the liquid surface 113a.

Barrier structure is provided, and located proximate the scoop entrance or inlet, to block gas exiting to the scoop. One such barrier structure is indicated at 121, and as having a barrier surface 12la projecting radially outwardly of the scoop inner lip 115b, toward the liquid ring, whereby liquid on the ring travels relatively past barrier surface 121a to enter the scoop at its inlet. The barrier surface has a doctor tip extent, indicated at 12 l b, controlling the radial thickness at t 2 of the liquid ring that enters the scoop. In this regard, t 2 is normally less than The doctor tin extent 121b is alsonormally of a width (parallel to axis 112) about the same as that of the scoop inlet.

The barrier surface is shown to have taper in the direction of relative travel of liquid that enters the scoop, and that taper is preferably convex, to minimize or prevent build up of liquid in a turbulent wake at the scoop entrance. Note in fig. 3 that the scoop inlet width w is of lesser extent than the liquid in the ring, ring liquid exists at widthwise opposite sides of the scoop, as at 1 13e and 113f.

Accordingly, separated gas is prevented, or substantially prevented, from entering the scoop to flow to the outlet, and an efficient gas-liquid separation is achieved.

Another aspect concerns the provision of means for effecting controllable displacement of the barrier structure toward the liquid ring, whereby the thickness t 2 of the liquid layer entering the scoop is controlled. In the fig. 2 and fig. 3 example, such barrier displacement control means is shown in the form of a spring 125, positioned to urge the barrier structure toward the liquid ring. A balance is achieved between the force of the spring acting to urge the barrier toward the liquid ring, and the force of liquid impinging on the convex surface 121 a of the barrier, to position the barrier radially as a function of separator rotary speed, liquid ring rotary speed, and liquid viscosity, whereby a controlled rate of liquid ingestion into the scoop to match liquid supply to the ring is achieved, and without air ingestion, the inlet is left open to liquid inflow, but is blocked for gas.

Guide structure is also provided for guiding such displacement of the barrier structure as it moves in direction toward and away from the liquid ring. See for example engaged relatively sliding surfaces 129 and 130 of the barrier and scoop stem 131, attached to the scoop and sliding in the bore in a sleeve 129a attached to the scoop. A stop 134 on the stem is engageable with the end 133a of the sleeve to limit radially outward movement of the barrier structure, and its doctor tip, as referred to.

Figs. 4 and 5 show use of a foil 40 or foils immersed in the liquid and angled relative to the direction of liquid ring travel, to receive liquid impingement acting to produce a force component in a radially outward (away from axis 12) direction.

That foil is connected to the barrier structure 121, as via struts 42, to exert force on the barrier acting to move it into or toward the liquid. Such force countered by the force exerted on the barrier convex surface, as referred to above, and a balance is achieved, as referred to. No spring is used in this example.

The advantage of these types of outlets for the three-phase separator are that large changes in liquid flow rate can be accommodated with only small changes in liquid height. This enables large changes in oil flow or water flow to be swallowed by the outlet without large increases in the pressure drop or location of the oil-water interface 7.

Another form of outlet is shown in fig. 6. An open outlet passage 50 is placed at the location of the desired radially inwardly facing oil level 51. The oil flows into the passage and forms a gas-oil interface 43 51. at the location where the jet flow from a liquid (oil) nozzle 44, which is produced by the centrifugally-induced head from that interface location, equals the incoming oil flow. Nozzle 44 is spaced radially outwardly from outlet passage 50, and connected thereto by a duct 54 (an open weir), which rotates with the rotor. The nozzle opening is preferably sized for the maximum possible oil flow. Flows less than that maximum cause the S RP4/iterface 43 to move more radially outward, reducing the head, and hence flow ffrm the nozzle.

A similar arrangement is shown for the water outlet 52. The principles are the same as described for the oil outlet. See water radially inwardly facing level 62, gaswater interface 63, flow 65 from liquid (water) nozzle 64, and duct 70 (an open weir).

The provision of these outlets enables additional power to be generated from the reaction forces of the water and oil jets emanating from the associated nozzles. The outlet flows can be collected in volutes similar to that previously shown in fig. la.

Either type of outlet can be used for either liquid, independently of the type of outlet chosen for the other liquid.

The reference to any prior art in this specification is not, and should not be taken as, an acknowledgement or any form of suggestion that that prior art forms part of the common general knowledge in Australia.

Claims (23)

1. In the method of operating rotating separator apparatus (32, 110), to which fluid, including gas and liquid is supplied in a fluid jet as via a nozzle (17), providing at said apparatus an outlet (13) for flowing liquid A of higher density, and providing at said apparatus an outlet (10) for flowing liquid B of lesser density, said liquids A and B having a stable interface location (7a) determined by the relative locations.of said outlets (10, 13), providing at least one of said outlets 13) in the form of a scoop (114) immersed in at least one of said liquids collecting as a centrifugally-induced liquidous ring (113) travelling relative to the scoop (114), the steps that include a) separating the liquids from the gas in said stream, at a first zone within said rotating apparatus (32, 110), b) separating the liquids into liquids of differing density at a second zone within said apparatus (32, 110), c) said separating including providing a scoop (114) immersed in at least one of said liquids travelling relative to the scoop (114), and d) providing a movable inlet barrier (121) in association with the scoop (114) to block entry of gas into the scoop (114).

2. The method of claim 1 wherein the fluid jet has momentum, and including transferring energy from the jet to said rotating apparatus (32, 110).

3. The method of claim 1 including transferring power from an external source to said rotating apparatus (32, 110).

4. The method of claim 1 wherein the fluid jet contains solid particles, and including providing a solids removal passage (22) in the rotating apparatus (32, 110), and including conducting the particles (21) which are separated by centrifugal force to said passage (22). The method of claim 1 which includes providing each of said outlets 13) in the form of a scoop immersed (114) in the liquid flowing to said outlet 13) and collecting as a centrifugally-induced liquidous ring (113) travelling relative to the scoop (114).

6. The method of claim 1 which includes providing at least one of said outlets 13) in the form of an open weir (54,

7. The method of claim 6 which includes flowing liquid via said weir (54, F-1,to a passage (50, 52) leading to a liquid nozzle (44, 64).

8. The method of claim 1 including supporting the barrier (121) for movement in response to changes in force applied to the barrier (121) by at least one of said liquids flowing relative to the scoop (114).

9. The method of claim 7 wherein liquid leaves the nozzle (44, 64) in the form of a jet-producing thrust (45, 65), and including transferring said thrust (45, 65) to said rotating separator apparatus (32, 110)- The method of claim 1 wherein blades are provided in association with said rotating operation apparatus (32, 110) and including flowing the separated gas to the blades to produce power transferred to the rotating apparatus (32, 110).

11. The method of claim 2 including providing a rotating annular surface at which the liquids are separated from the gas.

12. The method of claim 11 wherein said surface is provided by providing a separator annulus (2a) that is ported to pass liquids centrifugally away from gas.

13. The method of claim 11 wherein said surface is provided by separated liquids collecting centrifugally in a rotating ring.

14. The method of claim 1 which includes providing rotating barrier structure (12) between said outlets (10, 13), and passage means (23) for water to flow from one axial side of the barrier structure (12) to the opposite axial side of the barrier structure (12) toward said water outlet the oil collecting at said one side of the barrier structure and the water collecting at the opposite side of said barrier structure (12). The method of claim 1 including producing water and oil pressure heads in water and oil flhw via said nnozles (64, 44), and discharging water and oil injets 45) pressurized by said heads, for producing thrust transferred to said apparatus (32, 110).

16. In rotating separator apparatus (32, 110), to'which fluid, including gas and liquids is supplied in a fluid jet as via a nozzle providing at said apparatus an outlet (13) for flowing liquid A of higher density, and an outlet (10) for flowing liquid B of lesser density, said liquids A and B having a stable interface location (7a) determined by the relative locations of said outlets (10, 13), providing at least one of said outlets (10, 13) having the form of a scoop (114) immersed in at least one of said liquids collecting as a centrifugally-induced liquidous ring (113) travelling relative to the scoop (114), the combination that includes a) means for separating the liquids from the gas in said stream, at a first within said rotating apparatus (32, 110), b) means for separating the liquids into liquids of differing density at a second zone within said apparatus (32, 110), c) means for said separating including a scoop (114) immersed in at least one of said liquids travelling relative to the scoop (114), and d) a movable inlet barrier (121) in association with the scoop (114) to block entry of gas into the scoop (114).

17. The combination of claim 16 wherein the fluid jet has momentum, and including means for transferring energy from the jet to said rotating apparatus (32, 110).

18. The combination of claim 16 including means for transferring power from an external source to said rotating apparatus (32, 110).

19. The combination of claim 16 wherein the fluid jet contains solid particles, and including a solids removal passage (22) in the rotating apparatus (32, 110), and including means for conducting the particles (21) which are separated by centrifugal force to said passage (22). The combination of claim 16 which includes each of said outlets (10, 13) having the form of a scoop (114) immersed in the liquid flowing to said outlet 13) and collecting as a centrifugally-induced liquidous ring (113) travelling relative to the scoop (114).

21. The combination of claim 16 which includes at least one of said outlets 13) being in the form of an open weir (54,

22. The combination of claim 21 which includes means flowing liquid via said weir (54, 70) to a passage (50, 52) leading to a liquid nozzle (44, 64).

23. The combination of claim 16 including means supporting the barrier (121) for movement in response to changes in force applied to the barrier (121) by at least one of said liquids flowing relative to the scoop (114).

24. The combination of claim 22 wherein liquid leaves the nozzle (44, 64) in the form of a jet-producing thrust (45, 65) and including means transferring said thrust 65) to said rotating separator apparatus (32, 110).

25. The combination of claim 16 wherein blades are provided in association with said rotating operation apparatus (32, 110), and including means flowing the separated gas to the blades to provide power transferred to the rotating apparatus (32, 110). Documcnt47-13/ 081Il -11-

26. A method of operating rotating separator apparatus, substantially as herein disclosed with reference to the accompanying figures.

27. Rotating separator apparatus, substantially as herein disclosed with reference to the accompanying figures. DATED this 13 th day of August, 2001 MULTIPHASE POWER AND PROCESSING TECHNOLOGIES, LLC By Their Patent Attorneys DAVIES COLLISON CAVE