EP3801917A1 - Separateur rotodynamique pour fluide multiphasique sans moyeu central - Google Patents
Separateur rotodynamique pour fluide multiphasique sans moyeu centralInfo
- Publication number
- EP3801917A1 EP3801917A1 EP19721653.4A EP19721653A EP3801917A1 EP 3801917 A1 EP3801917 A1 EP 3801917A1 EP 19721653 A EP19721653 A EP 19721653A EP 3801917 A1 EP3801917 A1 EP 3801917A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- separator
- cylinder
- rotodynamic
- phase
- vanes
- 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- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B1/00—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles
- B04B1/04—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles with inserted separating walls
- B04B1/06—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles with inserted separating walls of cylindrical shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B1/00—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles
- B04B1/04—Centrifuges with rotary bowls provided with solid jackets for separating predominantly liquid mixtures with or without solid particles with inserted separating walls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B5/00—Other centrifuges
- B04B5/08—Centrifuges for separating predominantly gaseous mixtures
Definitions
- the present invention relates to the field of multiphase separators, allowing the separation of two phases, for example a liquid phase and a gaseous phase, of a multiphase fluid entering the separator.
- separators are especially used in petroleum applications for the recovery of hydrocarbons, and more generally in any type of application requiring the separation of two liquid / liquid phases of different densities or liquid / gas such as, for example, water treatment applications. gas.
- the separators can be used, either in so-called “bottom-well” configurations, or in so-called “underwater” configurations, or on platforms.
- bottom-well When used at the bottom of wells, their outside diameter is constrained by the environment of the well bottom, in particular by its diameter.
- the separators are generally disposed on the seabed, and are connected to conduits for the delivery of fluid from the well to the surface.
- the rotary gas separators 10 also called RGS for "Rotating Gas Separator" comprise, in a pipe 8, two series of fins or blading 3 and 4 integral with a shaft rotation 2, the rotation shaft 2 rotating about the axis xx, the axis xx corresponding to the axis of the pipe 8.
- the first series is composed of a helix 3 to put the multiphasic fluid in motion and rotate it to initiate a separation.
- the second series consists of purely radial pallets 4 which centrifuge the liquid at the pipe 8, which is fixed.
- the multiphasic fluid arrives through the inlet 1 in the separator 10 and is conveyed via the pipe 8.
- the first phase, liquid exits through the outlet 5 on the peripheral part and the second gas phase, emerges through the part 6 close to the rotation shaft 2.
- this system can induce a lower fluid pressure at the output than at the input (induced by the losses of charges).
- the present invention proposes to remedy these disadvantages. It relates to a rotodynamic separator for separating at least two phases, for example a liquid phase and a gaseous phase, from a multiphase fluid.
- This separator comprises at least one cylinder freely rotatable about the axis of the cylinder, corresponding to the axis of the separator, an axial inlet of a multiphasic fluid, an outlet of at least a first phase and an outlet of at least least a second phase.
- the output of the second phase is axial and the output of the first phase is arranged around the output of the second phase.
- the separator comprises at least one blade, disposed along the axis of the cylinder, in the direction of flow of the multiphase fluid.
- This or these blades are integral with the cylinder, so as to be rotated integrally.
- the inner diameter of the blades progressively decreases, in the fluid flow direction, so as to orient the second phase contained in the multiphasic fluid towards the central axial outlet.
- the inner diameter of the blades remains greater than the diameter of the output of the second phase so as not to hinder the output and / or induce disturbances to this flow.
- the invention relates to a rotodynamic separator for separating at least two phases from a multiphasic fluid, said rotodynamic separator comprising at least one free cylinder rotating about the axis of said cylinder, a substantially axial inlet of said multiphase fluid, an output of at least a first phase and an output of at least a second phase, said output of said at least second phase being substantially axial and at the center of said output of said at least first phase, said rotodynamic separator comprising at least one vane, each said vanes being disposed along said axis of said cylinder, in the direction of circulation of said multiphase fluid, each of said vanes being integral with said cylinder, each of said vanes being directed towards the axis of said cylinder.
- each of said vanes gradually decreases, in the portion of said separator located upstream of said outlet of said at least second phase, in the direction of circulation of said multiphasic fluid, while remaining greater than the internal diameter of said outlet. of said at least second phase.
- each of said blades is inclined relative to the radial direction, the inner radial end of each of said blades being downstream, in the direction of flow of said multiphase fluid, of the outer radial end of said blade.
- each of said vanes has an aerodynamic profile.
- said separator comprises a plurality of vanes, and for which said vanes are evenly distributed over the section of said cylinder.
- the first phase is a liquid phase and for which the second phase is a gaseous phase.
- the tangents of each of said blades at their junctions with said cylinder are inclined relative to the radial direction of said cylinder, preferably said tangents of each of said blades start from the junction of said blade and said cylinder to said axis of said cylinder and downstream in the direction of flow of said multiphase fluid.
- a central hub is disposed on the downstream part of the rotodynamic separator, in the direction of circulation of said multiphasic fluid, said central hub being fixed integrally to said cylinder by at least a second part of said vanes, said output of said at least second phase being disposed in said central hub, said second portion of said vanes extending from the outside diameter of said central hub to the inside diameter of said cylinder.
- At least one blade is positioned inside the central hub, in said output of said at least second phase.
- the rotodynamic separator comprises an electric or hydraulic machine, said electric or hydraulic machine driving a rotation shaft, said rotation shaft driving said central hub in rotation.
- the separator comprises an electric machine, the rotor of said electric machine being disposed on the outer periphery of said cylinder of said rotodynamic separator, for driving said cylinder.
- the invention also relates to the use of the rotodynamic separator according to one of the preceding characteristics for separating a multiphasic fluid in a downhole application, in an underwater application or in an onshore application for the recovery of hydrocarbons or reinjection of gas into the well.
- Figure 1 illustrates a separator according to the state of the prior art.
- FIG. 2 illustrates an embodiment of a rotodynamic separator according to the invention.
- FIG. 3a illustrates a second embodiment of a rotodynamic separator according to the invention.
- FIG. 3b illustrates a third embodiment of a rotodynamic separator.
- Figure 4 illustrates a longitudinal sectional view of the blades of an embodiment according to the invention.
- FIG. 5 illustrates a perspective view of another embodiment of the blades, according to the invention.
- Figure 6 illustrates the profile of helical vanes.
- the invention relates to a rotodynamic separator for separating at least two phases, for example a liquid phase and a gas phase of a multiphasic fluid or two liquid phases of different densities.
- a “separator” is a means for dissociating phases of a multiphase fluid.
- This rotodynamic separator hereinafter referred to as a “separator” comprises at least one free cylinder rotating about the axis of the cylinder, which corresponds to the axis of the separator, a substantially axial inlet of the multiphase fluid, an outlet of at least a first phase and an output of at least a second phase.
- rotodynamic separator refers to a separator for which the separation is made from a rotational movement, giving rise to different centrifugal effects in the phases.
- the output of the second phase is substantially axial and at the center of the output of the first phase.
- the separator also comprises at least one blade, disposed along the axis of the cylinder, in the direction of flow of the multiphase fluid. These blades are integral with the cylinder and directed towards the axis of the cylinder, starting from their junction with the cylinder.
- the inner diameter of each of the blades can gradually decrease, in the fluid flow direction while remaining greater than the internal diameter of the output of the second phase, so that this second phase can be routed to the output without disturbance.
- the separator may be free of central hub, the blades being secured to the cylinder disposed on the outer diameter of the blades. The cylinder thus surrounds the blades. This embodiment, without central hub is particularly interesting since the absence of central hub makes it possible not to restrict the fluid passage space on the one hand and not to increase the pressure drops on the other hand.
- the blades are also used to exert a centrifugal effect on the first phase (for example liquid), of greater density than the density of the second phase (for example gaseous). Therefore, the first phase is directed outwards, that is to say towards the cylinder wall, by the centrifugation induced by the blades.
- first phase for example liquid
- second phase for example gaseous
- the multiphase fluid arriving at the entrance passes through the blades.
- the second phase is progressively routed towards the center (that is to say towards the axis of the cylinder), while the first phase is oriented centrifugally outwards.
- the second phase exits through an axial outlet located in the center of the separator.
- the output of the first phase is around the exit of the second phase. It can be axial or radial. For downhole applications in particular where congestion is constrained, an axial output of the first phase is advantageous.
- the internal diameter of each of the blades may gradually decrease on the upstream portion of the separator, more particularly on the portion of the separator located upstream of the output of the second phase.
- the internal diameter of the vanes remains greater than the exit diameter of the second phase, so as not to disturb the flow in this zone.
- the inside diameter of the blading can remain constant.
- the blades being integral with the cylinder, itself free in rotation, the separator does not need a central axis to drive the rotating blades.
- the section of fluid passage in the cylinder is increased, which increases the maximum flow through the separator and reduce friction losses.
- the cylinder, the blades and the output of the second phase are coaxial.
- the first phase is a liquid phase and the second phase is a gaseous phase.
- this does not limit the invention to a separator of this type.
- the invention could also be used to separate two different density liquids. Indeed, one of the principles of operation is a centrifugal effect associated with a pressure gradient generated radially between the part comprising the blades and the part not comprising blades. It is therefore based on a difference in density between different phases contained in a fluid.
- the separator according to the invention could therefore be used to separate two phases of different densities of a multiphase fluid.
- the first phase may be a liquid phase and the second phase may be a gaseous phase.
- the separator is particularly well suited for separating a liquid and a gas.
- the blades may be inclined relative to the radial direction.
- the inner radial end of each blade can be downstream, in the direction of flow of the multiphase fluid, the outer radial end of the same vane.
- the vanes are advantageously arched to convey the gas to the center under the effect of the radial pressure gradient and centrifuge the liquid to the outer diameter.
- the blades may have an aerodynamic profile.
- an axial pressure difference can be induced in the system allowing, in addition to the separation of the liquid and gas phases, to increase the outlet pressure of the separator with respect to the inlet pressure.
- the vanes may be evenly distributed over the section of the cylinder.
- the spacing between the vanes on an orthoradial section may be regular. For example, one can have two blading at 180 ° four bladed 90 ° or six bladed 60 °. As a result, the operation of the system is improved by a good balancing of the wheel.
- the tangents of each of the blades at their junctions with the cylinder may be inclined relative to the radial direction of the cylinder.
- the tangents of each of the blades start from their junctions with the cylinder towards the axis of the cylinder and downstream, in the direction of flow of the multiphase fluid.
- the blades are inclined since their junction with the cylinder. This induces a camber of the blades as soon as they join the cylinder.
- This camber allows a better routing of the gas towards the center of the cylinder and an increase of the effect of overpressure and thus a better separation.
- the thickness of the vanes is decreasing from the junction of the vanes with the housing, inwards.
- a central hub can be used on the downstream portion of the separator in the flow direction of the multiphase fluid.
- the central hub may be fixed integrally to the cylinder by at least a portion of the blades. This portion of the blades, in direct rigid connection with the hub, is located in the downstream portion of the blades, the output of the gas phase being disposed in the central hub.
- the hub can be used to transmit rotation to the cylinder through the vanes. According to this configuration, this portion of the blades extends from the outer diameter of the central hub to the inner diameter of the cylinder.
- the central hub is hollow and can then serve as a wall for separating the liquid outlet and the gas outlet, the gas outlet being located inside the central hub, on a section which may for example be circular , or ring.
- the liquid outlet is disposed between the central hub and the cylinder. It may be annular or be constituted for example by the channels formed by the second part of the vanes, preferably uniformly distributed between the central hub or the cylinder.
- the central section for the central outlet of the gas can be provided with another series of blades, independent of the blades fixed on the cylinder.
- This second series of blades serves in particular to increase the pressure of the gas.
- the rotodynamic separator may comprise an electric or hydraulic machine, a rotation shaft, itself driving the central hub in rotation.
- the rotation shaft is coaxial with the hub, itself coaxial with the cylinder, and is disposed inside the hub.
- the rotation shaft and the hub can be integral.
- the rotodynamic separator may comprise an electric machine whose rotor is disposed on the outer periphery of the cylinder of the rotodynamic separator, to drive the cylinder.
- This configuration is particularly advantageous. Indeed, the separator no longer needs a rotation shaft to transmit the rotation to the cylinder.
- the gas outlet, integrated in the central hub is not blocked by the presence of the rotation shaft.
- the passage section of the gas outlet is thus increased, to increase the flow of fluid in the separator and can be provided with a second series of blades, allowing compression of the gas.
- the absence of a rotation shaft in the hub avoids disturbances of the gas flow, which improves the performance of system phase separations.
- the invention also relates to the use of the rotodynamic separator according to one of the preceding characteristics (or one of the combinations of the preceding features) for separating a multiphasic fluid in a downhole application, in an underwater application or in a an onshore application for the recovery of hydrocarbons or reinjection of gas into the well.
- a separator according to one of the preceding features can integrate more easily in a constrained environment such as a well bottom for example.
- these characteristics allow the separation of petroleum fluid, this fluid may in particular contain liquid or gaseous hydrocarbons, water, as well as other gases such as CO 2 or H 2 S.
- a separator according to the invention makes it possible to reduce its overall length with respect to a type device RGS, as illustrated for example in FIG. 1.
- FIG. 2 is a diagrammatic and nonlimiting illustration of an embodiment of a separator 20 according to the invention.
- This separator 20 comprises a cylinder 12, and vanes 15.
- Each vane 15 is integrally fixed to the cylinder 12, the cylinder 12 thus surrounding the vanes 15.
- This attachment may for example be obtained by welding the vanes 15 on the cylinder 12, by mass machining or by additive manufacturing.
- a radial end of the blades 15 is located at their junction with the cylinder 12.
- the second radial end is located inside the cylinder 12.
- vanes 15 are inclined towards the rear, in the direction of circulation of the fluid.
- the inner radial end of the blades 15 is located downstream of their outer radial end (also corresponding to the junction with the cylinder 12), in the longitudinal direction of the axis xx and the direction of the fluid flow.
- the blades 15 have, at least on a first portion 17, an inner radial end progressively leading the gas (represented by the small circles visible in FIG. 2) from the inlet 1 to the gas outlet 6.
- the vanes 15 may consist of a helical part whose outer diameter corresponds to that of the cylinder 12 and whose inner portion was cut by a cone from upstream to downstream, in the fluid flow direction.
- the inside diameter of the vanes 15 on at least the first portion 17 of the vanes remains always greater than the inside diameter of the gas outlet 6, corresponding for example the inner diameter of the central hub 22.
- the gas is directed correctly to the gas outlet 6 and the vanes do not disturb the flow of gas on the section of the gas outlet 6.
- the vanes 15 have a substantially helical shape around the axis xx of the cylinder 12.
- the helix is formed around the axis xx as in FIG. 6.
- the angle T corresponds to the position angle of the blade at its junction with the cylinder, in a section orthogonal to the axis xx.
- the variation of this angle corresponds to the angle G, in this way the rotational movement of the fluid is accentuated, which makes it possible to increase the centrifugal effect. allowing the separation of the liquid and the gas (or more generally, phases of different densities).
- a perspective view of these blades is shown in Figure 5.
- the vanes 15 may be evenly spaced.
- the liquid contained in the multiphase fluid at the inlet 1, for its part, is directed towards the liquid outlet 5 by a centrifugal effect induced by the vanes 15 which rotate in rotation about the axis xx of the cylinder 12.
- a rotation shaft 2 At the rear of the vanes 15, and set back from the first part where they are located, is a rotation shaft 2.
- This rotation shaft 2 allows the transmission of a torque and a rotational movement from a machine, for example, electric or hydraulic (not visible in Figure 2).
- the rotation shaft 2 drives a central hub 22 in rotation. This drive can be achieved by a rigid connection between the rotation shaft 2 and the central hub 22 but also by any means known to those skilled in the art.
- the central hub 22 is fixed integrally to the cylinder 12 by a second portion 18 of the vanes. This portion of the blades is located downstream of the first part described above. Unlike the first part, on this second part, the blades extend from the inside diameter of the cylinder to the outer diameter of the hub.
- This second part 18 of the blades serves to transmit rotation and torque to the cylinder 12. It also serves to ensure good coaxiality between the cylinder 12 and the central hub 22 for proper operation of the system.
- the cylinder 12, the central hub 22 and the rotation shaft 2 are coaxial.
- the central hub 22 and the rotation shaft 2 do not advance axially in the area where the first portion of the blades is located, the first part being constituted by the zone of the blades where the internal diameter of the blades progressively decreases.
- the central hub 22 and the rotation shaft 2 remain behind this first portion of the blades.
- no hub or central shaft closes the central passage of the fluid.
- the central hub 22 and the rotation shaft 2 do not reduce the passage section of the multiphasic fluid to the right of the first portion of the blades, and do not disturb the flow in this area. This improves the efficiency of the phase separation device.
- the rotation shaft 2 is located inside the hub 22, the rotation shaft 2 and the hub 22 being coaxial.
- the gas outlet 6 is located in a space between the central hub 22, which is hollow, and the rotation shaft 2.
- the outlet 6 is located in the annular space defined between the inner diameter of the central hub 22 and the outer diameter of the rotating shaft 2.
- the gas passage section is maximum.
- the section of the liquid outlet 5 is also preferably annular, located between the inner diameter of the cylinder 12 and the outer diameter of the central hub 22. Thus, the liquid outlet passage section 5 is maximum.
- the extension of the curve induced by the inner radial ends of the various vanes 15 is oriented substantially by the outer diameter of the outlet 6 of the gases.
- these inner radial ends form a channel driving the gas to the outlet 6 of gas.
- the outside diameter of the gas outlet 6 is in the extension of the curve generated by the inner radial ends of the vanes 15.
- FIG. 3a illustrates, in a schematic and nonlimiting manner, a second embodiment of a separator 30 according to the invention.
- the gas bubbles present in the multiphase fluid are illustrated by circles.
- the elements identical to those of Figure 2 are not described.
- this embodiment does not have a rotation shaft 2.
- the passage section of the gas outlet 6 can be cylindrical and defined by the internal diameter of the central hub 22. This mode of realization makes it possible to increase the gas flow rate at the outlet of the separator and to eliminate the disturbances of the output gas which could be induced by the presence of the rotation shaft 2.
- This embodiment is particularly advantageous for increasing the flow of gas at the outlet of the separator and the efficiency of the system.
- FIG. 3b illustrates, schematically and without limitation, a third embodiment of a separator 30 according to the invention.
- the gas bubbles present in the multiphase fluid are illustrated by circles.
- the elements identical to those of Figure 2 or Figure 3 are not described.
- a second series of blades 28, distinct from the vanes 15, is placed in the central hub 22.
- This second series of blades 28 is inclined: the inner radial end of the second series of blades 28 is located downstream, in the fluid flow direction, the outer radial end of the second vane series 28. The inclination of these blades allows compression of the fluid.
- the inner diameter of the second set of vanes 28 may be non-zero.
- the thickness of this second series of blades 28 decreases as a function of the diameter. Thus, the thickness is greatest at the junction of the second set of vanes 28 with the central hub 22 and is minimal at the inside diameter. In this way, the mechanical strength of this blading is ensured.
- Figure 4 illustrates, schematically and not limited to, blade configurations.
- the vanes 15a, 15b are aerodynamically profiled in order to orient the liquid towards the outside and the gas towards the axis xx of the cylinder 12 to separate these phases.
- the radial direction is represented by the axis rr.
- vanes 15a and 15b are inclined from their outer radial end, corresponding to their junction A with the cylinder 12. By the inclination, the inner radial end B of the vanes is located at the rear of the end outer radial axis A, in the axial direction and in the direction of the fluid flow F.
- This inclination of the blade 15a can induce an angle ⁇ between the blade 15a and the radial axis rr substantially constant on the blade 15a.
- the inclination of the blade 15a / 15b may be progressive or arranged in several zones discontinuously, for example, via a first angle b, between the blade 15b and the radial axis rr, then a second angle c between the blade 15b and the radial axis rr, as visible on the second blade 15b, in the direction of the flow F (also called the flow direction of the fluid) of FIG. 4.
- the blade 15b is composed of two zones, a first zone of constant slope b, then a second zone of constant slope c.
- Blading 15b could also be composed of several zones of constant slope or of a single zone whose slope varies gradually. In this case, the derivative of the slope is a continuous curve, without discontinuity. The absence of discontinuity makes it possible to avoid flow disturbances, which would then be synonymous with loss of efficiency of the device.
- Blades 15a and 15b have a slope a, b from their junction A
- the slope a, b in a plane defined by the radial axis and the longitudinal axis xx, at the tangent to the vane 15a, 15b, that is to say at the junction A of the vane 15a, 15b with the cylinder 12 is non-zero, the slope a, b being defined as the angle between the radial axis and the direction blading 15a, 15b.
- the tangents of the vanes 15a, 15b, at their junctions A with the cylinder 12 have a non-zero angle with the radial axis of the blade, preferably this angle is between 5 and 85 ° and preferably between 20 and 60 ° allowing better phase separation performance.
- the different vanes 15 of a separator may have slopes a, b, c which are identical or different.
Landscapes
- Centrifugal Separators (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Separating Particles In Gases By Inertia (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1854520A FR3081352B1 (fr) | 2018-05-28 | 2018-05-28 | Separateur rotodynamique pour fluide multiphasique sans moyeu central |
| PCT/EP2019/061975 WO2019228778A1 (fr) | 2018-05-28 | 2019-05-09 | Separateur rotodynamique pour fluide multiphasique sans moyeu central |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP3801917A1 true EP3801917A1 (fr) | 2021-04-14 |
Family
ID=63209522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19721653.4A Withdrawn EP3801917A1 (fr) | 2018-05-28 | 2019-05-09 | Separateur rotodynamique pour fluide multiphasique sans moyeu central |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20210213462A1 (fr) |
| EP (1) | EP3801917A1 (fr) |
| FR (1) | FR3081352B1 (fr) |
| WO (1) | WO2019228778A1 (fr) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2795635A (en) * | 1953-08-28 | 1957-06-11 | Phillips Petroleum Co | Centrifuge |
| FR1282172A (fr) * | 1960-12-09 | 1962-01-19 | Rateau Soc | Perfectionnement aux séparateurs centrifuges |
| NO157967C (no) * | 1986-01-15 | 1991-05-08 | Jacob Kalleberg | Separator for skilling av to sammenblandede vaesker med ulike egenvekter. |
| US7569094B2 (en) * | 2006-07-06 | 2009-08-04 | The United States Of America As Represented By The Secretary Of The Air Force | Method and apparatus for separating particles |
| WO2013164002A2 (fr) * | 2012-05-03 | 2013-11-07 | Eigamil Mohamed Ahmed | Traitement de fluides par passage au travers d'un ou plusieurs circuits hélicoïdaux et exposition à un champ électrique ou magnétique |
-
2018
- 2018-05-28 FR FR1854520A patent/FR3081352B1/fr not_active Expired - Fee Related
-
2019
- 2019-05-09 EP EP19721653.4A patent/EP3801917A1/fr not_active Withdrawn
- 2019-05-09 US US17/058,993 patent/US20210213462A1/en not_active Abandoned
- 2019-05-09 WO PCT/EP2019/061975 patent/WO2019228778A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019228778A1 (fr) | 2019-12-05 |
| FR3081352A1 (fr) | 2019-11-29 |
| FR3081352B1 (fr) | 2020-06-12 |
| US20210213462A1 (en) | 2021-07-15 |
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