WO2021186133A1 - Perforation means for a tank of natural gas in the liquid state - Google Patents

Perforation means for a tank of natural gas in the liquid state Download PDF

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Publication number
WO2021186133A1
WO2021186133A1 PCT/FR2021/050444 FR2021050444W WO2021186133A1 WO 2021186133 A1 WO2021186133 A1 WO 2021186133A1 FR 2021050444 W FR2021050444 W FR 2021050444W WO 2021186133 A1 WO2021186133 A1 WO 2021186133A1
Authority
WO
WIPO (PCT)
Prior art keywords
tank
perforation
perforating
tube
drum
Prior art date
Application number
PCT/FR2021/050444
Other languages
French (fr)
Other versions
WO2021186133A4 (en
Inventor
Bertrand BUGNICOURT
Emmanuel HIVERT
Aissata SOW
Sylvestre PELTIER
Laurent Spittael
Nicolas Dupont
Alexandre DIVOT
Bruno SORREGUIETA-ADER
Original Assignee
Gaztransport Et Technigaz
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 Gaztransport Et Technigaz filed Critical Gaztransport Et Technigaz
Priority to KR1020217024511A priority Critical patent/KR102586601B1/en
Priority to KR1020237033428A priority patent/KR102654638B1/en
Priority to CN202180022932.4A priority patent/CN115836177A/en
Publication of WO2021186133A1 publication Critical patent/WO2021186133A1/en
Publication of WO2021186133A4 publication Critical patent/WO2021186133A4/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D5/00Arrangements for operating and controlling machines or devices for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D5/08Means for actuating the cutting member to effect the cut
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D5/00Arrangements for operating and controlling machines or devices for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D5/08Means for actuating the cutting member to effect the cut
    • B26D5/14Crank and pin means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D1/00Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor
    • B26D1/0006Cutting members therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D5/00Arrangements for operating and controlling machines or devices for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D5/08Means for actuating the cutting member to effect the cut
    • B26D5/10Hand or foot actuated means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/0006Means for guiding the cutter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/02Perforating by punching, e.g. with relatively-reciprocating punch and bed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26FPERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
    • B26F1/00Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
    • B26F1/24Perforating by needles or pins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B25/00Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby
    • B63B25/02Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods
    • B63B25/08Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid
    • B63B25/12Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed
    • B63B25/16Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed heat-insulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D1/00Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor
    • B26D1/0006Cutting members therefor
    • B26D2001/002Materials or surface treatments therefor, e.g. composite materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D1/00Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor
    • B26D1/0006Cutting members therefor
    • B26D2001/0053Cutting members therefor having a special cutting edge section or blade section
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D1/00Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor
    • B26D1/0006Cutting members therefor
    • B26D2001/006Cutting members therefor the cutting blade having a special shape, e.g. a special outline, serrations

Definitions

  • the present invention relates to the field of natural gas tanks in the liquid state in maritime transport. More particularly, the invention refers to the devices prior to the repair of such tanks used in the event of a leak of natural gas in the liquid state from such a tank.
  • Natural gas in the liquid state is transported by sea in sealed and thermally insulating storage tanks on transport ships. Natural gas is kept in liquid form to increase the amount of liquid natural gas transported per tank, the volume of one liter of natural gas in liquid form being much less than the volume of one liter of natural gas in gaseous form. These tanks maintain the liquid natural gas at very low temperature, and more precisely at a temperature below -163 ° C, temperature at which the natural gas is in liquid form at atmospheric pressure.
  • Such liquid natural gas tanks can also be used as a fuel tank by some ships. In other words, ships load and store liquid natural gas in their tanks and then use the liquid natural gas as fuel for the ship's engine (s).
  • these tanks can be used for the terrestrial storage of liquid natural gas such as for example to recover the liquid natural gas on the docks during the unloading of the liquid natural gas transported by tanks arranged on the ships.
  • Liquid natural gas tanks generally have a parallelepipedal shape, the walls of which are mainly composed of a primary space and a secondary space, each of the spaces comprising a thermally insulating layer and a sealed layer, respectively ensuring the maintenance of the liquid natural gas. at -163 ° C and the capacity of liquid natural gas in the tank.
  • a liquid natural gas leak can occur at the sealed layer of the primary space, for example due to wear or due to improper assembly of the gasket.
  • the waterproof layer of the primary space The liquid natural gas contained in the tank then infiltrates into the primary space and invades the thermally insulating layer of the primary space. The liquid natural gas then spreads throughout the thermally insulating layer of the primary space.
  • the tank containing liquid natural gas To access and repair the leak in the waterproof layer, the tank containing liquid natural gas must be emptied.
  • the liquid natural gas is thus evacuated from the tank, for example by known means which aim to discharge the liquid natural gas out of the damaged tank.
  • a significant amount of liquid natural gas may remain in the thermally insulating layer of the primary space. Since the internal volume of the vessel is empty, there is no longer a pressure balance between the thermally insulating layer of the primary space and the internal volume. The weight of this LNG in the thermally insulating layer of the primary space pushes the sealed layer towards the internal volume of the vessel, which can damage the vessel.
  • the nitrogen injected into the tank and at a temperature higher than the temperature of the liquid natural gas initially contained in the tank fills the internal volume of the latter, thus increasing the temperature within the internal volume of the tank.
  • This hotter nitrogen increases the temperature of the walls of the tank.
  • the temperature of the liquid natural gas infiltrated into the walls of the vessel then increases, causing the state of the natural gas to change from a liquid state to a gaseous state.
  • This vaporization of natural gas then causes an increase in the pressure on the walls of the vessel by exerting a force deforming the thermally insulating layer from the primary space towards the internal volume of the vessel.
  • the vaporization of the latter at least partially damages the vessel walls, in particular by tearing off the sealed layer constituting the vessel wall.
  • the present invention proposes a perforation device making it possible to produce an orifice of sufficient diameter in the sealed layer of the primary space to allow the natural gas infiltrated into the thermally insulating layer to reach the internal volume of the tank very quickly. , and this while avoiding increasing the pressure exerted on the wall or walls of this tank.
  • the object of the present invention is therefore to facilitate the evacuation of the liquid natural gas infiltrated into the thermally insulating layer of the primary space.
  • the main object of the present invention is a perforation device for a sealed and thermally insulating tank configured to contain a fluid, characterized in that the perforation device comprises an actuating means and a perforation member of the tank, the actuating means being configured to generate movement of the perforating member.
  • the perforator is configured to perforate the vessel, the actuator being adapted to allow or block movement of the perforator.
  • the actuating means comprises at least a fixed part and a movable part. The fixed part of the actuating means allowing the perforation device to be held in position in space, by fixing it to another object, for example.
  • the mobile part helps set the perforating member in motion, the latter performing the action of perforating the tank.
  • the vessel is configured to contain a fluid, advantageously liquid natural gas (LNG), at a temperature of around -163 ° C at atmospheric pressure.
  • LNG liquid natural gas
  • the tank is thus thermally insulated, maintaining a cryogenic temperature being essential to maintain the fluid in the liquid state.
  • the tank is sealed, preventing the leak and / or loss of the fluid contained in the tank.
  • the tank is delimited in space by a plurality of walls. These walls generally take the form of a rectangular parallelepiped.
  • the perforation device makes it possible to partially perforate at least one of the walls of the plurality of walls of the vessel, advantageously the bottom wall of the vessel, and thus produces a sufficiently large section hole to allow the return of the infiltrated natural gas. in the thickness of the walls towards the inside of the tank.
  • the actuating means comprises at least one frame, a drum and a cable connecting the perforation member to the drum, the drum being configured to be rotated about an axis of rotation. and driving the winding or unwinding of the cable around the drum.
  • the frame houses the drum and at least part of the cable.
  • the frame is an element of the fixed part of the actuating means, the drum and the cable being for their part elements of the movable part of the actuating means.
  • the drum is advantageously cylindrical in shape and movable in rotation about an axis of rotation.
  • the means for actuating the perforating member also includes a crank for manually driving the rotating drum.
  • the cable comprises a first end integral with the drum and a second end integral with the perforation member.
  • the cable is made of metallic or synthetic material.
  • the cable is made partly of a synthetic material and partly of a metallic material.
  • the perforating member comprises at least one perforating head and a body, each extending longitudinally one after the other.
  • the perforation member includes a first portion consisting of the body by which the perforation member is integral with the cable and a second portion consisting of the perforation head configured to perform the perforation action.
  • the body is an element here ensuring the connection between the cable and the perforation head, the body not directly participating in the perforation of a wall of the tank.
  • the body imparts inertia through its mass which allows the perforation member to fulfill its function of breaking through the primary sealed layer of the tank.
  • the perforation head is a cylinder, one of the ends of which is bevelled, so as to form a perforation point.
  • the perforation head is the element of the perforation member performing the action of perforating the wall of the tank.
  • the perforation head longitudinally extends the body of the perforation member.
  • the body generally takes the form of a cylinder, the perforation head axially extending the cylinder forming the body at one of its ends.
  • the body has a first longitudinal end integral with the perforation head and a second longitudinal end integral with the cable.
  • the body extends between a first longitudinal end and a second longitudinal end, the body being integral with the perforation head at its first longitudinal end and integral with the cable at its second longitudinal end.
  • the body is integral on the one hand with the cable and on the other hand with the punch head, so that the punch head is opposite the cable with respect to the body.
  • the body includes a plurality of wings and a shaft from which the plurality of wings emerge radially.
  • the shaft of the body generally takes the form of a cylinder bounded by the first and second longitudinal ends from which the plurality of wings emerge radially. It is understood that the wings each emerge in a plane in which is inscribed an axis passing through the center of the cylinder and through the two longitudinal ends of the body.
  • the wings are flat sides of generally rectangular shape.
  • the body includes at least three wings distributed angularly evenly around the shaft of the body. Whether the plurality of wings include three or more wings, the angular sector separating two neighboring wings, that is to say two wings separated by a space not comprising a wing, is constant regardless of the number of wings. .
  • the plurality of wings extend in a star shape in a plane perpendicular to the main axis of extension of the piercing member, the center of which would be represented by the shaft of the body and of which each branch of the The star would be materialized by each wing of the plurality of wings.
  • At least one wing of the plurality of wings comprises a free end defining at least in part a circumference of the body and having a coating which promotes sliding of the body.
  • Each wing of the plurality of wings has three free ends, a first and a second free end extending from the shaft of the body outwardly of the perforating member and a third free end extending parallel to the body shaft. body shaft between the other two ends.
  • each of the plurality of wings helps define a circumference of the body, the third ends being the most radially outwardly projecting elements of the body.
  • Each of the third ends of the plurality of wings includes a coating to help decrease the frictional forces applied between the third ends of the plurality of wings and an outer member, such as a metal tube constituting the vessel.
  • the coating can, according to a nonlimiting example, be made of synthetic material such as for example high density polyethylene (PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. This type of coating makes it possible to reduce the frictional forces between the third ends of the plurality of wings and a metal element, for example.
  • the body carries a disc at its second longitudinal end.
  • the disc is thus integral with the body at the level of the second longitudinal end of the body.
  • the disc extends primarily in a plane perpendicular to the longitudinal axis of the shaft, this axis also passing through a center of the disc.
  • the function of the disc is to keep the cable above the perforation member, especially when the latter is installed in a tube. In this way, the cable does not come between the perforator and the tube.
  • the disc has at least one through opening.
  • a through opening is understood to mean an opening opening out on either side of the disc, a fluid thus being able to circulate through the disc by circulating through the through opening.
  • the through opening can be closed on its periphery and formed an orifice crossing.
  • the through opening can also be opened on the outer circumference of the disc and formed a through groove.
  • the disc can include a plurality of through openings.
  • the through opening or the plurality of through openings are specially sized so as not to slow down the fall of the piercing member during its release.
  • the tube may contain fluid, and the presence of a hole in the disc thus allows fluid to flow through the disc without slowing down the fall of the perforator.
  • the disc has at least one through groove allowing the passage of the cable.
  • the through groove extends from a periphery of the disc and towards the center of it.
  • the through groove allows mounting of the disc on the perforating member once the latter is linked to the cable connecting the body to the drum. Indeed, when mounting the disc on the perforating member, the disc is mounted on the body by inserting the cable through the groove, from the periphery of the disc to the center thereof.
  • the through groove of the disc facilitates the mounting of the disc on the body since the cable may have been previously attached to the body.
  • the disc is at least partly made of material which promotes the sliding of the disc.
  • the disc is at least partly made of synthetic material, such as for example high density polyethylene (PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. It will be understood that the disc can be brought into contact with a surface at the level of its periphery, the material favoring the sliding of the disc being on this surface.
  • PE-HD high density polyethylene
  • PTFE polytetrafluoroethylene
  • the disc is of disc slip material, but the disc assembly may be of disc slip material without departing from the scope of the invention.
  • the disc can also be made of metallic material and be covered at least on its periphery by a synthetic material, such as those described above.
  • the disc has a diameter less than or equal to a diameter in which the free ends of the plurality of wings fit.
  • the actuating means comprises a means for blocking the rotation of the drum, the blocking means being configured to release the perforation member and obtain its fall.
  • the drum has at least one opening configured to accommodate the means for blocking the rotation of the drum.
  • the means for blocking the rotation of the drum comprises at least one rod, the rod having a rectilinear portion surrounded at least in part by a sleeve made of material favoring the extraction of the blocking means from the opening of the drum, such as polyethylene high density (PE-HD) or polytetrafluoroethylene (PTFE), otherwise known as Teflon.
  • PE-HD polyethylene high density
  • PTFE polytetrafluoroethylene
  • the subject of the invention is also a sealed and thermally insulating tank configured to contain a fluid, the tank comprising a plurality of walls, characterized in that the tank comprises a tube passing through at least one of the walls of the tank and s' extending between a first end formed inside the tank and a second end formed outside the tank, the tank comprising a perforating device according to any one of the preceding characteristics.
  • the vessel is capable of storing a fluid, the plurality of vessel walls providing sealing and thermal insulation of said vessel.
  • the tank also includes a perforation device comprising at least one of the features described above. It is understood here that the tank and the perforating device are two separate objects which can cooperate with each other.
  • the tank is thus delimited in space by the plurality of walls, the plurality of walls advantageously taking a parallelepipedal shape.
  • the tube passes through one of the walls of the plurality of walls of the tank, advantageously a ceiling, having a first end opening out inside the tank and a second end. end opening to the outside of the tank.
  • the end opening inside the tank is close to a bottom wall of the tank.
  • the perforation device is installed at the end of the tube opening out to the outside of the tank, so that the perforating member can be in motion between the first and second ends of the tube, or even up to the wall. bottom of the tank.
  • the perforating member is disposed in the tube, the drum winding the cable to hoist the perforating member.
  • the perforation member can be partly set in motion in the tube by virtue of the rotation of the drum, the direction of rotation of the drum winding or unwinding the cable around the drum, which has the consequence of bringing together or of move the perforation member of the drum away from the bottom wall of the tank.
  • the perforator and the tube are configured so that the perforator slides in the tube.
  • the perforator thus has a section smaller than the section of the tube, in order to avoid jamming the perforator in the tube.
  • the circumference in which the free ends of the plurality of wings are at least partially inscribed is necessarily smaller than the internal section of the tube.
  • each wall of the plurality of walls comprises successively in the direction of the thickness from the outside towards the inside of the tank, a secondary thermal insulation barrier, a membrane of secondary waterproofing, a primary thermal insulation barrier and a primary waterproofing membrane and intended to be in contact with the fluid contained in the tank, the primary waterproofing membrane having a perforation zone arranged opposite the end of the tube opening inside the tank.
  • the secondary thermal insulation barrier and the secondary waterproofing membrane form a secondary space of the vessel, while the primary thermal insulation barrier and the primary waterproofing membrane form a primary space of the vessel. It is also understood that the secondary waterproofing membrane is carried by the secondary thermal insulation barrier while being in contact with the primary thermal insulation barrier.
  • Thermal insulation barriers help maintain the temperature of the fluid stored in the tank by limiting heat exchange between the environment outside the tank and the inside of the tank.
  • the sealing membranes prevent any leakage of fluid to the outside of the tank.
  • the perforation zone is characterized by a thinning of the primary waterproofing membrane facilitating the perforation of the latter by the perforation member.
  • the tube is positioned so that the end opening inside the tank is facing the perforation area.
  • the primary waterproofing membrane forms a stud comprising at least one flat area at the level of the perforation area.
  • the stud allows the perforation area to be brought closer to the end opening inside the tank, reducing the risk that the perforator will puncture the secondary waterproofing membrane, after having perforated the primary waterproofing membrane.
  • the perforation member perforates the flat zone of the stud, the latter advantageously facing the end opening inside the vessel of the tube.
  • the length of the perforation head following the direction of movement of the perforator is less than the thickness of the primary insulating barrier or else the thickness corresponding to the sum of the thickness of the primary insulating barrier and the height of the stud.
  • the invention further relates to a vessel comprising a tank according to any one of the preceding characteristics.
  • the vessel comprises the vessel capable of storing a fluid, the plurality of vessel walls ensuring the sealing and thermal insulation of said vessel.
  • the vessel also includes a perforation device comprising at least one of the features described above.
  • the subject of the invention is also a method for perforating a tank fitted to a ship according to any one of the preceding characteristics, characterized in that a first step consists in installing the perforating device at the level of the second end.
  • the first step is to position the actuating means of the piercing device at the second end of the tube, the piercing member being installed in the tube also at the second end of the tube.
  • a second step consists in sliding the perforating member in the tube to bring it against a bottom wall of the tank.
  • the second step consists in bringing, that is to say lowering in a controlled manner, the perforating member in the tube against a bottom wall of the tank. To do this, the perforator slides in the tube.
  • a third step consists in positioning the perforation member in the tube at a release height, then in blocking a constituent drum of the perforation device once the perforation member is positioned at said height. release.
  • the user positions the perforator at a certain height, such as three meters, and then blocks the rotation of the drum to accommodate the perforator at that height.
  • the perforation member is positioned on the bottom wall of the tank so as to take a reference. This position is then referred to as the measurement start point and acts as the starting reference for the release height.
  • a fourth step consists in releasing the perforation member.
  • the perforation member accumulates kinetic energy which it will transmit in the form of mechanical energy at the time of its impact on the perforation zone.
  • the height is set so that the perforator can accumulate sufficient kinetic energy to perforate the primary waterproofing membrane.
  • the second step, the third step, the fourth step are repeated until the primary waterproofing membrane is perforated.
  • a fourth step consists of hoisting the perforating member into the tube.
  • FIG. 1 is a sectional diagram of a tank equipped with a perforation device according to the invention
  • FIG. 2 is a cross section of a means for actuating the perforating device according to Figure 1;
  • FIG. 3 is a perspective view of the perforating member of the perforating device according to Figure 1;
  • FIG. 4 is a perspective view of a constituent locking means of the actuating means of the perforation device.
  • the characteristics, variants and the different embodiments of the invention can be associated with each other, in various combinations, as long as they are not incompatible or exclusive with respect to each other. It is in particular possible to imagine variants of the invention comprising only a selection of characteristics described below in isolation from the other characteristics described, if this selection of characteristics is sufficient to confer a technical advantage and / or to differentiate the invention. compared to the state of the prior art.
  • FIG. 1 a sealed and thermally insulating tank 2 delimited in space by a plurality of walls 4, the tank 2 generally taking the form of a rectangular parallelepiped of which only four of its walls are illustrated. here.
  • the tank 2 is configured to contain and / or store a fluid, and more particularly a cryogenic liquid, such as for example liquid natural gas or liquefied petroleum gas.
  • a cryogenic liquid such as for example liquid natural gas or liquefied petroleum gas.
  • this type of tank 2 is used in maritime transport, as tank for transporting liquid natural gas, or as a fuel tank for a ship.
  • this tank 2 can also be used for onshore storage of natural gas.
  • Natural gas is denser in liquid form than in gaseous form, so the storage of natural gas is quantitatively more important when natural gas is in liquid form. Natural gas is in liquid form at atmospheric pressure at a temperature of -
  • Vessel 2 is configured to maintain liquid natural gas at a temperature of no more than -163 ° C.
  • each wall of the plurality of walls 4 of the tank 2 comprises successively in the direction of the thickness from the outside to the inside of the tank 2, a secondary space 16 and a primary space 14 sealed and independent l 'from each other.
  • the secondary space comprises a secondary thermal insulation barrier 6 and a secondary waterproofing membrane 8 carried by the secondary thermal insulation barrier 6.
  • the primary space comprises a primary thermal insulation barrier 10 resting against the membrane d. secondary sealing 8 and a primary sealing membrane 12 carried by the primary thermal insulation barrier 10. This primary sealing membrane 12 is intended to be in contact with the fluid contained in the tank 2.
  • the secondary thermal insulation barrier 6 is in contact with the external environment of the tank 2, in particular with a support structure.
  • the secondary thermal insulation barrier 6 is for example in contact with an internal hull of the ship.
  • the secondary thermal insulation barrier 6 thus has an external face 18, turned towards the external environment of the tank 2.
  • the secondary sealing membrane 8 is for its part in contact on the one hand with the thermal insulation barrier.
  • secondary 6 and on the other hand with the primary thermal insulation barrier 10 which carries the primary waterproofing membrane 12.
  • the thermal insulation barriers 6, 10 participate in maintaining the temperature inside the tank 2 while that the waterproofing membranes 8, 12 form an impermeable layer to the fluids that the tank 2 could contain.
  • the tank 2 comprises a perforation device 32 comprising at least one actuating means 34 and a perforating member 36 of the vessel 2, the actuating means 34 being configured to set the actuating member in motion. perforation 36. This is how the actuating means 34 can hoist the perforation member 36, or even authorize its release.
  • the perforation device 32 is configured to pierce the primary waterproofing membrane 12 and form an orifice connecting the internal volume of the primary thermal insulation barrier 10 to an internal volume 15 of the tank 2, in order to be able to rapidly evacuate the fluid. infiltrated into the primary space 14 of the plurality of walls 4, during the unloading of the fluid contained in the tank 2, without causing the destruction of the plurality of walls 4 of the tank 2.
  • the tank 2 comprises at least one tube 38 passing through at least one of the walls of the tank 2, this wall also being referred to in the remainder of the description by the terms "tank ceiling 40".
  • the tube 38 extends longitudinally between a first end 42 opening into the internal volume 15 of the tank 2 and a second end 44 opening out to the outside of the tank 2, the tube 38 extending substantially along an axis vertical A between these two ends.
  • the terms “inner end 42” will be used to also refer to the first end 42 of the tube 38 which extends inside the tank 2, these two expressions referring to the same object.
  • the terms “outer end 44” will be used to refer to the second end 44 of the tube 38 which is disposed outside the vessel 2, these two expressions thus referring to the same object.
  • the tube 38 thus comprises two portions, an outer portion 46 which extends between the outer end 44 of the tube 38 and the tank ceiling 40, and an inner portion 48 which extends between the inner end 42 of the tube 38. and the tank ceiling 40.
  • the inner end 42 of the tube 38 is close to a wall opposite the tank ceiling 40 with respect to inside the tank 2, the opposite wall being referred to in the remainder of the description as "tank bottom 50".
  • the internal portion 48 of the tube 38 extends from the top of the tank 40 through the tube 38 towards the bottom of the tank 50, without however touching the latter.
  • the tube 38 may include, at the level of the outer portion 46, an inlet 52 of a device for measuring the level of fluid contained by the tank 2, the measuring device not being shown in the figures.
  • the tube 38 can therefore adapt a function of measuring the level of fluid in the tank, in addition to the function that it fulfills with regard to the perforation device 32 according to the invention.
  • the inlet 52 is separate from the outer end 44 of the tube 38.
  • a tube 38 as described above having an inlet 52 of the measuring device positioned at the outer end 44 of the tube 38 does not. would not be outside the scope of the invention.
  • the tube 38 is hollow between the outer end 44 and the inner end 42.
  • the tube 38 has a recess 54 delimited by an inner face 33 of the tube 38 extending between each of its ends 42, 44, the recess 54 being terminated by an external mouth 56, at the level of the external end 44 of the tube 38, and by an internal mouth 58, at the level of the internal end 42 of the tube 38.
  • the tube 38 is at least partially immersed in the fluid, the latter at least partially filling the recess 54 of the internal portion 48 of the tube 38.
  • the device measuring device can be positioned in the tube 38 at the level of the external portion 46 of the latter and reach the inside of the tank 2 to measure the level of fluid present in the tube 38, this level being assimilated to a quantity of fluid contained in the tank 2.
  • the interior mouth 58 of the tube 38 is opposite at least part of the bottom of the tank 50. More particularly, the interior mouth 58 is opposite a perforation zone 60 of the positioned on the bottom of the tank 50.
  • the perforation zone 60 is defined as such because the primary waterproofing membrane 12 is of a thickness less than or equal to the level of this zone compared to the rest of the tank bottom 50, the thickness of the primary waterproofing membrane 12 being measured in a direction perpendicular to a major extension plane of the primary waterproofing membrane 12.
  • the primary waterproofing membrane 12 can thus be perforated more easily by the perforation device 32.
  • the perforation of the primary waterproofing membrane 12 must not, however, affect the secondary space 16, the perforation member 36 thus not having to reach the secondary waterproofing membrane 8.
  • the perforation zone 60 takes the form of a stud 62 which emerges from the primary waterproofing membrane 12 and which comprises a flat zone 64.
  • the stud 62 extends towards the internal volume 15 of the tank 2 of so that the flat zone 64 is opposite the interior mouth 58 of the tube 38.
  • the perforation member 36 perforates the primary sealing membrane 12 at the level of the flat zone 64 without reaching the sealing membrane secondary 8.
  • the tube comprises a means 55 for stopping the descent of the perforating member 36 at the level of the inner mouth 58 of the tube.
  • This stop means takes, for example, the form of a welded disc extending mainly in a plane perpendicular to the vertical axis A.
  • the disc comprises an advantageously circular hole configured so that a part of the member of perforation reaches the primary waterproofing membrane 12 without the perforation member 36 completely coming out of the tube 38.
  • the tube 38 carries the perforation device 32 disposed at the outer end 44 of this tube 38.
  • the perforating device 32 comprises the actuating means 34 and the perforating member 36 of the tank 2, the actuating means 34 being configured to generate a movement of the perforating member 36.
  • the actuating means 34 allows thus to set in motion or to immobilize the perforating member 36. In other words, the movement of the perforating member 36 is placed under the control of the actuating means 34.
  • the actuating means 34 comprises at least a frame 66, a drum 68 and a cable 70 connecting the perforating member 36 to the drum 68.
  • the drum 68 is configured to be rotated about an axis of rotation B on all the figures. The rotation of the drum 68 around the axis of rotation B causes the winding or unwinding of the cable 70 around the drum 68.
  • the drum 68 is rotated here manually, in particular by means of a crank 72.
  • the actuating means 34 of the perforating member 36 comprises a manual system for rotating the drum 68, this manual system comprising at least the crank 72.
  • actuation 34 of the perforation device 32 can alternatively be motorized or even automated without thereby departing from the scope of the invention.
  • the crank 72 extends along a transverse axis C perpendicular to the vertical axis A between the handle 74 and the inner end 76 of the crank 72.
  • the handle 74 of the crank 72 allows the user to put in movement the actuating means 34 of the perforating device 32, in particular by rotating the crank 72 around the transverse axis C.
  • the inner end 76 of the crank 72 comprises a toothed wheel 78 of the drum 68, and is held in place. position by a first rotation bearing 80 of the frame 66.
  • the crank 72 is also supported in addition to the first rotation bearing 80 by a second rotation bearing 82 of the frame 66, this second rotation bearing 82 being in contact with the crank 72 between the handle 74 and the inner end 76 of the crank 72.
  • the drum 68 of the actuating means 34 comprises an element driven 84 in rotation by the toothed wheel 78 of the crank 72, the driven element 84 being for example a pinion.
  • the driven element 84 is configured to be able to be rotated about the axis of rotation B of the drum 68.
  • the toothed wheel 78 of the crank 72 rotates around the axis of rotation B the driven element 84 of the drum 68 and the drum 68.
  • the direction rotation of the crank 72 around the transverse axis C influences the direction of rotation of the drum 68.
  • the drum 68 comprises in addition to the driven element 84 a shaft 86 extending between a first side disc 85 and a second side disc 87, the side discs 85, 87 being of greater diameter than that of the shaft 86.
  • the side discs 85, 87 are larger in diameter than that of the shaft 86.
  • side discs 85, 87 being symmetrical to each other with respect to the shaft 86, a characteristic for one of the side discs 85, 87 can be applied to the other side disc 85, 87.
  • the center of the drum 68, the center of the shaft 86, the center of the side discs 85, 87 and the axis of rotation B are coincident.
  • the shaft 86 of the drum 68 secures the drum 68 to the frame 66, while allowing the rotation of the drum 68 around the axis of rotation B.
  • the cable 70 winds around the shaft 86 of the drum 68 between the side discs 85, 87, the latter guiding the cable 70 as it is wound up or unwound from the drum.
  • the first side disc 85 like the second side disc 87 has at least one positioning hole 88.
  • the positioning hole 88 is positioned here between the center of the first side disc 85 and a peripheral edge 90 of the first side disc 85, the positioning orifice 88 generally taking the form of an oblong hole, the largest dimension of which extends in a radial direction of the drum. As illustrated in FIG.
  • the first lateral disc 85 comprises a plurality of positioning orifices 88, each of the orifices 88 being formed through the first lateral disc 85 of the drum 68 and distributed angularly around the axis of rotation. B of drum 68.
  • the drum 68 comprises at least one advantageously colored notch 160 on one of the peripheral edges 90 of one of the lateral discs 85, 87, the notch 160 being designed to be at least partially visible by a user of the perforating device 32.
  • the drum 68 includes a notch 160 on each side disc 85, 87 of the drum 68 so that the user can locate or count the revolutions of the drum while being disposed on either side.
  • the actuating means 34 also comprises a means 92 for blocking the rotation of the drum 68, the blocking means 92 being configured to block or release the setting. movement of the perforating member 36. More particularly, the blocking means 92 cooperates with the positioning orifice 88 to block the rotation of the drum 68 around the axis of rotation B, the blocking means 92 extending through example at least partly in the positioning hole 88.
  • the locking means 92 comprises an advantageously rectangular handle 94 and a rod 96 extending from the handle 94 towards an insertion end 98 of the locking means 92 in a positioning hole 88. of the drum 68.
  • the handle 94 is an area through which the user takes hold of the locking means 92, the rod 96 being for its part intended to be housed in the positioning orifice 88. Indeed, a portion of the rod 96 extending from the insertion end 98 towards the handle 94 fits in the positioning hole 88 of the drum 68, then blocking the rotation of the drum 68 about the axis of rotation B.
  • the locking means 92 is manually withdrawn from the drum 68.
  • the locking means 92 comprises a sleeve 100 s' extending from the insertion end 98 towards the handle 94, promoting the sliding of the rod 96 in the positioning hole 88, the sleeve 100 being made at least in part of a synthetic material such as high density polyethylene ( PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. This material has the characteristic of reducing the frictional forces between the locking means 92 and the drum 68.
  • PE-HD high density polyethylene
  • PTFE polytetrafluoroethylene
  • the presence of the sleeve 100 around the rod 96 at the level of the insertion end 98 facilitates the extraction of the locking means.
  • 92 of the positioning orifice 88 of the drum 68 Taking into account the necessarily great weight of the perforating member so that it performs its mission in a liquid environment, such a sleeve 100 reduces the effort required to extract the locking means. 92 of the positioning hole 88.
  • the drum 68 is integral with the cable 70, the drum 68 causing during its rotation around the axis of rotation B the winding or unwinding of the cable 70 around the drum 68.
  • the locking means 92 is housed in the orifice of positioning 88, the winding or unwinding of the cable 70 cannot then occur.
  • the cable 70 of the actuating means 34 comprises a first end 102 integral with the drum 68 and a second end 104 integral with the perforating member 36.
  • the first end 102 of the cable 70 is integral with the drum 68 at the level of the shaft 86 of the drum 68.
  • the actuating means 34 optionally comprises a guide element 112 of the cable 70, optimizing the winding or unwinding of the cable 70 around the drum 68.
  • the actuating means 34 optionally comprises a return roller 114, advantageously a shaft, around which the cable 70 can slide.
  • the frame 66 of the actuating means 34 comprises a plurality of sides, of which a first side 115 is in particular visible in FIG. 2, and a fixing flange 118.
  • the fixing flange 118 of the frame 66 extends mainly in a plane. substantially perpendicular to the vertical axis A.
  • the plurality of sides of the frame 66 and the fixing flange 118 thus delimits a space 116 in which the drum 68 and the cable 70 are housed in particular at least partially.
  • the space 116 of the frame 66 is in communication with the external environment of the frame 66 at the level of the fixing flange 118, allowing at least part of the cable 70 to be outside the frame 66.
  • first end 102 of the cable 70 connected the drum 68 is positioned inside the frame 66 in the space 116 and the second end 104 of the cable 70 is positioned outside the frame 66, the cable 70 partly passing through the space 116 of the frame 66.
  • the second end 104 of the cable 70 is integral with the perforation 36.
  • the fixing flange 118 of the frame 66 is intended to be in contact with the outer end 44 of the tube 38.
  • the fixing flange 118 of the frame 66 is positioned opposite a fixing flange of the outer cover 56. of the tube 38, the fixing flange 118 of the frame 66 and the fixing flange 120 of the tube 38 being intended to cooperate with each other in order to make the frame 66 integral with the tube 38.
  • This assembly secures the fixing device. perforation 32 on the tube 38.
  • This assembly also provides a seal between the fixing flange 118 of the frame 66 and the fixing flange 120 of the tube 38.
  • the frame 66 is mounted on the tube 38 at the level of the outer end 44 of the tube 38, at least part of the cable 70 and the perforating member 36 is positioned in the hollow part 54 of the tube 38, this part of the cable 70 and the perforating member 36 aligning substantially along the vertical axis A, the pivot member 114 ensuring the positioning of the perforating member 36 along this axis, as illustrated in the figure 2.
  • the perforating member 36 disposed in the tube 38 is retained in suspension at the level of the second end 104 of the cable 70.
  • the rotation of the drum 68 causing the winding or unwinding of the cable 70 around. of the drum 68, also causes the approximation or removal of the perforating member 36 from the outer end 44 and / or the inner end 42 of the tube 38.
  • the body 124 comprises a shaft 128 delimited longitudinally by the first longitudinal end 126 and by the second longitudinal end 129 of the body 124, extending along the vertical axis A.
  • the shaft 128 here generally takes the form of a cylinder whose center coincides with the vertical axis A. Moreover, it is more particularly the shaft 128 of the body 124 which, at each of its ends, is secured to the cable 70 and to the perforation head 122.
  • the shaft 128 includes a groove 130 extending from the periphery of the shaft 128 to the center of the cylinder at the second longitudinal end 129 of the body 124. This groove 130 facilitates the mounting of the cable 70 on the shaft. 128 of body 124.
  • the shaft 128 of the perforation member 36 can comprise a fixing ring positioned more particularly at the level of the second longitudinal end 129 on which the cable 70 can be fixed.
  • the body 124 also carries a plurality of wings 132, each of these wings emerging radially from the shaft 128 of the body 124.
  • Each wing of the plurality of wings 132 extends longitudinally between the first longitudinal end 126 and the second end. longitudinal 129 of the body 124 and perpendicular to the shaft 128 outwardly of the perforator 36.
  • each wing of the plurality of wings 132 extends from the shaft 128 of the body 124. towards the outside of the perforation member 36 mainly in a plane in which the vertical axis A is inscribed.
  • Each wing of the plurality of wings 132 forms a rectangular flat sidewall with three free edges.
  • a first and a second free edges 134, 136 participate in delimiting each wing at the level of the first longitudinal end 126 and of the second longitudinal end 129 of the body 124.
  • Each wing of the plurality of wings 132 comprises a third free edge 138 advantageously parallel to the vertical axis A and extending at least in part between the first edge 134 and the second edge 136 of each wing of the plurality of wings 132.
  • the plurality of wings 132 has six wings distributed so that an angular sector between each of the wings of the plurality of wings 132 is regular.
  • the distance separating the third free edge 138 from two adjacent wings of the plurality of wings 132 is equal regardless of the adjacent wings of the plurality of wings 132 chosen to perform this measurement, the distance being measured perpendicularly to the vertical axis A.
  • the plurality of wings 132 comprises at least three wings. When the body 124 has three wings, they are distributed around the shaft 128 of the body 124 so as to form angles of substantially 120 degrees.
  • the third free edge 138 of each wing of the plurality of wings 132 at least partially delimits a circumference of the body 124, being inscribed in a circle which materializes this circumference.
  • the third free edge 138 of each wing of the plurality of wings 132 carries a coating 140 promoting the sliding of the body 124 in the tube 38.
  • This coating 140 advantageously extends from the first edge 134 to the second edge 136 of each wing. , thus covering the whole of the third free edge 138 of each wing.
  • the coating 140 is made of a synthetic material, such as high density polyethylene (HD-PE) or polytetrafluoroethylene (PTFE), otherwise called Teflon, in order to decrease the frictional forces between the third free edge 138 of each wing of the plurality.
  • wings 132 of the perforation member 36 and an internal face of the tube 38 Apart from the coating 140, the perforation member 36 is advantageously made of stainless steel, so that its weight is sufficient to allow perforation of the membrane primary seal 12 at the perforation zone 60.
  • the body 124 carries at its second longitudinal end 129 a disc 142 preventing the passage of the cable 70 at the level of the plurality of wings 132 when the perforating member 36 is in the recess 54 of the tube 38. Indeed, when the perforating member 36 is stopped at the end of its fall, the drum 68 continues to be driven in rotation by the weight of the cable 70. A part of the cable 70 accumulates on the disc 142, the latter hindering the passage of the cable 70 between the plurality of wings 132 and the internal face 33 of the tube 38.
  • the disc 142 extends mainly in a plane perpendicular to the vertical axis A, this axis coinciding with the center of the disc 142.
  • the disc 142 has an upper face 144 and a lower face, not visible in the figures, opposite to each other, the lower face facing towards the shaft 128 and towards the plurality of wings 132 of the body. 124.
  • the diameter of the disc 142 is equal to or less than a diameter in which the third free edges 138 of the plurality of wings 132 fit.
  • the diameter of the disc 142 must be large enough to accommodate it. preventing cable 70 from passing through a space between a peripheral edge 148 of disc 142 and an inner surface of tube 38.
  • the disc 142 comprises at least one through opening 146, and advantageously a plurality of through openings 146, these openings allowing fluid to flow through the disc 142 when the latter falls into the tube 38.
  • the term “through” is understood to mean that the opening opens onto the lower face and the upper face 144 of the disc 142, thus connecting the two faces of the disc 142.
  • the disc 142 as illustrated in FIG. 3 comprises a plurality of through openings 146 arranged close to the radially outer periphery of the disc 142.
  • the openings of the plurality of through openings 146 can be closed on their peripheries thus constituting through orifices, or open on the outer circumference of the disc then constituting through grooves.
  • the disc 142 has a peripheral edge 148 which extends between the upper and lower faces of the disc 142, the plurality of through openings 146 being formed close to this peripheral edge 148 without however being in contact with the latter. here.
  • the peripheral edge 148 has a chamfered shape between the upper face 144 and the lower face of the disc 142. It is understood that the peripheral edge 148 advantageously has three faces: a first face extending in a plane perpendicular to the plane of extension of the faces. upper 144 and lower of the disc 142, a second face providing the connection between the upper face 144 and the first face of the peripheral edge 148 and a third face providing the connection between the lower face of the disc 142 and the first face of the peripheral edge 148.
  • the disc 142 includes a groove 150 extending from the peripheral edge 148 of the disc 142 to the center thereof.
  • the groove 150 is formed so as to be aligned with the groove 130 of the shaft 128, the groove 150 allowing, similarly to the groove 130 of the shaft 128, the cable 70 to be mounted on the perforating member 36. It is possible to mount the cable 70 on the perforating member 36. can thus mount the disc 142 on the perforating member 36 after having attached it to the cable 70.
  • the disc 142 comprises a closed through orifice, instead of the groove 150, through which the cable 70 passes.
  • the disc 142 has at least one fixing hole 152 and advantageously several fixing holes 152 making it possible to make the disc 142 integral with the shaft 128 of the body 124.
  • the fixing hole or holes 152 cooperate with fixing means. not shown in the figures, such as screws for example, to fix the disc 142 to the shaft 128 of the body 124.
  • the perforation member 36 comprises the perforation head 122 generally taking the form of a cylinder 121 extending between a connecting edge 154 and a perforation cone 156.
  • the cylinder 121 has at least one groove 123 extending from it. the perforation cone 156 towards the connecting edge 154.
  • the perforation head 122 is integral with the body 124 at the level of the connecting edge 154, the latter thus being in contact with the first longitudinal end 126 of the body 124.
  • the perforation cone 156 of the perforation head 122 has a conical shape up to 'to a piercing point 158.
  • a user places the perforation device 32 at the level of the inlet mouth of the tube 38 of the tank 2, thus constituting a first step of the perforation process.
  • the perforation device 32 is positioned at the level of the outer mouth of the tube 38 so that the space 116 of the frame 66 is in contact with the outer mouth 56 of the tube 38 and that part of the cable 70 and the perforation 36 are disposed in the recess 54 of the tube 38 at the level of the outer end 44 of the tube 38.
  • the cable 70 is then wound around the drum 68 to keep the perforator 36 at the level of the outer end 44 of tube 38.
  • a second step consists in positioning the perforating member 36 at the level of the inner end 42 of the tube 38.
  • the user turns the crank 72 so that the drum 68 unwinds the cable 70 causing the descent of the cable.
  • perforation member 36 in the tube 38 in the direction of the bottom wall of the tank 2.
  • the descent of the perforation member 36 is thus controlled by the user turning the crank 72.
  • the drum 69 comprises a braking system limiting the rotational speed of the drum 68 and thus preventing the perforating member 36 from being released and breaking through one of the walls of the plurality of walls 4 of the tank 2.
  • This braking system is reversible so that the user can remove it when he wishes to release the perforating member 36.
  • the controlled descent of the perforating member 36 is carried out up to 'to this the piercing point 158 of the perforation member 36 comes into contact with the flat area 64 of the stud 62 of the tank bottom 50.
  • a third step of the perforation process consists of hoisting the perforating member 36 in the tube 38 to a release height and then blocking the drum 68 once the perforating member 36 is positioned at said height.
  • the user raises the perforation member 36 to a determined height which depends on factors such as the thickness of the primary waterproofing membrane, or even the presence of fluid in the tube 38.
  • this height is three meters, measured along the vertical axis A.
  • the user can count the number of revolutions that the drum 68 makes when the latter is hoisted before release.
  • the size of the drum 68 is configured so that the circumference of the drum 60 is approximately one meter, so that one turn of the rotating drum 68 causes the winding or unwinding of one meter of the drum. cable 70.
  • a fourth step of the method consists in releasing the perforating member 36. The user thus releases the drum 68 from the locking means 92, the perforating member 36 being driven by its weight towards the flat area 64 of the stud 62 of the bottom. tank 50.
  • the weight of the perforator 36 propels at a sufficient speed the perforating tip 158 of the perforating member 158 towards the flat area 64 of the stud 62 of the tank bottom 50, thus generating kinetic energy.
  • kinetic energy is converted into mechanical energy so that the piercing tip 158 perforates the primary waterproofing membrane 12 at the planar area 64 of the pad 62.
  • the perforation member 36 is raised by the user to the outer end 44 of the tube 38.
  • a fifth step of the perforation process then consists in hoisting the perforating member 36 into the tube 38. If the perforating member 36 has not sufficiently pierced the primary waterproofing membrane 12 following a first test , the user starts the perforation process again by positioning the perforation member 36 at the determined height from the interior mouth 58 of the tube 38 and again releasing from the perforation member 36 onto the primary waterproofing membrane 12, thus constituting a fifth step of the perforation process.
  • the user can thus start the perforation process again, and more particularly the second, third and fourth steps, until the primary waterproofing membrane 12 is perforated.
  • the user repeats these three steps as long as the hole in the primary waterproofing membrane 12 is not of a sufficient area for the fluid to very quickly exit the primary thermal insulation layer and join the internal volume 15 of the tank 2.
  • the unloading of the fluid contained in the tank 2 can be carried out without damaging the wall of the tank 2.
  • the liquid natural gas infiltrated into at least one of the walls 4 joins the internal volume 15. of the tank 2 via the perforation produced by the perforation member 36 in the primary waterproofing membrane 12.
  • the fluid infiltrated into the primary thermal insulation barrier 10 can thus be recovered, thus avoiding any risk of overpressure inside the wall of the tank which has been infiltrated.
  • actuating means 34 of the perforation member can be at least partially motorized, or even fully automated without departing from the scope of the invention.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Forests & Forestry (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The invention primarily relates to a perforating device (32) for a sealed, thermally insulating tank (2) designed to contain a fluid, characterised in that said perforating device (32) comprises an actuation means (34) and a perforating member (36) for the tank (2), the actuation means (34) being designed to produce a movement of the perforating member (36).

Description

DESCRIPTION DESCRIPTION
Titre : Moyen de perforation d’une cuve de gaz naturel à l’état liquideTitle: Means of perforating a natural gas tank in the liquid state
La présente invention se rapporte au domaine des cuves de gaz naturel à l’état liquide dans le transport maritime. Plus particulièrement, l’invention fait référence aux dispositifs préalables à la réparation de telles cuves mis en oeuvre en cas de fuite de gaz naturel à l’état liquide depuis une telle cuve. The present invention relates to the field of natural gas tanks in the liquid state in maritime transport. More particularly, the invention refers to the devices prior to the repair of such tanks used in the event of a leak of natural gas in the liquid state from such a tank.
Le gaz naturel à l’état liquide, ou gaz naturel liquide, est transporté par voie maritime dans des cuves de stockage étanches et thermiquement isolantes ménagées sur des navires de transport. Le gaz naturel est maintenu sous forme liquide pour augmenter la quantité de gaz naturel liquide transporté par cuve, le volume d’un litre de gaz naturel sous forme liquide étant bien inférieur au volume d’un litre de gaz naturel sous forme gazeuse. Ces cuves maintiennent le gaz naturel liquide à très basse température, et plus précisément à une température inférieure à -163°C, température à laquelle le gaz naturel est sous forme liquide à pression atmosphérique. Natural gas in the liquid state, or liquid natural gas, is transported by sea in sealed and thermally insulating storage tanks on transport ships. Natural gas is kept in liquid form to increase the amount of liquid natural gas transported per tank, the volume of one liter of natural gas in liquid form being much less than the volume of one liter of natural gas in gaseous form. These tanks maintain the liquid natural gas at very low temperature, and more precisely at a temperature below -163 ° C, temperature at which the natural gas is in liquid form at atmospheric pressure.
De telles cuves de gaz naturel liquide peuvent également être utilisées comme réservoir de carburant par certains navires. En d’autres termes, les navires chargent et stockent du gaz naturel liquide dans leurs cuves puis utilisent ensuite le gaz naturel liquide comme carburant pour le ou les moteurs du navire. Such liquid natural gas tanks can also be used as a fuel tank by some ships. In other words, ships load and store liquid natural gas in their tanks and then use the liquid natural gas as fuel for the ship's engine (s).
De plus, ces cuves peuvent être utilisées pour le stockage terrestre de gaz naturel liquide comme par exemple pour récupérer le gaz naturel liquide sur les quais lors du déchargement du gaz naturel liquide transportées par des cuves ménagées sur les navires. In addition, these tanks can be used for the terrestrial storage of liquid natural gas such as for example to recover the liquid natural gas on the docks during the unloading of the liquid natural gas transported by tanks arranged on the ships.
Les cuves de gaz naturel liquide présentent globalement une forme parallélépipédique dont les parois sont composées principalement d’un espace primaire et d’un espace secondaire, chacun des espaces comprenant une couche thermiquement isolante et une couche étanche, assurant respectivement le maintien du gaz naturel liquide à -163°C et la contenance du gaz naturel liquide dans la cuve. Liquid natural gas tanks generally have a parallelepipedal shape, the walls of which are mainly composed of a primary space and a secondary space, each of the spaces comprising a thermally insulating layer and a sealed layer, respectively ensuring the maintenance of the liquid natural gas. at -163 ° C and the capacity of liquid natural gas in the tank.
Cependant, une fuite de gaz naturel liquide peut survenir au niveau de la couche étanche de l’espace primaire, par exemple en raison d’une usure ou en raison d’un mauvais assemblage de la couche étanche de l’espace primaire. Le gaz naturel liquide contenu dans la cuve s’infiltre alors dans l’espace primaire et envahi la couche thermiquement isolante de l’espace primaire. Le gaz naturel liquide se répand alors dans l’ensemble de la couche thermiquement isolante de l’espace primaire. However, a liquid natural gas leak can occur at the sealed layer of the primary space, for example due to wear or due to improper assembly of the gasket. the waterproof layer of the primary space. The liquid natural gas contained in the tank then infiltrates into the primary space and invades the thermally insulating layer of the primary space. The liquid natural gas then spreads throughout the thermally insulating layer of the primary space.
Pour accéder à la fuite de la couche étanche et la réparer, la cuve contenant du gaz naturel liquide doit être vidée. Le gaz naturel liquide est ainsi évacué de la cuve, par exemple par des moyens connus qui visent à décharger le gaz naturel liquide hors de la cuve endommagée. A l’issue de cette étape de vidange de la cuve, une quantité significative de gaz naturel liquide peut demeurer dans la couche thermiquement isolante de G espace primaire. Le volume interne de la cuve étant vide, il n’y a plus d’équilibre de pression entre la couche thermiquement isolante de l’espace primaire et le volume interne. Le poids de ce GNL dans la couche thermiquement isolante de l’espace primaire pousse la couche étanche vers le volume interne de la cuve, ce qui peut endommager celle-ci. De plus du diazote injecté dans la cuve et de température plus élevée que la température du gaz naturel liquide contenu initialement dans la cuve, remplit le volume interne de cette dernière, augmentant ainsi la température au sein du volume interne de la cuve. Ce diazote plus chaud augmente la température des parois de la cuve. La température du gaz naturel liquide infiltré dans les parois de la cuve augmente alors, entraînant un changement d’état du gaz naturel, pour le faire passer d’un état liquide à un état gazeux. Cette vaporisation du gaz naturel provoque alors une augmentation de la pression sur les parois de la cuve en exerçant une force déformant la couche thermiquement isolante de l’espace primaire vers le volume interne de la cuve. Selon la quantité de gaz naturel infiltré dans les parois de cuve, la vaporisation de ce dernier endommage au moins en partie les parois de la cuve, notamment par arrachement de la couche étanche constituant la paroi de cuve. To access and repair the leak in the waterproof layer, the tank containing liquid natural gas must be emptied. The liquid natural gas is thus evacuated from the tank, for example by known means which aim to discharge the liquid natural gas out of the damaged tank. After this step of emptying the vessel, a significant amount of liquid natural gas may remain in the thermally insulating layer of the primary space. Since the internal volume of the vessel is empty, there is no longer a pressure balance between the thermally insulating layer of the primary space and the internal volume. The weight of this LNG in the thermally insulating layer of the primary space pushes the sealed layer towards the internal volume of the vessel, which can damage the vessel. In addition, the nitrogen injected into the tank and at a temperature higher than the temperature of the liquid natural gas initially contained in the tank, fills the internal volume of the latter, thus increasing the temperature within the internal volume of the tank. This hotter nitrogen increases the temperature of the walls of the tank. The temperature of the liquid natural gas infiltrated into the walls of the vessel then increases, causing the state of the natural gas to change from a liquid state to a gaseous state. This vaporization of natural gas then causes an increase in the pressure on the walls of the vessel by exerting a force deforming the thermally insulating layer from the primary space towards the internal volume of the vessel. Depending on the quantity of natural gas infiltrated into the vessel walls, the vaporization of the latter at least partially damages the vessel walls, in particular by tearing off the sealed layer constituting the vessel wall.
Dans ce contexte, la présente invention propose un dispositif de perforation permettant de produire un orifice de diamètre suffisant dans la couche étanche de l’espace primaire pour permettre au gaz naturel infiltré dans la couche thermiquement isolante de rejoindre très rapidement le volume interne de la cuve, et ce en évitant d’augmenter la pression exercée sur la ou les parois de cette cuve. La présente invention a donc pour but de faciliter l’évacuation du gaz naturel liquide infiltré dans la couche thermiquement isolante de l’espace primaire.In this context, the present invention proposes a perforation device making it possible to produce an orifice of sufficient diameter in the sealed layer of the primary space to allow the natural gas infiltrated into the thermally insulating layer to reach the internal volume of the tank very quickly. , and this while avoiding increasing the pressure exerted on the wall or walls of this tank. The object of the present invention is therefore to facilitate the evacuation of the liquid natural gas infiltrated into the thermally insulating layer of the primary space.
Pour cela, la présente invention a pour principal objet un dispositif de perforation pour une cuve étanche et thermiquement isolante configurée pour contenir un fluide, caractérisé en ce que le dispositif de perforation comprend un moyen d’actionnement et un organe de perforation de la cuve, le moyen d’actionnement étant configuré pour générer un mouvement de l’organe de perforation. For this, the main object of the present invention is a perforation device for a sealed and thermally insulating tank configured to contain a fluid, characterized in that the perforation device comprises an actuating means and a perforation member of the tank, the actuating means being configured to generate movement of the perforating member.
L’organe de perforation est configuré pour perforer la cuve, le moyen d’actionnement étant conçu pour autoriser ou bloquer le mouvement de l’organe de perforation. Le moyen d’actionnement comprend au moins une partie fixe et une partie mobile. La partie fixe du moyen d’actionnement permettant le maintien en position du dispositif de perforation dans l’espace, en le fixant sur un autre objet par exemple. La partie mobile participe à mettre en mouvement l’organe de perforation, ce dernier réalisant l’action de perforation de la cuve. The perforator is configured to perforate the vessel, the actuator being adapted to allow or block movement of the perforator. The actuating means comprises at least a fixed part and a movable part. The fixed part of the actuating means allowing the perforation device to be held in position in space, by fixing it to another object, for example. The mobile part helps set the perforating member in motion, the latter performing the action of perforating the tank.
La cuve est configurée pour contenir un fluide, avantageusement du gaz naturel liquide (GNL), à une température avoisinant - 163°C à pression atmosphérique. La cuve est ainsi thermiquement isolée, le maintien d’une température cryogénique étant primordial pour maintenir le fluide à l’état liquide. De plus, la cuve est étanche, évitant la fuite et/ou la perte du fluide contenu dans la cuve. The vessel is configured to contain a fluid, advantageously liquid natural gas (LNG), at a temperature of around -163 ° C at atmospheric pressure. The tank is thus thermally insulated, maintaining a cryogenic temperature being essential to maintain the fluid in the liquid state. In addition, the tank is sealed, preventing the leak and / or loss of the fluid contained in the tank.
La cuve est délimitée dans l’espace par une pluralité de parois. Ces parois prennent globalement la forme d’un parallélépipède rectangle. Le dispositif de perforation permet de perforer partiellement au moins l’une des parois de la pluralité de parois de la cuve, avantageusement la paroi de fond de la cuve, et réalise ainsi un trou de section suffisamment importante pour autoriser le retour du gaz naturel infiltré dans l’épaisseur des parois vers l’intérieur de la cuve. The tank is delimited in space by a plurality of walls. These walls generally take the form of a rectangular parallelepiped. The perforation device makes it possible to partially perforate at least one of the walls of the plurality of walls of the vessel, advantageously the bottom wall of the vessel, and thus produces a sufficiently large section hole to allow the return of the infiltrated natural gas. in the thickness of the walls towards the inside of the tank.
Selon une caractéristique optionnelle de l’invention, le moyen d’actionnement comporte au moins un bâti, un tambour et un câble reliant l’organe de perforation au tambour, le tambour étant configuré pour être mis en rotation autour d’un axe de rotation et entraîner l’enroulement ou le déroulement du câble autour du tambour. Le bâti loge le tambour et au moins une partie du câble. Le bâti est un élément de la partie fixe du moyen d’actionnement, le tambour et le câble étant quant à eux des éléments de la partie mobile du moyen d’actionnement. According to an optional characteristic of the invention, the actuating means comprises at least one frame, a drum and a cable connecting the perforation member to the drum, the drum being configured to be rotated about an axis of rotation. and driving the winding or unwinding of the cable around the drum. The frame houses the drum and at least part of the cable. The frame is an element of the fixed part of the actuating means, the drum and the cable being for their part elements of the movable part of the actuating means.
Le tambour est avantageusement de forme cylindrique et mobile en rotation autour d’un axe de rotation. Le moyen d’actionnement de l’organe de perforation comprend également une manivelle permettant d’entraîner manuellement le tambour en rotation. The drum is advantageously cylindrical in shape and movable in rotation about an axis of rotation. The means for actuating the perforating member also includes a crank for manually driving the rotating drum.
Le câble comprend une première extrémité solidaire du tambour et une deuxième extrémité solidaire de l’organe de perforation. Ainsi, la rotation du tambour dans un sens de rotation ou en sens inverse de rotation provoque l’enroulement ou le déroulement du câble autour du tambour. Le câble étant solidaire de l’organe de perforation, l’organe de perforation est ainsi en suspension au bout du câble. La rotation du tambour entraîne le mouvement de l’organe de perforation, soit pour le faire monter, soit pour le laisser chuter par gravité pour perforer la couche étanche, soit pour le descendre et prendre une référence sur la paroi de fond de la cuve. The cable comprises a first end integral with the drum and a second end integral with the perforation member. Thus, the rotation of the drum in one direction of rotation or in the opposite direction of rotation causes the cable to be wound or unwound around the drum. The cable being integral with the perforation member, the perforation member is thus suspended at the end of the cable. The rotation of the drum causes the movement of the perforator, either to raise it, or to let it fall by gravity to perforate the waterproof layer, or to lower it and take a reference on the bottom wall of the tank.
Le câble est constitué en matière métallique ou synthétique. On peut également imaginer que le câble est constitué en partie d’une matière synthétique et en partie d’une matière métallique.The cable is made of metallic or synthetic material. One can also imagine that the cable is made partly of a synthetic material and partly of a metallic material.
Selon une autre caractéristique optionnelle de l’invention, l’organe de perforation comprend au moins une tête de perforation et un corps, chacun s’étendant longitudinalement l’un à la suite de l’autre. According to another optional feature of the invention, the perforating member comprises at least one perforating head and a body, each extending longitudinally one after the other.
L’organe de perforation comprend une première portion constituée du corps par laquelle l’organe de perforation est solidaire du câble et une deuxième portion constituée de la tête de perforation configurée pour réaliser l’action de perforation. The perforation member includes a first portion consisting of the body by which the perforation member is integral with the cable and a second portion consisting of the perforation head configured to perform the perforation action.
Le corps est un élément assurant ici la liaison entre le câble et la tête de perforation, le corps ne participant pas directement à la perforation d’une paroi de la cuve. Le corps confère par sa masse une inertie qui permet à l’organe de perforation de remplir sa fonction qui consiste à défoncer la couche étanche primaire de la cuve. The body is an element here ensuring the connection between the cable and the perforation head, the body not directly participating in the perforation of a wall of the tank. The body imparts inertia through its mass which allows the perforation member to fulfill its function of breaking through the primary sealed layer of the tank.
La tête de perforation est un cylindre dont l’une des extrémités est biseautée, de sorte à former une pointe de perforation. La tête de perforation est l’élément de l’organe de perforation réalisant l’action de perforation de la paroi de la cuve. La tête de perforation prolonge longitudinalement le corps de l’organe de perforation. On peut imaginer que le corps prend globalement la forme d’un cylindre, la tête de perforation prolongeant axialement le cylindre formant le corps au niveau de l’une de ses extrémités. The perforation head is a cylinder, one of the ends of which is bevelled, so as to form a perforation point. The perforation head is the element of the perforation member performing the action of perforating the wall of the tank. The perforation head longitudinally extends the body of the perforation member. One can imagine that the body generally takes the form of a cylinder, the perforation head axially extending the cylinder forming the body at one of its ends.
Selon une autre caractéristique optionnelle de l’invention, le corps présente une première extrémité longitudinale solidaire de la tête de perforation et une deuxième extrémité longitudinale solidaire du câble. According to another optional feature of the invention, the body has a first longitudinal end integral with the perforation head and a second longitudinal end integral with the cable.
Le corps s’étend entre une première extrémité longitudinale et une deuxième extrémité longitudinale, le corps étant solidaire de la tête de perforation au niveau de sa première extrémité longitudinale et solidaire du câble au niveau de sa deuxième extrémité longitudinale. Autrement dit, le corps est solidaire d’une part du câble et d’une autre part de la tête de perforation, de sorte que la tête de perforation est opposée au câble par rapport au corps. The body extends between a first longitudinal end and a second longitudinal end, the body being integral with the perforation head at its first longitudinal end and integral with the cable at its second longitudinal end. In other words, the body is integral on the one hand with the cable and on the other hand with the punch head, so that the punch head is opposite the cable with respect to the body.
Selon une autre caractéristique optionnelle de l’invention, le corps comprend une pluralité d’ailes et un arbre duquel émerge radialement la pluralité d’ailes. According to another optional feature of the invention, the body includes a plurality of wings and a shaft from which the plurality of wings emerge radially.
L’arbre du corps prend globalement la forme d’un cylindre délimités par les première et deuxième extrémités longitudinales duquel émerge radialement la pluralité d’ailes. On comprend que les ailes émergent chacune dans un plan dans lequel s’inscrit un axe passant par le centre du cylindre et par les deux extrémités longitudinales du corps. The shaft of the body generally takes the form of a cylinder bounded by the first and second longitudinal ends from which the plurality of wings emerge radially. It is understood that the wings each emerge in a plane in which is inscribed an axis passing through the center of the cylinder and through the two longitudinal ends of the body.
Les ailes sont des flancs plats de forme globalement rectangulaire. Le corps comprend au moins trois ailes réparties angulairement de façon régulière autour de l’arbre du corps. Que la pluralité d’ailes comprenne trois ailes ou plus, le secteur angulaire séparant deux ailes voisines, c’est-à-dire deux ailes séparées par un espace ne comprenant pas d’aile, est constante quel que soit le nombre d’ailes. The wings are flat sides of generally rectangular shape. The body includes at least three wings distributed angularly evenly around the shaft of the body. Whether the plurality of wings include three or more wings, the angular sector separating two neighboring wings, that is to say two wings separated by a space not comprising a wing, is constant regardless of the number of wings. .
La pluralité d’ailes s’étend sous une forme d’étoile dans un plan perpendiculaire à l’axe d’extension principale de l’organe de perforation, dont le centre serait représenté par l’arbre du corps et dont chaque branche de l’étoile serait matérialisée par chaque aile de la pluralité d’ailes.The plurality of wings extend in a star shape in a plane perpendicular to the main axis of extension of the piercing member, the center of which would be represented by the shaft of the body and of which each branch of the The star would be materialized by each wing of the plurality of wings.
Selon une autre caractéristique optionnelle de l’invention, au moins une aile de la pluralité d’ailes comprend une extrémité libre délimitant au moins en partie une circonférence du corps et possédant un revêtement favorisant un glissement du corps. Chaque aile de la pluralité d’ailes présente trois extrémités libres, une première et une deuxième extrémités libres s’étendant depuis l’arbre du corps vers l’extérieur de l’organe de perforation et une troisième extrémité libre s’étendant parallèlement à l’arbre de corps entre les deux autres extrémités. According to another optional characteristic of the invention, at least one wing of the plurality of wings comprises a free end defining at least in part a circumference of the body and having a coating which promotes sliding of the body. Each wing of the plurality of wings has three free ends, a first and a second free end extending from the shaft of the body outwardly of the perforating member and a third free end extending parallel to the body shaft. body shaft between the other two ends.
La troisième extrémité de chacune des ailes de la pluralité d’ailes participe à définir une circonférence du corps, les troisièmes extrémités étant les éléments les plus en saillie radialement vers l’exrérieur du corps. The third end of each of the plurality of wings helps define a circumference of the body, the third ends being the most radially outwardly projecting elements of the body.
Chacune des troisièmes extrémités de la pluralité d’ailes comprend un revêtement aidant à diminuer les forces de frottement s’appliquant entre les troisièmes extrémités de la pluralité d’ailes et un élément externe, par exemple un tube métallique constitutif de la cuve. Plus particulièrement, le revêtement peut, selon un exemple non limitatif, être en matière synthétique comme par exemple du polyéthylène à haute densité (PE-HD) ou du polytétrafluoroéthylène (PTFE), autrement appelé Teflon . Ce type de revêtement permet de diminuer les forces de frottement entre les troisièmes extrémités de la pluralité d’ailes et un élément métallique par exemple. Each of the third ends of the plurality of wings includes a coating to help decrease the frictional forces applied between the third ends of the plurality of wings and an outer member, such as a metal tube constituting the vessel. More particularly, the coating can, according to a nonlimiting example, be made of synthetic material such as for example high density polyethylene (PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. This type of coating makes it possible to reduce the frictional forces between the third ends of the plurality of wings and a metal element, for example.
Selon une autre caractéristique optionnelle de l’invention, le corps porte un disque au niveau de sa deuxième extrémité longitudinale. According to another optional feature of the invention, the body carries a disc at its second longitudinal end.
Le disque est ainsi solidaire du corps au niveau de la deuxième extrémité longitudinale du corps.The disc is thus integral with the body at the level of the second longitudinal end of the body.
Le disque s’étend principalement dans un plan perpendiculaire à l’axe longitudinal de l’arbre, cet axe passant également par un centre du disque. The disc extends primarily in a plane perpendicular to the longitudinal axis of the shaft, this axis also passing through a center of the disc.
Le disque a pour fonction de maintenir le câble au-dessus de l’organe de perforation, notamment lorsque celui-ci est installé dans un tube. De la sorte, le câble ne s’interpose pas entre l’organe de perforation et le tube. The function of the disc is to keep the cable above the perforation member, especially when the latter is installed in a tube. In this way, the cable does not come between the perforator and the tube.
Selon une autre caractéristique optionnelle de l’invention, le disque comporte au moins une ouverture traversante. According to another optional feature of the invention, the disc has at least one through opening.
On comprend par ouverture traversante une ouverture débouchant de part et d’autre du disque, un fluide pouvant ainsi circuler à travers le disque en circulant au travers de l’ouverture traversante. L’ouverture traversante peut être fermée sur sa périphérie et formée un orifice traversant. Alternativement, l’ouverture traversante peut également être ouvert sur la circonférence externe du disque et formée une saignée traversante. A through opening is understood to mean an opening opening out on either side of the disc, a fluid thus being able to circulate through the disc by circulating through the through opening. The through opening can be closed on its periphery and formed an orifice crossing. Alternatively, the through opening can also be opened on the outer circumference of the disc and formed a through groove.
Le disque peut comprendre une pluralité d’ouvertures traversantes. L’ouverture traversante ou la pluralité d’ouvertures traversantes sont spécialement dimensionnées pour ne pas ralentir la chute de l’organe de perforation lors de son largage. En effet, le tube peut contenir du fluide, et la présence de trou dans le disque autorise ainsi la circulation du fluide au travers du disque sans freiner la chute de l’organe de perforation. The disc can include a plurality of through openings. The through opening or the plurality of through openings are specially sized so as not to slow down the fall of the piercing member during its release. In fact, the tube may contain fluid, and the presence of a hole in the disc thus allows fluid to flow through the disc without slowing down the fall of the perforator.
Le disque comporte au moins une saignée traversante autorisant le passage du câble. The disc has at least one through groove allowing the passage of the cable.
La saignée traversante s’étend depuis une périphérie du disque et vers le centre de celui-ci. La saignée traversante autorise le montage du disque sur l’organe de perforation une fois que ce dernier est lié au câble reliant le corps au tambour. En effet, lors du montage du disque sur l’organe de perforation, le disque est monté sur le corps en insérant le câble à travers la saignée, de la périphérie du disque jusqu’au centre de celui-ci. La saignée traversante du disque facilite le montage du disque sur le corps puisque le câble peut avoir été préalablement attaché au corps.The through groove extends from a periphery of the disc and towards the center of it. The through groove allows mounting of the disc on the perforating member once the latter is linked to the cable connecting the body to the drum. Indeed, when mounting the disc on the perforating member, the disc is mounted on the body by inserting the cable through the groove, from the periphery of the disc to the center thereof. The through groove of the disc facilitates the mounting of the disc on the body since the cable may have been previously attached to the body.
Selon une autre caractéristique optionnelle de l’invention, le disque est au moins en partie en matière favorisant le glissement du disque. According to another optional feature of the invention, the disc is at least partly made of material which promotes the sliding of the disc.
Le disque est au moins en partie en matière synthétique, comme par exemple du polyéthylène à haute densité (PE-HD) ou du polytétrafluoroéthylène (PTFE) , autrement appelé Teflon . On comprend que le disque peut être amené à être en contact avec une surface au niveau de sa périphérie, la matière favorisant le glissement du disque étant sur cette surface. The disc is at least partly made of synthetic material, such as for example high density polyethylene (PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. It will be understood that the disc can be brought into contact with a surface at the level of its periphery, the material favoring the sliding of the disc being on this surface.
Au moins la périphérie du disque est en matière favorisant le glissement du disque, mais l’ensemble de disque peut être en matière favorisant le glissement du disque sans pour autant sortir du cadre de l’invention. De plus et selon un autre mode de réalisation, le disque peut également être constitué en matière métallique et être recouvert au moins sur sa périphérie par une matière synthétique, telle que celles exposées ci-dessus. At least the periphery of the disc is of disc slip material, but the disc assembly may be of disc slip material without departing from the scope of the invention. In addition and according to another embodiment, the disc can also be made of metallic material and be covered at least on its periphery by a synthetic material, such as those described above.
Selon une autre caractéristique optionnelle de l’invention, le disque présente un diamètre inférieur ou égal à un diamètre dans lequel s’inscrivent les extrémités libres de la pluralité d’ailes. Selon une autre caractéristique optionnelle de l’invention, le moyen d’actionnement comprend un moyen de blocage de la rotation du tambour, le moyen de blocage étant configuré pour libérer l’organe de perforation et obtenir sa chute. According to another optional characteristic of the invention, the disc has a diameter less than or equal to a diameter in which the free ends of the plurality of wings fit. According to another optional characteristic of the invention, the actuating means comprises a means for blocking the rotation of the drum, the blocking means being configured to release the perforation member and obtain its fall.
Le tambour présente au moins une ouverture configurée pour loger le moyen de blocage de la rotation du tambour. Le moyen de blocage de la rotation du tambour comporte au moins une tige, la tige présentant une portion rectiligne entourée au moins en partie par un manchon en matière favorisant l’extraction du moyen de blocage hors de l’ouverture du tambour, comme du polyéthylène à haute densité (PE-HD) ou du polytétrafluoroéthylène (PTFE), autrement appelé Téflon . The drum has at least one opening configured to accommodate the means for blocking the rotation of the drum. The means for blocking the rotation of the drum comprises at least one rod, the rod having a rectilinear portion surrounded at least in part by a sleeve made of material favoring the extraction of the blocking means from the opening of the drum, such as polyethylene high density (PE-HD) or polytetrafluoroethylene (PTFE), otherwise known as Teflon.
Lorsque la tige est logée dans l’ouverture du tambour, ce dernier ne peut pas être entraîné en rotation, l’organe de perforation étant alors immobilisé. L’extraction de la tige du tambour permet de libérer la mise en rotation du tambour autorisant ainsi la chute de l’organe de perforation. When the rod is housed in the opening of the drum, the latter cannot be rotated, the perforating member then being immobilized. The extraction of the rod from the drum frees the rotation of the drum, thus allowing the perforation member to fall.
L’invention a également pour objet une cuve étanche et thermiquement isolante configurée pour contenir un fluide, la cuve comprenant une pluralité de parois, caractérisée en ce que la cuve comporte un tube traversant au moins l’une des parois de la cuve et s’étendant entre une première extrémité ménagée à l’intérieur de la cuve et une deuxième extrémité ménagée à l’extérieur de la cuve, cuve comprenant un dispositif de perforation selon l’une quelconque des caractéristiques précédentes. The subject of the invention is also a sealed and thermally insulating tank configured to contain a fluid, the tank comprising a plurality of walls, characterized in that the tank comprises a tube passing through at least one of the walls of the tank and s' extending between a first end formed inside the tank and a second end formed outside the tank, the tank comprising a perforating device according to any one of the preceding characteristics.
La cuve est capable de stocker un fluide, la pluralité de parois de la cuve assurant l’étanchéité et l’isolation thermique de ladite cuve. La cuve comprend également un dispositif de perforation comprenant au moins l’une des caractéristiques précédemment décrites. On comprend ici que la cuve et le dispositif de perforation sont deux objets distincts qui peuvent coopérer l’un avec l’autre. The vessel is capable of storing a fluid, the plurality of vessel walls providing sealing and thermal insulation of said vessel. The tank also includes a perforation device comprising at least one of the features described above. It is understood here that the tank and the perforating device are two separate objects which can cooperate with each other.
La cuve est ainsi délimitée dans l’espace par la pluralité de parois, la pluralité de parois prenant avantageusement une forme parallélépipédique. The tank is thus delimited in space by the plurality of walls, the plurality of walls advantageously taking a parallelepipedal shape.
Le tube traverse l’une des parois de la pluralité de parois de la cuve, avantageusement un plafond, en présentant une première extrémité débouchant à l’intérieur de la cuve et une deuxième extrémité débouchant à l’extérieur de la cuve. L’extrémité débouchant à l’intérieur de la cuve est proche d’une paroi de fond de la cuve. The tube passes through one of the walls of the plurality of walls of the tank, advantageously a ceiling, having a first end opening out inside the tank and a second end. end opening to the outside of the tank. The end opening inside the tank is close to a bottom wall of the tank.
Le dispositif de perforation est installé au niveau de l’extrémité du tube débouchant à l’extérieur de la cuve, de sorte que l’organe de perforation puisse être en mouvement entre les première et deuxième extrémité du tube, voire jusqu’à la paroi de fond de la cuve. The perforation device is installed at the end of the tube opening out to the outside of the tank, so that the perforating member can be in motion between the first and second ends of the tube, or even up to the wall. bottom of the tank.
Selon une autre caractéristique optionnelle de l’invention, l’organe de perforation est disposé dans le tube, le tambour enroulant le câble pour hisser l’organe de perforation. According to another optional feature of the invention, the perforating member is disposed in the tube, the drum winding the cable to hoist the perforating member.
On comprend que l’organe de perforation peut être en partie mis en mouvement dans le tube grâce à la rotation du tambour, le sens de rotation du tambour enroulant ou déroulant le câble autour du tambour, ce qui a pour conséquence de rapprocher ou d’éloigner l’organe de perforation du tambour de la paroi de fond de la cuve. It is understood that the perforation member can be partly set in motion in the tube by virtue of the rotation of the drum, the direction of rotation of the drum winding or unwinding the cable around the drum, which has the consequence of bringing together or of move the perforation member of the drum away from the bottom wall of the tank.
Selon une autre caractéristique optionnelle de l’invention, l’organe de perforation et le tube sont configurés pour que l’organe de perforation coulisse dans le tube. According to another optional feature of the invention, the perforator and the tube are configured so that the perforator slides in the tube.
L’organe de perforation présente ainsi une section plus petite que la section du tube, cela dans le but d’éviter de coincer l’organe de perforation dans le tube. The perforator thus has a section smaller than the section of the tube, in order to avoid jamming the perforator in the tube.
On comprend que pour que l’organe de perforation puisse être en mouvement dans le tube, la circonférence dans laquelle s’inscrivent au moins en partie les extrémités libres de la pluralité d’ailes est nécessairement plus petite que la section interne du tube. It is understood that in order for the perforator to be able to move in the tube, the circumference in which the free ends of the plurality of wings are at least partially inscribed is necessarily smaller than the internal section of the tube.
Selon une autre caractéristique optionnelle de l’invention, chaque paroi de la pluralité de parois comporte successivement dans le sens de l’épaisseur depuis l’extérieur vers l’intérieur de la cuve, une barrière d’isolation thermique secondaire, une membrane d’étanchéité secondaire, une barrière d’isolation thermique primaire et une membrane d’étanchéité primaire et destinée à être en contact avec le fluide contenu dans le cuve, la membrane d’étanchéité primaire présentant une zone de perforation disposée en regard de l’extrémité du tube débouchant à l’intérieur de la cuve.According to another optional characteristic of the invention, each wall of the plurality of walls comprises successively in the direction of the thickness from the outside towards the inside of the tank, a secondary thermal insulation barrier, a membrane of secondary waterproofing, a primary thermal insulation barrier and a primary waterproofing membrane and intended to be in contact with the fluid contained in the tank, the primary waterproofing membrane having a perforation zone arranged opposite the end of the tube opening inside the tank.
La barrière d’isolation thermique secondaire et la membrane d’étanchéité secondaire forment un espace secondaire de la cuve, tandis que la barrière d’isolation thermique primaire et la membrane d’étanchéité primaire forment un espace primaire de la cuve. On comprend également que la membrane d’étanchéité secondaire est portée par la barrière d’isolation thermique secondaire tout en étant en contact avec la barrière d’isolation thermique primaire. The secondary thermal insulation barrier and the secondary waterproofing membrane form a secondary space of the vessel, while the primary thermal insulation barrier and the primary waterproofing membrane form a primary space of the vessel. It is also understood that the secondary waterproofing membrane is carried by the secondary thermal insulation barrier while being in contact with the primary thermal insulation barrier.
Les barrières d’isolation thermique participent au maintien de la température du fluide stocké dans la cuve en limitant les échanges thermiques entre l’environnement extérieur de la cuve et l’intérieur de la cuve. Les membranes d’étanchéité empêchent toutes fuites du fluide vers l’extérieur de la cuve. Thermal insulation barriers help maintain the temperature of the fluid stored in the tank by limiting heat exchange between the environment outside the tank and the inside of the tank. The sealing membranes prevent any leakage of fluid to the outside of the tank.
La zone de perforation est caractérisée par un amincissement de la membrane d’étanchéité primaire facilitant la perforation de cette dernière par l’organe de perforation. Le tube est positionné de sorte que l’extrémité débouchant à l’intérieur de la cuve soit en regard de la zone de perforation. The perforation zone is characterized by a thinning of the primary waterproofing membrane facilitating the perforation of the latter by the perforation member. The tube is positioned so that the end opening inside the tank is facing the perforation area.
Selon une autre caractéristique optionnelle de l’invention, la membrane d’étanchéité primaire forme un plot comportant au moins une zone plane au niveau de la zone de perforation. According to another optional feature of the invention, the primary waterproofing membrane forms a stud comprising at least one flat area at the level of the perforation area.
Le plot permet de rapprocher la zone de perforation de l’extrémité débouchant à l’intérieur de la cuve, diminuant le risque que l’organe de perforation perfore la membrane d’étanchéité secondaire, après avoir perforer la membrane d’étanchéité primaire. L’organe de perforation perfore la zone plane du plot, cette dernière étant avantageusement en regard de l’extrémité débouchant à l’intérieur de la cuve du tube. The stud allows the perforation area to be brought closer to the end opening inside the tank, reducing the risk that the perforator will puncture the secondary waterproofing membrane, after having perforated the primary waterproofing membrane. The perforation member perforates the flat zone of the stud, the latter advantageously facing the end opening inside the vessel of the tube.
Selon une autre caractéristique optionnelle de l’invention, la longueur de la tête de perforation suivant le sens du mouvement du perforateur est inférieure à l’épaisseur de la barrière isolante primaire ou bien à l’épaisseur correspondant à la somme de l’épaisseur de la barrière isolante primaire et la hauteur du plot. Cela permet avantageusement d’éviter de perforer la membrane secondaire en créant par l’intermédiaire de la membrane primaire une butée au niveau de la pluralité d’ailes. According to another optional characteristic of the invention, the length of the perforation head following the direction of movement of the perforator is less than the thickness of the primary insulating barrier or else the thickness corresponding to the sum of the thickness of the primary insulating barrier and the height of the stud. This advantageously makes it possible to avoid perforating the secondary membrane by creating a stop via the primary membrane at the level of the plurality of wings.
L’invention concerne de plus un navire comprenant une cuve selon l’une quelconque des caractéristiques précédentes. The invention further relates to a vessel comprising a tank according to any one of the preceding characteristics.
Le navire comprend la cuve capable de stocker un fluide, la pluralité de parois de la cuve assurant l’étanchéité et l’isolation thermique de ladite cuve. Le navire comprend également un dispositif de perforation comprenant au moins l’une des caractéristiques précédemment décrites. L’invention a également pour objet un procédé de perforation d’une cuve équipant un navire selon l’une quelconque des caractéristiques précédentes, caractérisé en ce qu’une première étape consiste à installer le dispositif de perforation au niveau de la deuxième extrémité. The vessel comprises the vessel capable of storing a fluid, the plurality of vessel walls ensuring the sealing and thermal insulation of said vessel. The vessel also includes a perforation device comprising at least one of the features described above. The subject of the invention is also a method for perforating a tank fitted to a ship according to any one of the preceding characteristics, characterized in that a first step consists in installing the perforating device at the level of the second end.
La première étape consiste à positionner le moyen d’actionnement du dispositif de perforation au niveau de la deuxième extrémité du tube, l’organe de perforation étant installé dans le tube également au niveau de la deuxième extrémité du tube. The first step is to position the actuating means of the piercing device at the second end of the tube, the piercing member being installed in the tube also at the second end of the tube.
Selon une autre caractéristique de l’invention, une deuxième étape consiste à coulisser l’organe de perforation dans le tube pour l’amener contre une paroi de fond de la cuve. According to another characteristic of the invention, a second step consists in sliding the perforating member in the tube to bring it against a bottom wall of the tank.
On comprend que la deuxième étape consiste à amener, c’est-à-dire descendre de manière contrôlée, l’organe de perforation dans le tube contre une paroi de fond de la cuve. Pour ce faire, l’organe de perforation coulisse dans le tube. It is understood that the second step consists in bringing, that is to say lowering in a controlled manner, the perforating member in the tube against a bottom wall of the tank. To do this, the perforator slides in the tube.
Selon une autre caractéristique de l’invention, une troisième étape consiste à positionner l’organe de perforation dans le tube à une hauteur de largage, puis à bloquer un tambour constitutif du dispositif de perforation une fois l’organe de perforation positionné à ladite hauteur de largage.According to another characteristic of the invention, a third step consists in positioning the perforation member in the tube at a release height, then in blocking a constituent drum of the perforation device once the perforation member is positioned at said height. release.
L’utilisateur positionne l’organe de perforation à une certaine hauteur, par exemple de trois mètres, puis bloque la rotation du tambour pour immobilier l’organe de perforation à cette hauteur. Pour s’assurer que la mesure de la hauteur de largage de l’organe de perforation soit correcte, l’organe de perforation est positionné sur la paroi de fond de la cuve de manière à prendre une référence. Cette position est alors qualifiée de point de début de mesure et fait office de référence de départ de la hauteur de largage. The user positions the perforator at a certain height, such as three meters, and then blocks the rotation of the drum to accommodate the perforator at that height. To ensure that the measurement of the release height of the perforation member is correct, the perforation member is positioned on the bottom wall of the tank so as to take a reference. This position is then referred to as the measurement start point and acts as the starting reference for the release height.
Selon une autre caractéristique de l’invention, une quatrième étape consiste à larguer l’organe de perforation. According to another characteristic of the invention, a fourth step consists in releasing the perforation member.
L’utilisateur libère la mise en rotation du tambour pour libérer l’organe de perforation et le laisser s’écraser contre la paroi de fond de la cuve. Entraîné par son poids vers la zone de perforation, l’organe de perforation accumule de l’énergie cinétique qu’il transmettra sous forme d’énergie mécanique au moment de son impact sur la zone de perforation. La hauteur est définie pour que l’organe de perforation puisse accumuler suffisamment d’énergie cinétique en vue de perforer la membrane d’étanchéité primaire. Selon une caractéristique optionnelle de l’invention, la deuxième étape, la troisième étape, la quatrième étape sont répétées jusqu’à ce que la membrane d’étanchéité primaire soit perforée.The user releases the rotation of the drum to free the perforating member and let it crash against the bottom wall of the tank. Driven by its weight towards the perforation zone, the perforation member accumulates kinetic energy which it will transmit in the form of mechanical energy at the time of its impact on the perforation zone. The height is set so that the perforator can accumulate sufficient kinetic energy to perforate the primary waterproofing membrane. According to an optional characteristic of the invention, the second step, the third step, the fourth step are repeated until the primary waterproofing membrane is perforated.
Selon une caractéristique optionnelle de l’invention, une quatrième étape consiste à hisser l’organe de perforation dans le tube. According to an optional feature of the invention, a fourth step consists of hoisting the perforating member into the tube.
D’autres caractéristiques, détails et avantages de l’invention ressortiront plus clairement à la lecture de la description qui suit d’une part, et de plusieurs exemples de réalisation donnés à titre indicatif et non limitatif en référence aux dessins schématiques annexés d’autre part, sur lesquels : Other characteristics, details and advantages of the invention will emerge more clearly on reading the description which follows, on the one hand, and of several embodiments given by way of indication and not by way of limitation with reference to the appended schematic drawings on the other hand. share, on which:
[Fig. 1] est un schéma en coupe d’une cuve équipé d’un dispositif de perforation selon l’invention ; [Fig. 1] is a sectional diagram of a tank equipped with a perforation device according to the invention;
[Fig. 2] est une coupe transversale d’un moyen d’actionnement du dispositif de perforation selon la figure 1 ; [Fig. 2] is a cross section of a means for actuating the perforating device according to Figure 1;
[Fig. 3] est une vue en perspective de l’organe de perforation du dispositif de perforation selon la figure 1 ; [Fig. 3] is a perspective view of the perforating member of the perforating device according to Figure 1;
[Fig. 4] est une vue en perspective d’un moyen de blocage constitutif du moyen d’actionnement du dispositif de perforation. [Fig. 4] is a perspective view of a constituent locking means of the actuating means of the perforation device.
Les caractéristiques, variantes et les différentes formes de réalisation de l’invention peuvent être associées les unes avec les autres, selon diverses combinaisons, dans la mesure où elles ne sont pas incompatibles ou exclusives les unes par rapport aux autres. On pourra notamment imaginer des variantes de l’invention ne comprenant qu’une sélection de caractéristiques décrites par la suite de manière isolée des autres caractéristiques décrites, si cette sélection de caractéristiques est suffisante pour conférer un avantage technique et/ou pour différencier l’invention par rapport à l’état de la technique antérieur. The characteristics, variants and the different embodiments of the invention can be associated with each other, in various combinations, as long as they are not incompatible or exclusive with respect to each other. It is in particular possible to imagine variants of the invention comprising only a selection of characteristics described below in isolation from the other characteristics described, if this selection of characteristics is sufficient to confer a technical advantage and / or to differentiate the invention. compared to the state of the prior art.
Tout d’abord, sur la figure 1 est représentée une cuve 2 étanche et thermiquement isolante délimitée dans l’espace par une pluralité de parois 4, la cuve 2 prenant globalement la forme d’un parallélépipède rectangle dont seulement quatre de ses parois sont illustrées ici. La cuve 2 est configurée pour contenir et/ou stocker un fluide, et plus particulièrement un liquide cryogénique, comme par exemple du gaz naturel liquide ou du gaz de pétrole liquéfié. Selon un exemple non limitatif, ce type de cuve 2 est utilisée dans le transport maritime, comme cuve de transport de gaz naturel liquide, ou encore comme réservoir de carburant d’un navire. Par ailleurs, cette cuve 2 peut également être utilisée pour le stockage terrestre de gaz naturel First, in Figure 1 is shown a sealed and thermally insulating tank 2 delimited in space by a plurality of walls 4, the tank 2 generally taking the form of a rectangular parallelepiped of which only four of its walls are illustrated. here. The tank 2 is configured to contain and / or store a fluid, and more particularly a cryogenic liquid, such as for example liquid natural gas or liquefied petroleum gas. According to a non-limiting example, this type of tank 2 is used in maritime transport, as tank for transporting liquid natural gas, or as a fuel tank for a ship. Furthermore, this tank 2 can also be used for onshore storage of natural gas.
Le gaz naturel est plus dense sous forme liquide que sous forme gazeuse, le stockage de gaz naturel est donc plus important quantitativement lorsque le gaz naturel est sous forme liquide. Le gaz naturel est sous forme liquide à pression atmosphérique à une température de -Natural gas is denser in liquid form than in gaseous form, so the storage of natural gas is quantitatively more important when natural gas is in liquid form. Natural gas is in liquid form at atmospheric pressure at a temperature of -
163 °C. 163 ° C.
La cuve 2 est configurée pour maintenir le gaz naturel liquide à une température d’au plus de -163 °C. Pour cela, chaque paroi de la pluralité de parois 4 de la cuve 2 comporte successivement dans le sens de l’épaisseur de l’extérieur vers l’intérieur de la cuve 2, un espace secondaire 16 et un espace primaire 14 étanches et indépendants l’un de l’autre. Vessel 2 is configured to maintain liquid natural gas at a temperature of no more than -163 ° C. For this, each wall of the plurality of walls 4 of the tank 2 comprises successively in the direction of the thickness from the outside to the inside of the tank 2, a secondary space 16 and a primary space 14 sealed and independent l 'from each other.
L’espace secondaire comprend une barrière d’isolation thermique secondaire 6 et une membrane d’étanchéité secondaire 8 portée par la barrière d’isolation thermique secondaire 6. L’espace primaire comprend une barrière d’isolation thermique primaire 10 reposant contre la membrane d’étanchéité secondaire 8 et une membrane d’étanchéité primaire 12 portée par la barrière d’isolation thermique primaire 10. Cette membrane d’étanchéité primaire 12 est destinée à être en contact avec le fluide contenu dans la cuve 2. The secondary space comprises a secondary thermal insulation barrier 6 and a secondary waterproofing membrane 8 carried by the secondary thermal insulation barrier 6. The primary space comprises a primary thermal insulation barrier 10 resting against the membrane d. secondary sealing 8 and a primary sealing membrane 12 carried by the primary thermal insulation barrier 10. This primary sealing membrane 12 is intended to be in contact with the fluid contained in the tank 2.
La barrière d’isolation thermique secondaire 6 est en contact avec l’environnement extérieur de la cuve 2, en particulier avec une structure de support. Dans le cas où la cuve est installée sur un navire, la barrière d’isolation thermique secondaire 6 est par exemple en contact avec une coque interne du navire. La barrière d’isolation thermique secondaire 6 présente ainsi une face externe 18, tournée vers l’environnement extérieur de la cuve 2. La membrane d’étanchéité secondaire 8 est quant à elle en contact d’une part avec la barrière d’isolation thermique secondaire 6 et d’autre part avec la barrière d’isolation thermique primaire 10 qui porte la membrane d’étanchéité primaire 12. Les barrières d’isolation thermique 6, 10 participent au maintien de la température à l’intérieur de la cuve 2 tandis que les membranes d’étanchéité 8, 12 forme une couche imperméable aux fluides que pourrait contenir la cuve 2. Selon l’invention, la cuve 2 comprend un dispositif de perforation 32 comprenant au moins un moyen d’actionnement 34 et un organe de perforation 36 de la cuve 2, le moyen d’actionnement 34 étant configuré pour mettre en mouvement l’organe de perforation 36. C’est ainsi que le moyen d’actionnement 34 peut hisser l’organe de perforation 36, ou encore autoriser son largage. The secondary thermal insulation barrier 6 is in contact with the external environment of the tank 2, in particular with a support structure. In the case where the tank is installed on a ship, the secondary thermal insulation barrier 6 is for example in contact with an internal hull of the ship. The secondary thermal insulation barrier 6 thus has an external face 18, turned towards the external environment of the tank 2. The secondary sealing membrane 8 is for its part in contact on the one hand with the thermal insulation barrier. secondary 6 and on the other hand with the primary thermal insulation barrier 10 which carries the primary waterproofing membrane 12. The thermal insulation barriers 6, 10 participate in maintaining the temperature inside the tank 2 while that the waterproofing membranes 8, 12 form an impermeable layer to the fluids that the tank 2 could contain. According to the invention, the tank 2 comprises a perforation device 32 comprising at least one actuating means 34 and a perforating member 36 of the vessel 2, the actuating means 34 being configured to set the actuating member in motion. perforation 36. This is how the actuating means 34 can hoist the perforation member 36, or even authorize its release.
Le dispositif de perforation 32 est configuré pour percer la membrane d’étanchéité primaire 12 et former un orifice reliant le volume interne de la barrière d’isolation thermique primaire 10 à un volume interne 15 de la cuve 2, afin de pouvoir évacuer rapidement le fluide infiltré dans l’espace primaire 14 de la pluralité de parois 4, lors du déchargement du fluide contenu dans la cuve 2, sans entraîner la destruction de la pluralité de parois 4 de la cuve 2. The perforation device 32 is configured to pierce the primary waterproofing membrane 12 and form an orifice connecting the internal volume of the primary thermal insulation barrier 10 to an internal volume 15 of the tank 2, in order to be able to rapidly evacuate the fluid. infiltrated into the primary space 14 of the plurality of walls 4, during the unloading of the fluid contained in the tank 2, without causing the destruction of the plurality of walls 4 of the tank 2.
La description du dispositif de perforation 32 et d’un procédé de perforation de la cuve 2 seront réalisés à la suite de la description à venir d’un tube 38 de la cuve 2 guidant l’organe de perforation 36 du dispositif de perforation 32. The description of the perforation device 32 and of a method for perforating the tank 2 will be made following the description to come of a tube 38 of the tank 2 guiding the perforating member 36 of the perforating device 32.
La cuve 2 comporte au moins un tube 38 traversant au moins l’une des parois de la cuve 2, cette paroi étant également dénommée dans la suite de la description par les termes « plafond de cuve 40 ». Le tube 38 s’étend longitudinalement entre une première extrémité 42 débouchant dans le volume interne 15 de la cuve 2 et une deuxième extrémité 44 débouchant à l’extérieur de la cuve 2, le tube 38 s’étendant sensiblement le long d’un axe vertical A entre ces deux extrémités. Dans la suite de la description, on utilisera les termes « extrémité intérieure 42 » pour faire également référence à la première extrémité 42 du tube 38 qui s’étend à l’intérieur de la cuve 2, ces deux expressions faisant référence au même objet. De même, on utilisera les termes « extrémité extérieure 44 » pour faire référence à la deuxième extrémité 44 du tube 38 qui est disposée à l’extérieur de la cuve 2, ces deux expressions faisant ainsi référence au même objet. The tank 2 comprises at least one tube 38 passing through at least one of the walls of the tank 2, this wall also being referred to in the remainder of the description by the terms "tank ceiling 40". The tube 38 extends longitudinally between a first end 42 opening into the internal volume 15 of the tank 2 and a second end 44 opening out to the outside of the tank 2, the tube 38 extending substantially along an axis vertical A between these two ends. In the remainder of the description, the terms "inner end 42" will be used to also refer to the first end 42 of the tube 38 which extends inside the tank 2, these two expressions referring to the same object. Likewise, the terms "outer end 44" will be used to refer to the second end 44 of the tube 38 which is disposed outside the vessel 2, these two expressions thus referring to the same object.
Le tube 38 comporte ainsi deux portions, une portion externe 46 qui s’étend entre l’extrémité extérieure 44 du tube 38 et le plafond de cuve 40, et une portion interne 48 qui s’étend entre l’extrémité intérieure 42 du tube 38 et le plafond de cuve 40. Avantageusement, l’extrémité intérieure 42 du tube 38 est proche d’une paroi opposée au plafond de cuve 40 par rapport à l’intérieur de la cuve 2, la paroi opposée étant dénommée dans la suite de la description « fond de cuve 50 ». Ainsi, la portion interne 48 du tube 38 s’étend depuis le plafond de cuve 40 par le tube 38 vers le fond de cuve 50, sans néanmoins toucher cette dernière. The tube 38 thus comprises two portions, an outer portion 46 which extends between the outer end 44 of the tube 38 and the tank ceiling 40, and an inner portion 48 which extends between the inner end 42 of the tube 38. and the tank ceiling 40. Advantageously, the inner end 42 of the tube 38 is close to a wall opposite the tank ceiling 40 with respect to inside the tank 2, the opposite wall being referred to in the remainder of the description as "tank bottom 50". Thus, the internal portion 48 of the tube 38 extends from the top of the tank 40 through the tube 38 towards the bottom of the tank 50, without however touching the latter.
Le tube 38 peut comprendre, au niveau de la portion externe 46, une entrée 52 d’un dispositif de mesure du niveau de fluide contenu par la cuve 2, le dispositif de mesure n’étant pas représenté sur les figures. Le tube 38 peut donc adapter une fonction de mesure du niveau de fluide dans la cuve, en plus de la fonction qu’il remplit à l’égard du dispositif de perforation 32 selon l’invention. The tube 38 may include, at the level of the outer portion 46, an inlet 52 of a device for measuring the level of fluid contained by the tank 2, the measuring device not being shown in the figures. The tube 38 can therefore adapt a function of measuring the level of fluid in the tank, in addition to the function that it fulfills with regard to the perforation device 32 according to the invention.
Ici, l’entrée 52 est distincte de l’extrémité extérieure 44 du tube 38. Cependant, un tube 38 tel que décrit ci-dessus présentant une entrée 52 du dispositif de mesure positionnée au niveau de l’extrémité extérieure 44 du tube 38 ne sortirait pas du cadre de l’invention. Here, the inlet 52 is separate from the outer end 44 of the tube 38. However, a tube 38 as described above having an inlet 52 of the measuring device positioned at the outer end 44 of the tube 38 does not. would not be outside the scope of the invention.
Le tube 38 est creux entre l’extrémité extérieure 44 et l’extrémité intérieure 42. En d’autres termes, le tube 38 présente un évidement 54 délimité par une face interne 33 du tube 38 s’étendant entre chacune de ses extrémités 42, 44, l’évidement 54 étant terminé par une bouche extérieure 56, au niveau de l’extrémité extérieure 44 du tube 38, et par une bouche intérieure 58, au niveau de l’extrémité intérieure 42 du tube 38. Lorsque le dispositif de perforation 32 est installé sur le tube 38, l’organe de perforation 36 coulisse dans l’évidement 54 du tube 38 entre chacune des extrémités 42, 44 du tube 38. The tube 38 is hollow between the outer end 44 and the inner end 42. In other words, the tube 38 has a recess 54 delimited by an inner face 33 of the tube 38 extending between each of its ends 42, 44, the recess 54 being terminated by an external mouth 56, at the level of the external end 44 of the tube 38, and by an internal mouth 58, at the level of the internal end 42 of the tube 38. When the perforating device 32 is installed on the tube 38, the perforating member 36 slides in the recess 54 of the tube 38 between each of the ends 42, 44 of the tube 38.
De plus, lorsque la cuve 2 contient un fluide, le tube 38 est au moins en partie immergée dans le fluide, ce dernier remplissant au moins en partie l’évidement 54 de la portion interne 48 du tube 38. De la sorte, le dispositif de mesure peut être positionné dans le tube 38 au niveau de la portion externe 46 de ce dernier et atteindre l’intérieur de la cuve 2 pour mesurer le niveau de fluide présent dans le tube 38, ce niveau étant assimilé à une quantité de fluide contenu dans la cuve 2. In addition, when the tank 2 contains a fluid, the tube 38 is at least partially immersed in the fluid, the latter at least partially filling the recess 54 of the internal portion 48 of the tube 38. In this way, the device measuring device can be positioned in the tube 38 at the level of the external portion 46 of the latter and reach the inside of the tank 2 to measure the level of fluid present in the tube 38, this level being assimilated to a quantity of fluid contained in the tank 2.
La bouche intérieure 58 du tube 38 est en regard d’au moins une partie du fond de cuve 50. Plus particulièrement, la bouche intérieure 58 est en regard d’une zone de perforation 60 de la positionnée sur le fond du cuve 50. La zone de perforation 60 est définie comme telle car la membrane d’étanchéité primaire 12 est d’une épaisseur inférieure ou égale au niveau de cette zone comparée au reste du fond de cuve 50, l’épaisseur de la membrane d’étanchéité primaire 12 se mesurant selon une direction perpendiculaire à un plan d’extension majoritaire de la membrane d’étanchéité primaire 12. La membrane d’étanchéité primaire 12 peut ainsi être perforée plus facilement par le dispositif de perforation 32. The interior mouth 58 of the tube 38 is opposite at least part of the bottom of the tank 50. More particularly, the interior mouth 58 is opposite a perforation zone 60 of the positioned on the bottom of the tank 50. The perforation zone 60 is defined as such because the primary waterproofing membrane 12 is of a thickness less than or equal to the level of this zone compared to the rest of the tank bottom 50, the thickness of the primary waterproofing membrane 12 being measured in a direction perpendicular to a major extension plane of the primary waterproofing membrane 12. The primary waterproofing membrane 12 can thus be perforated more easily by the perforation device 32.
La perforation de la membrane d’étanchéité primaire 12 ne doit cependant pas affecter l’espace secondaire 16, l’organe de perforation 36 ne devant ainsi pas atteindre la membrane d’étanchéité secondaire 8. The perforation of the primary waterproofing membrane 12 must not, however, affect the secondary space 16, the perforation member 36 thus not having to reach the secondary waterproofing membrane 8.
Pour cela, la zone de perforation 60 prend la forme d’un plot 62 qui émerge de la membrane d’étanchéité primaire 12 et qui comporte une zone plane 64. Le plot 62 s’étend vers le volume interne 15 de la cuve 2 de sorte que la zone plane 64 est en regard de la bouche intérieure 58 du tube 38. Dans cette configuration, l’organe de perforation 36 perfore la membrane d’étanchéité primaire 12 au niveau de la zone plane 64 sans atteindre la membrane d’étanchéité secondaire 8. For this, the perforation zone 60 takes the form of a stud 62 which emerges from the primary waterproofing membrane 12 and which comprises a flat zone 64. The stud 62 extends towards the internal volume 15 of the tank 2 of so that the flat zone 64 is opposite the interior mouth 58 of the tube 38. In this configuration, the perforation member 36 perforates the primary sealing membrane 12 at the level of the flat zone 64 without reaching the sealing membrane secondary 8.
Par ailleurs, le tube comprend un moyen d’arrêt 55 de la descente de l’organe de perforation 36 au niveau de la bouche intérieure 58 du tube. Ce moyen d’arrêt prend, par exemple, la forme d’un disque soudée s’étendant principalement dans un plan perpendiculaire à l’axe vertical A. Le disque comprend un trou avantageusement circulaire configuré pour qu’une partie de l’organe de perforation atteigne la membrane d’étanchéité primaire 12 sans pour autant que l’organe de perforation 36 sorte totalement du tube 38. Furthermore, the tube comprises a means 55 for stopping the descent of the perforating member 36 at the level of the inner mouth 58 of the tube. This stop means takes, for example, the form of a welded disc extending mainly in a plane perpendicular to the vertical axis A. The disc comprises an advantageously circular hole configured so that a part of the member of perforation reaches the primary waterproofing membrane 12 without the perforation member 36 completely coming out of the tube 38.
Selon l’invention, le tube 38 porte le dispositif de perforation 32 disposé au niveau de l’extrémité extérieure 44 de ce tube 38. According to the invention, the tube 38 carries the perforation device 32 disposed at the outer end 44 of this tube 38.
Le dispositif de perforation 32 comprend le moyen d’actionnement 34 et l’organe de perforation 36 de la cuve 2, le moyen d’actionnement 34 étant configuré pour générer un mouvement l’organe de perforation 36. Le moyen d’actionnement 34 permet ainsi de mettre en mouvement ou d’immobiliser l’organe de perforation 36. En d’autres termes, le mouvement de l’organe de perforation 36 est placé sous la dépendance du moyen d’actionnement 34. Le moyen d’actionnement 34 comprend au moins un bâti 66, un tambour 68 et un câble 70 reliant l’organe de perforation 36 au tambour 68. Le tambour 68 est configuré pour être mis en rotation autour d’un axe de rotation B sur l’ensemble des figures. La rotation du tambour 68 autour de l’axe de rotation B entraîne l’enroulement ou le déroulement du câble 70 autour du tambour 68. Le tambour 68 est mis en rotation ici manuellement, notamment grâce à une manivelle 72. The perforating device 32 comprises the actuating means 34 and the perforating member 36 of the tank 2, the actuating means 34 being configured to generate a movement of the perforating member 36. The actuating means 34 allows thus to set in motion or to immobilize the perforating member 36. In other words, the movement of the perforating member 36 is placed under the control of the actuating means 34. The actuating means 34 comprises at least a frame 66, a drum 68 and a cable 70 connecting the perforating member 36 to the drum 68. The drum 68 is configured to be rotated about an axis of rotation B on all the figures. The rotation of the drum 68 around the axis of rotation B causes the winding or unwinding of the cable 70 around the drum 68. The drum 68 is rotated here manually, in particular by means of a crank 72.
Tel qu’illustré plus particulièrement sur la figure 2, le moyen d’actionnement 34 de l’organe de perforation 36 comprend un système manuel de mise en rotation du tambour 68, ce système manuel comprenant au moins la manivelle 72. Le moyen d’actionnement 34 du dispositif de perforation 32 peut alternativement être motorisé voire automatisé sans pour autant sortir de cadre de l’invention. As illustrated more particularly in FIG. 2, the actuating means 34 of the perforating member 36 comprises a manual system for rotating the drum 68, this manual system comprising at least the crank 72. The means for rotating the drum 68. actuation 34 of the perforation device 32 can alternatively be motorized or even automated without thereby departing from the scope of the invention.
La manivelle 72 s’étend le long d’un axe transversal C perpendiculaire à l’axe vertical A entre la poignée 74 et le bout intérieur 76 de la manivelle 72. La poignée 74 de la manivelle 72 permet à l’utilisateur de mettre en mouvement le moyen d’actionnement 34 du dispositif de perforation 32, notamment en entraînant en rotation la manivelle 72 autour de l’axe transversal C. Le bout intérieur 76 de la manivelle 72 comprend une roue dentée 78 du tambour 68, et est maintenu en position par un premier palier de rotation 80 du bâti 66. La manivelle 72 est également soutenu en plus du premier palier de rotation 80 par un deuxième palier de rotation 82 du bâti 66, ce deuxième palier de rotation 82 étant en contact avec la manivelle 72 entre la poignée 74 et le bout intérieur 76 de la manivelle 72. Ces paliers de rotation de la manivelle 72 sur le bâti 66 assurent le maintien de la rotation de la manivelle 72 autour de l’axe transversal C. The crank 72 extends along a transverse axis C perpendicular to the vertical axis A between the handle 74 and the inner end 76 of the crank 72. The handle 74 of the crank 72 allows the user to put in movement the actuating means 34 of the perforating device 32, in particular by rotating the crank 72 around the transverse axis C. The inner end 76 of the crank 72 comprises a toothed wheel 78 of the drum 68, and is held in place. position by a first rotation bearing 80 of the frame 66. The crank 72 is also supported in addition to the first rotation bearing 80 by a second rotation bearing 82 of the frame 66, this second rotation bearing 82 being in contact with the crank 72 between the handle 74 and the inner end 76 of the crank 72. These bearings for rotation of the crank 72 on the frame 66 ensure that the rotation of the crank 72 is maintained around the transverse axis C.
Le tambour 68 du moyen d’actionnement 34 comprend un élément entraîné 84 en rotation par la roue dentée 78 de la manivelle 72, l’élément entraîné 84 étant par exemple un pignon. L’élément entraîné 84 est configuré pour pouvoir être en rotation autour de l’axe de rotation B du tambour 68. Ainsi, lorsque la manivelle 72 est mise en rotation autour de l’axe transversal C par un utilisateur, la roue dentée 78 de la manivelle 72 entraîne en rotation autour de l’axe de rotation B l’élément entraîné 84 du tambour 68 et le tambour 68. Le sens de rotation de la manivelle 72 autour de l’axe transversal C influe sur le sens de rotation du tambour 68. The drum 68 of the actuating means 34 comprises an element driven 84 in rotation by the toothed wheel 78 of the crank 72, the driven element 84 being for example a pinion. The driven element 84 is configured to be able to be rotated about the axis of rotation B of the drum 68. Thus, when the crank 72 is rotated about the transverse axis C by a user, the toothed wheel 78 of the crank 72 rotates around the axis of rotation B the driven element 84 of the drum 68 and the drum 68. The direction rotation of the crank 72 around the transverse axis C influences the direction of rotation of the drum 68.
Le tambour 68 comprend en plus de l’élément entraîné 84 un arbre 86 s’étendant entre un premier disque latéral 85 et un deuxième disque latéral 87, les disques latéraux 85, 87 étant de diamètre supérieur à celui de l’arbre 86. Les disques latéraux 85, 87 étant symétrique l’un par à l’autre par rapport à l’arbre 86, une caractéristique pour l’un des disques latéraux 85, 87 pourra être appliquée à l’autre disque latéral 85, 87. Le centre du tambour 68, le centre de l’arbre 86, le centre des disques latéraux 85, 87 et l’axe de rotation B sont confondus. L’arbre 86 du tambour 68 permet de fixer le tambour 68 au bâti 66, tout en autorisant la rotation du tambour 68 autour de l’axe de rotation B. The drum 68 comprises in addition to the driven element 84 a shaft 86 extending between a first side disc 85 and a second side disc 87, the side discs 85, 87 being of greater diameter than that of the shaft 86. The side discs 85, 87 are larger in diameter than that of the shaft 86. side discs 85, 87 being symmetrical to each other with respect to the shaft 86, a characteristic for one of the side discs 85, 87 can be applied to the other side disc 85, 87. The center of the drum 68, the center of the shaft 86, the center of the side discs 85, 87 and the axis of rotation B are coincident. The shaft 86 of the drum 68 secures the drum 68 to the frame 66, while allowing the rotation of the drum 68 around the axis of rotation B.
Le câble 70 s’enroule autour de l’arbre 86 du tambour 68 entre les disques latéraux 85, 87, ces derniers guidant le câble 70 lorsque celui-ci est enroulé ou déroulé du tambour. Le premier disque latéral 85, tout comme le deuxième disque latéral 87 présente au moins un orifice de positionnement 88. L’orifice de positionnement 88 est positionné ici entre le centre du premier disque latéral 85 et un bord périphérique 90 du premier disque latéral 85, l’orifice de positionnement 88 prenant globalement la forme d’un trou oblong dont la dimension la plus grande s’étend dans une direction radiale du tambour. Tel qu’illustré sur la figure 2, le premier disque latéral 85 comprend une pluralité d’orifices de positionnement 88, chacun des orifices 88 étant formé au travers du premier disque latéral 85 du tambour 68 et réparti angulairement autour de l’axe de rotation B du tambour 68. The cable 70 winds around the shaft 86 of the drum 68 between the side discs 85, 87, the latter guiding the cable 70 as it is wound up or unwound from the drum. The first side disc 85, like the second side disc 87 has at least one positioning hole 88. The positioning hole 88 is positioned here between the center of the first side disc 85 and a peripheral edge 90 of the first side disc 85, the positioning orifice 88 generally taking the form of an oblong hole, the largest dimension of which extends in a radial direction of the drum. As illustrated in FIG. 2, the first lateral disc 85 comprises a plurality of positioning orifices 88, each of the orifices 88 being formed through the first lateral disc 85 of the drum 68 and distributed angularly around the axis of rotation. B of drum 68.
Le tambour 68 comprend au moins une encoche 160 avantageusement colorée sur un des bords périphériques 90 d’un des disques latéraux 85, 87, l’encoche 160 étant conçu pour être au moins partiellement visible par un utilisateur du dispositif de perforation 32. Alternativement, le tambour 68 comprend une encoche 160 sur chaque disque latéral 85, 87 du tambour 68 pour que l’utilisateur puisse repérer ou compter les tours de tambour en étant disposé d’un côté comme de l’autre. The drum 68 comprises at least one advantageously colored notch 160 on one of the peripheral edges 90 of one of the lateral discs 85, 87, the notch 160 being designed to be at least partially visible by a user of the perforating device 32. Alternatively, the drum 68 includes a notch 160 on each side disc 85, 87 of the drum 68 so that the user can locate or count the revolutions of the drum while being disposed on either side.
Le moyen d’actionnement 34 comprend également un moyen de blocage 92 de la rotation du tambour 68, le moyen de blocage 92 étant configuré pour bloquer ou libérer la mise en mouvement de l’organe de perforation 36. Plus particulièrement, le moyen de blocage 92 coopère avec l’orifice de positionnement 88 pour bloquer la rotation du tambour 68 autour de l’axe de rotation B, le moyen de blocage 92 s’étendant par exemple au moins en partie dans l’orifice de positionnement 88. The actuating means 34 also comprises a means 92 for blocking the rotation of the drum 68, the blocking means 92 being configured to block or release the setting. movement of the perforating member 36. More particularly, the blocking means 92 cooperates with the positioning orifice 88 to block the rotation of the drum 68 around the axis of rotation B, the blocking means 92 extending through example at least partly in the positioning hole 88.
Le moyen de blocage 92, tel qu’illustré sur la figure 4, comporte une poignée 94 avantageusement rectangulaire et une tige 96 s’étendant de la poignée 94 vers une extrémité d’insertion 98 du moyen de blocage 92 dans un orifice de positionnement 88 du tambour 68. La poignée 94 est une zone par laquelle l’utilisateur prend en main le moyen de blocage 92, la tige 96 étant quant à elle destinée à être logée dans l’orifice de positionnement 88. En effet, une portion de la tige 96 s’étendant depuis l’extrémité d’insertion 98 vers la poignée 94 se loge dans l’orifice de positionnement 88 du tambour 68, bloquant alors la rotation du tambour 68 autour de l’axe de rotation B. The locking means 92, as illustrated in FIG. 4, comprises an advantageously rectangular handle 94 and a rod 96 extending from the handle 94 towards an insertion end 98 of the locking means 92 in a positioning hole 88. of the drum 68. The handle 94 is an area through which the user takes hold of the locking means 92, the rod 96 being for its part intended to be housed in the positioning orifice 88. Indeed, a portion of the rod 96 extending from the insertion end 98 towards the handle 94 fits in the positioning hole 88 of the drum 68, then blocking the rotation of the drum 68 about the axis of rotation B.
Pour libérer la rotation du tambour 68 et ainsi autoriser la chute de l’organe de perforation, le moyen de blocage 92 est retiré manuellement du tambour 68. Pour faciliter son extraction du tambour 68, le moyen de blocage 92 comporte un manchon 100 s’étendant depuis l’extrémité d’insertion 98 vers la poignée 94, favorisant le glissement de la tige 96 dans l’orifice de positionnement 88, le manchon 100 étant constitué au moins en partie d’une matière synthétique comme du polyéthylène à haute densité (PE-HD) ou du polytétrafluoroéthylène (PTFE), autrement appelé Téflon . Cette matière a pour caractéristique de diminuer les forces de frottement entre le moyen de blocage 92 et le tambour 68. La présence du manchon 100 autour de la tige 96 au niveau de l’extrémité d’insertion 98 facilite l’extraction du moyen de blocage 92 de l’orifice de positionnement 88 du tambour 68. Compte tenu du poids nécessairement important de l’organe de perforation pour que celui réalise sa mission dans un environnement liquide, un tel manchon 100 réduit l’effort nécessaire pour extraite le moyen de blocage 92 de l’orifice de positionnement 88.To release the rotation of the drum 68 and thus allow the fall of the perforating member, the locking means 92 is manually withdrawn from the drum 68. To facilitate its extraction from the drum 68, the locking means 92 comprises a sleeve 100 s' extending from the insertion end 98 towards the handle 94, promoting the sliding of the rod 96 in the positioning hole 88, the sleeve 100 being made at least in part of a synthetic material such as high density polyethylene ( PE-HD) or polytetrafluoroethylene (PTFE), otherwise called Teflon. This material has the characteristic of reducing the frictional forces between the locking means 92 and the drum 68. The presence of the sleeve 100 around the rod 96 at the level of the insertion end 98 facilitates the extraction of the locking means. 92 of the positioning orifice 88 of the drum 68. Taking into account the necessarily great weight of the perforating member so that it performs its mission in a liquid environment, such a sleeve 100 reduces the effort required to extract the locking means. 92 of the positioning hole 88.
Comme mentionné auparavant, le tambour 68 est solidaire du câble 70, le tambour 68 entraînant lors de sa rotation autour de l’axe de rotation B l’enroulement ou le déroulement du câble 70 autour du tambour 68. Lorsque le moyen de blocage 92 est logé dans l’orifice de positionnement 88, l’enroulement ou le déroulement du câble 70 ne peut alors pas se produire. As mentioned previously, the drum 68 is integral with the cable 70, the drum 68 causing during its rotation around the axis of rotation B the winding or unwinding of the cable 70 around the drum 68. When the locking means 92 is housed in the orifice of positioning 88, the winding or unwinding of the cable 70 cannot then occur.
Tel illustré sur la figure 2, le câble 70 du moyen d’actionnement 34 comprend une première extrémité 102 solidaire du tambour 68 et une deuxième extrémité 104 solidaire de l’organe de perforation 36. La première extrémité 102 du câble 70 est solidaire du tambour 68 au niveau de l’arbre 86 du tambour 68. As illustrated in Figure 2, the cable 70 of the actuating means 34 comprises a first end 102 integral with the drum 68 and a second end 104 integral with the perforating member 36. The first end 102 of the cable 70 is integral with the drum 68 at the level of the shaft 86 of the drum 68.
Le moyen d’actionnement 34 comporte optionnellement un élément de guidage 112 du câble 70, optimisant l’enroulement ou le déroulement du câble 70 autour du tambour 68. The actuating means 34 optionally comprises a guide element 112 of the cable 70, optimizing the winding or unwinding of the cable 70 around the drum 68.
Le moyen d’actionnement 34 comprend optionnellement un galet de renvoi 114, avantageusement un arbre, autour duquel peut glisser le câble 70. The actuating means 34 optionally comprises a return roller 114, advantageously a shaft, around which the cable 70 can slide.
Le bâti 66 du moyen d’actionnement 34 comprend une pluralité de flancs, dont un premier flanc 115 est notamment visible sur la figure 2, et une bride de fixation 118. La bride de fixation 118 du bâti 66 s’étend principalement dans un plan sensiblement perpendiculaire à l’axe vertical A. La pluralité de flancs du bâti 66 et la bride de fixation 118 délimite ainsi un espace 116 dans lequel sont notamment logés au moins partiellement le tambour 68 et le câble 70. L’espace 116 du bâti 66 est en communication avec l’environnement extérieur du bâti 66au niveau de la bride de fixation 118, permettant à au moins une partie du câble 70 d’être à l’extérieur du bâti 66. En effet, la première extrémité 102 du câble 70 reliée au tambour 68 se positionne à l’intérieur du bâti 66 dans l’espace 116 et la deuxième extrémité 104 du câble 70 se positionne à l’extérieur du bâti 66, le câble 70 traversant en partie l’espace 116 du bâti 66. La deuxième extrémité 104 du câble 70 est solidaire de l’organe de perforation 36. The frame 66 of the actuating means 34 comprises a plurality of sides, of which a first side 115 is in particular visible in FIG. 2, and a fixing flange 118. The fixing flange 118 of the frame 66 extends mainly in a plane. substantially perpendicular to the vertical axis A. The plurality of sides of the frame 66 and the fixing flange 118 thus delimits a space 116 in which the drum 68 and the cable 70 are housed in particular at least partially. The space 116 of the frame 66 is in communication with the external environment of the frame 66 at the level of the fixing flange 118, allowing at least part of the cable 70 to be outside the frame 66. Indeed, the first end 102 of the cable 70 connected the drum 68 is positioned inside the frame 66 in the space 116 and the second end 104 of the cable 70 is positioned outside the frame 66, the cable 70 partly passing through the space 116 of the frame 66. The second end 104 of the cable 70 is integral with the perforation 36.
La bride de fixation 118 du bâti 66 est destinée à être en contact avec l’extrémité extérieure 44 du tube 38. Pour cela, la bride de fixation 118 du bâti 66 est positionnée en regard d’une bride de fixation de la bouche extérieure 56 du tube 38, la bride de fixation 118 du bâti 66 et la bride de fixation 120 du tube 38 étant destinées à coopérer l’une avec l’autre pour rendre solidaire le bâti 66 du tube 38. Cet assemblage assure la fixation du dispositif de perforation 32 sur le tube 38. Cet assemblage réalise également une étanchéité entre la bride de fixation 118 du bâti 66 et la bride de fixation 120 du tube 38. The fixing flange 118 of the frame 66 is intended to be in contact with the outer end 44 of the tube 38. For this, the fixing flange 118 of the frame 66 is positioned opposite a fixing flange of the outer cover 56. of the tube 38, the fixing flange 118 of the frame 66 and the fixing flange 120 of the tube 38 being intended to cooperate with each other in order to make the frame 66 integral with the tube 38. This assembly secures the fixing device. perforation 32 on the tube 38. This assembly also provides a seal between the fixing flange 118 of the frame 66 and the fixing flange 120 of the tube 38.
Une fois le bâti 66 monté sur le tube 38 au niveau de l’extrémité extérieure 44 du tube 38, au moins une partie du câble 70 et l’organe de perforation 36 se positionne dans la partie creuse 54 du tube 38, cette partie du câble 70 et l’organe de perforation 36 s’alignant sensiblement le long de l’axe vertical A, l’élément pivot 114 assurant le positionnement de l’organe de perforation 36 le long de cet axe, comme qu’illustré sur la figure 2. Positionné de la sorte, l’organe de perforation 36 disposé dans le tube 38 est retenu en suspension au niveau de la deuxième extrémité 104 du câble 70. La rotation du tambour 68, provoquant l’enroulement ou le déroulement du câble 70 autour du tambour 68, entraîne également le rapprochement ou l’éloignement de l’organe de perforation 36 de l’extrémité extérieure 44 et/ou de l’extrémité intérieure 42 du tube 38. Once the frame 66 is mounted on the tube 38 at the level of the outer end 44 of the tube 38, at least part of the cable 70 and the perforating member 36 is positioned in the hollow part 54 of the tube 38, this part of the cable 70 and the perforating member 36 aligning substantially along the vertical axis A, the pivot member 114 ensuring the positioning of the perforating member 36 along this axis, as illustrated in the figure 2. Positioned in this way, the perforating member 36 disposed in the tube 38 is retained in suspension at the level of the second end 104 of the cable 70. The rotation of the drum 68, causing the winding or unwinding of the cable 70 around. of the drum 68, also causes the approximation or removal of the perforating member 36 from the outer end 44 and / or the inner end 42 of the tube 38.
Selon l’exemple illustré sur la figure 3, l’organe de perforation 36 comprend au moins une tête de perforation 122 et un corps 124, chacun s’étendant l’un à la suite de l’autre. Plus précisément, le corps 124 de l’organe de perforation 36 s’étend longitudinalement entre une première extrémité longitudinale 126 solidaire de la tête de perforation 122 et une deuxième extrémité longitudinale 129 solidaire de la deuxième extrémité 104 du câble 70. On comprend que le câble 70 est ainsi opposé à la tête de perforation 122 par rapport au corps 124 de l’organe de perforation 36. According to the example illustrated in Figure 3, the perforator 36 comprises at least one perforation head 122 and a body 124, each extending one after the other. More specifically, the body 124 of the perforation member 36 extends longitudinally between a first longitudinal end 126 integral with the perforation head 122 and a second longitudinal end 129 integral with the second end 104 of the cable 70. It is understood that the cable 70 is thus opposed to the perforation head 122 relative to the body 124 of the perforation member 36.
Le corps 124 comprend un arbre 128 délimité longitudinalement par la première extrémité longitudinale 126 et par la deuxième extrémité longitudinale 129 du corps 124, en s’étendant le long de l’axe vertical A. L’arbre 128 prend ici globalement la forme d’un cylindre dont le centre est confondu avec l’axe vertical A. Par ailleurs, c’est plus particulièrement l’arbre 128 du corps 124 qui, au niveau de chacune de ses extrémités, est solidaire du câble 70 et de la tête de perforation 122. The body 124 comprises a shaft 128 delimited longitudinally by the first longitudinal end 126 and by the second longitudinal end 129 of the body 124, extending along the vertical axis A. The shaft 128 here generally takes the form of a cylinder whose center coincides with the vertical axis A. Moreover, it is more particularly the shaft 128 of the body 124 which, at each of its ends, is secured to the cable 70 and to the perforation head 122.
L’arbre 128 comprend une rainure 130 s’étendant de la périphérie de l’arbre 128 jusqu’au centre du cylindre au niveau de la deuxième extrémité longitudinale 129 du corps 124. Cette rainure 130 facilite le montage du câble 70 sur l’arbre 128 du corps 124. Selon un autre mode de réalisation, l’arbre 128 de l’organe de perforation 36 peut comprendre un anneau de fixation positionné plus particulièrement au niveau de la deuxième extrémité longitudinale 129 sur lequel peut être fixé le câble 70. The shaft 128 includes a groove 130 extending from the periphery of the shaft 128 to the center of the cylinder at the second longitudinal end 129 of the body 124. This groove 130 facilitates the mounting of the cable 70 on the shaft. 128 of body 124. According to another embodiment, the shaft 128 of the perforation member 36 can comprise a fixing ring positioned more particularly at the level of the second longitudinal end 129 on which the cable 70 can be fixed.
Le corps 124 porte également une pluralité d’ailes 132, chacune de ces ailes émergeant radialement de l’arbre 128 du corps 124. Chaque aile de la pluralité d’ailes 132 s’étend longitudinalement entre la première extrémité longitudinale 126 et la deuxième extrémité longitudinale 129 du corps 124 et perpendiculairement à l’arbre 128 vers l’extérieur de l’organe de perforation 36. En d’autres termes, chaque aile de la pluralité d’ailes 132 s’étend depuis l’arbre 128 du corps 124 vers l’extérieur de l’organe de perforation 36 principalement dans un plan dans lequel l’axe vertical A s’inscrit. The body 124 also carries a plurality of wings 132, each of these wings emerging radially from the shaft 128 of the body 124. Each wing of the plurality of wings 132 extends longitudinally between the first longitudinal end 126 and the second end. longitudinal 129 of the body 124 and perpendicular to the shaft 128 outwardly of the perforator 36. In other words, each wing of the plurality of wings 132 extends from the shaft 128 of the body 124. towards the outside of the perforation member 36 mainly in a plane in which the vertical axis A is inscribed.
Chaque aile de la pluralité d’ailes 132 forme un flanc plat rectangulaire présentant trois bords libres. Un premier et un deuxième bords libres 134, 136 participent à délimiter chaque aile au niveau de la première extrémité longitudinale 126 et de la deuxième extrémité longitudinale 129 du corps 124. Ainsi, le premier et deuxième bords libres 134, 136, de chaque aile s’étend sensiblement perpendiculairement à l’axe vertical A. Chaque aile de la pluralité d’ailes 132 comprend un troisième bord libre 138 avantageusement parallèle à l’axe vertical A et s’étendant au moins en partie entre le premier bord 134 et le deuxième bord 136 de chaque aile de la pluralité d’ailes 132. Each wing of the plurality of wings 132 forms a rectangular flat sidewall with three free edges. A first and a second free edges 134, 136 participate in delimiting each wing at the level of the first longitudinal end 126 and of the second longitudinal end 129 of the body 124. Thus, the first and second free edges 134, 136, of each wing s 'extends substantially perpendicular to the vertical axis A. Each wing of the plurality of wings 132 comprises a third free edge 138 advantageously parallel to the vertical axis A and extending at least in part between the first edge 134 and the second edge 136 of each wing of the plurality of wings 132.
Dans l’exemple illustré sur la figure 3, la pluralité d’ailes 132 compte six ailes réparties de sorte qu’un secteur angulaire entre chacune des ailes de la pluralité d’ailes 132 soit régulier.In the example illustrated in Figure 3, the plurality of wings 132 has six wings distributed so that an angular sector between each of the wings of the plurality of wings 132 is regular.
On comprend ainsi que la distance séparant le troisième bord libre 138 de deux ailes adjacentes de la pluralité d’ailes 132 est égale quel que soit les ailes adjacentes de la pluralité d’ailes 132 choisies pour effectuer cette mesure, la distance se mesurant perpendiculairement à l’axe vertical A. Selon un autre mode de réalisation, la pluralité d’ailes 132 comprend au moins trois ailes. Lorsque le corps 124 comporte trois ailes, elles sont réparties autour de l’arbre 128 du corps 124 de sorte à former des angles de sensiblement 120 degrés. Le troisième bord libre 138 de chaque aile de la pluralité d’ailes 132 délimite au moins en partie une circonférence du corps 124, en s’inscrivant dans un cercle qui matérialise cette circonférence. It is thus understood that the distance separating the third free edge 138 from two adjacent wings of the plurality of wings 132 is equal regardless of the adjacent wings of the plurality of wings 132 chosen to perform this measurement, the distance being measured perpendicularly to the vertical axis A. According to another embodiment, the plurality of wings 132 comprises at least three wings. When the body 124 has three wings, they are distributed around the shaft 128 of the body 124 so as to form angles of substantially 120 degrees. The third free edge 138 of each wing of the plurality of wings 132 at least partially delimits a circumference of the body 124, being inscribed in a circle which materializes this circumference.
Le troisième bord libre 138 de chaque aile de la pluralité d’ailes 132 porte un revêtement 140 favorisant le glissement du corps 124 dans le tube 38. Ce revêtement 140 s’étend avantageusement du premier bord 134 jusqu’au deuxième bord 136 de chaque aile, recouvrant ainsi l’ensemble du troisième bord libre 138 de chaque aile. Le revêtement 140 est en matière synthétique, tel que du polyéthylène à haute densité (HD-PE) ou du polytétrafluoroéthylène (PTFE), autrement appelé Téflon , afin de diminuer les forces de frottement entre le troisième bord libre 138 de chaque aile de la pluralité d’ailes 132 de l’organe de perforation 36 et une face interne le tube 38. En dehors du revêtement 140, l’organe de perforation 36 est avantageusement en acier inoxydable, afin que son poids soit suffisant pour permettre la perforation de la membrane d’étanchéité primaire 12 au niveau de la zone de perforation 60. The third free edge 138 of each wing of the plurality of wings 132 carries a coating 140 promoting the sliding of the body 124 in the tube 38. This coating 140 advantageously extends from the first edge 134 to the second edge 136 of each wing. , thus covering the whole of the third free edge 138 of each wing. The coating 140 is made of a synthetic material, such as high density polyethylene (HD-PE) or polytetrafluoroethylene (PTFE), otherwise called Teflon, in order to decrease the frictional forces between the third free edge 138 of each wing of the plurality. wings 132 of the perforation member 36 and an internal face of the tube 38. Apart from the coating 140, the perforation member 36 is advantageously made of stainless steel, so that its weight is sufficient to allow perforation of the membrane primary seal 12 at the perforation zone 60.
Le corps 124 porte au niveau de sa deuxième extrémité longitudinale 129 un disque 142 empêchant le passage du câble 70 au niveau de la pluralité d’ailes 132 lorsque l’organe de perforation 36 est dans l’évidement 54 du tube 38. En effet, lorsque l’organe de perforation 36 est stoppé à la fin de sa chute, le tambour 68 continue à être entraîné en rotation par le poids du câble 70. Une partie du câble 70 s’accumule sur le disque 142, ce dernier entravant le passage du câble 70 entre la pluralité d’ailes 132 et la face interne 33 du tube 38. Le disque 142 s’étend principalement dans un plan perpendiculaire à l’axe vertical A, cet axe étant confondu avec le centre du disque 142. The body 124 carries at its second longitudinal end 129 a disc 142 preventing the passage of the cable 70 at the level of the plurality of wings 132 when the perforating member 36 is in the recess 54 of the tube 38. Indeed, when the perforating member 36 is stopped at the end of its fall, the drum 68 continues to be driven in rotation by the weight of the cable 70. A part of the cable 70 accumulates on the disc 142, the latter hindering the passage of the cable 70 between the plurality of wings 132 and the internal face 33 of the tube 38. The disc 142 extends mainly in a plane perpendicular to the vertical axis A, this axis coinciding with the center of the disc 142.
Le disque 142 présente une face supérieure 144 et une face inférieure, non visible sur les figures, opposées l’une par rapport à l’autre, la face inférieure étant tournée vers l’arbre 128 et vers la pluralité d’ailes 132 du corps 124. Par ailleurs, le diamètre du disque 142 est égal ou inférieur à un diamètre dans lequel s’inscrivent les troisièmes bords libres 138 de la pluralité d’ailes 132. Cependant, le diamètre du disque 142 doit être suffisamment grand pour empêcher le câble 70 de passer dans un espace entre un bord périphérique 148 du disque 142 et une surface interne du tube 38. The disc 142 has an upper face 144 and a lower face, not visible in the figures, opposite to each other, the lower face facing towards the shaft 128 and towards the plurality of wings 132 of the body. 124. On the other hand, the diameter of the disc 142 is equal to or less than a diameter in which the third free edges 138 of the plurality of wings 132 fit. However, the diameter of the disc 142 must be large enough to accommodate it. preventing cable 70 from passing through a space between a peripheral edge 148 of disc 142 and an inner surface of tube 38.
Le disque 142 comporte au moins une ouverture traversante 146, et avantageusement une pluralité d’ouvertures traversantes 146, ces ouvertures autorisant la circulation du fluide au travers du disque 142 lorsque ce dernier chute dans le tube 38. On comprend par le terme « traversante » que l’ouverture débouche sur la face inférieure et la face supérieure 144 du disque 142, reliant ainsi les deux faces du disque 142. Le disque 142 tel qu’illustré sur la figure 3 comprend une pluralité d’ouvertures traversantes 146 disposée proche de la périphérie radialement externe du disque 142. Les ouvertures de la pluralité d’ouvertures traversantes 146 peuvent être fermées sur leurs périphéries constituant ainsi des orifices traversants, ou ouvertes sur la circonférence externe du disque constituant alors des saignées traversantes. En effet, le disque 142 présente un bord périphérique 148 qui s’étend entre les faces supérieure et inférieure du disque 142, la pluralité d’ouvertures traversantes 146 étant ménagée proche de ce bord périphérique 148 sans pour autant être en contact avec celui-ci ici. The disc 142 comprises at least one through opening 146, and advantageously a plurality of through openings 146, these openings allowing fluid to flow through the disc 142 when the latter falls into the tube 38. The term “through” is understood to mean that the opening opens onto the lower face and the upper face 144 of the disc 142, thus connecting the two faces of the disc 142. The disc 142 as illustrated in FIG. 3 comprises a plurality of through openings 146 arranged close to the radially outer periphery of the disc 142. The openings of the plurality of through openings 146 can be closed on their peripheries thus constituting through orifices, or open on the outer circumference of the disc then constituting through grooves. Indeed, the disc 142 has a peripheral edge 148 which extends between the upper and lower faces of the disc 142, the plurality of through openings 146 being formed close to this peripheral edge 148 without however being in contact with the latter. here.
Le bord périphérique 148 présente une forme chanfreinée entre la face supérieure 144 et la face inférieure du disque 142. On comprend que le bord périphérique 148 présente avantageusement trois faces : une première face s’étendant dans un plan perpendiculaire au plan d’extension des faces supérieure 144 et inférieure du disque 142, une deuxième face assurant la liaison entre la face supérieure 144 et la première face du bord périphérique 148 et une troisième face assurant la liaison entre la face inférieure du disque 142 et la première face du bord périphérique 148. The peripheral edge 148 has a chamfered shape between the upper face 144 and the lower face of the disc 142. It is understood that the peripheral edge 148 advantageously has three faces: a first face extending in a plane perpendicular to the plane of extension of the faces. upper 144 and lower of the disc 142, a second face providing the connection between the upper face 144 and the first face of the peripheral edge 148 and a third face providing the connection between the lower face of the disc 142 and the first face of the peripheral edge 148.
Le disque 142 comprend une saignée 150 s’étendent depuis le bord périphérique 148 du disque 142 jusqu’au centre de celui-ci. La saignée 150 est ménagée de façon à être alignée avec la rainure 130 de l’arbre 128, la saignée 150 permettant, similairement à la rainure 130 de l’arbre 128, le montage du câble 70 sur l’organe de perforation 36. On peut ainsi monter le disque 142 sur l’organe de perforation 36 après l’avoir attaché au câble 70. Selon un autre mode de réalisation, le disque 142 comprend un orifice traversant fermé, au lieu de la saignée 150, à travers lequel passe le câble 70. The disc 142 includes a groove 150 extending from the peripheral edge 148 of the disc 142 to the center thereof. The groove 150 is formed so as to be aligned with the groove 130 of the shaft 128, the groove 150 allowing, similarly to the groove 130 of the shaft 128, the cable 70 to be mounted on the perforating member 36. It is possible to mount the cable 70 on the perforating member 36. can thus mount the disc 142 on the perforating member 36 after having attached it to the cable 70. According to another embodiment, the disc 142 comprises a closed through orifice, instead of the groove 150, through which the cable 70 passes.
Le disque 142 présente au moins un orifice de fixation 152 et avantageusement plusieurs orifices de fixation 152 permettant de rendre solidaire le disque 142 de l’arbre 128 du corps 124. Pour cela, le ou les orifices de fixation 152 coopèrent avec des moyens de fixation non représentés sur les figures, tels que des vis par exemple, pour fixer le disque 142 à l’arbre 128 du corps 124. The disc 142 has at least one fixing hole 152 and advantageously several fixing holes 152 making it possible to make the disc 142 integral with the shaft 128 of the body 124. For this, the fixing hole or holes 152 cooperate with fixing means. not shown in the figures, such as screws for example, to fix the disc 142 to the shaft 128 of the body 124.
L’organe de perforation 36 comprend la tête de perforation 122 prenant globalement la forme d’un cylindre 121 s’étendant entre un bord de liaison 154 et un cône de perforation 156. Le cylindre 121 présente au moins une gorge 123 s’étendant depuis le cône de perforation 156 vers le bord de liaison 154. The perforation member 36 comprises the perforation head 122 generally taking the form of a cylinder 121 extending between a connecting edge 154 and a perforation cone 156. The cylinder 121 has at least one groove 123 extending from it. the perforation cone 156 towards the connecting edge 154.
La tête de perforation 122 est solidaire du corps 124 au niveau du bord de liaison 154, ce dernier étant ainsi en contact avec la première extrémité longitudinale 126 du corps 124. Le cône de perforation 156 de la tête de perforation 122 présente une forme conique jusqu’à une pointe perforante 158. The perforation head 122 is integral with the body 124 at the level of the connecting edge 154, the latter thus being in contact with the first longitudinal end 126 of the body 124. The perforation cone 156 of the perforation head 122 has a conical shape up to 'to a piercing point 158.
On va maintenant décrire un procédé de perforation de la cuve 2 dans lequel l’organe de perforation 36 est mis en mouvement pour perforer une des parois de la pluralité de parois 4 de la cuve 2. We will now describe a method of perforating the tank 2 in which the perforating member 36 is set in motion to perforate one of the walls of the plurality of walls 4 of the tank 2.
Lorsqu’une fuite du fluide contenu dans la cuve 2 à travers la membrane d’étanchéité primaire 12 a été identifiée, un utilisateur met en place le dispositif de perforation 32 au niveau de la bouche d’entrée du tube 38 de la cuve 2, constituant ainsi une première étape du procédé de perforation. Le dispositif de perforation 32 est positionné au niveau de la bouche extérieur du tube 38 de sorte que l’espace 116 du bâti 66 soit en contact de la bouche extérieure 56 du tube 38 et qu’une partie du câble 70 et l’organe de perforation 36 soient disposés dans l’évidement 54 du tube 38 au niveau de l’extrémité extérieure 44 du tube 38. Le câble 70 est alors enroulé autour du tambour 68 pour maintenir l’organe de perforation 36 au niveau de l’extrémité extérieure 44 du tube 38. Une deuxième étape consiste à positionner l’organe de perforation 36 au niveau de l’extrémité intérieure 42 du tube 38. Pour cela, l’utilisateur tourne la manivelle 72 de sorte que le tambour 68 déroule le câble 70 entraînant la descente de l’organe de perforation 36 dans le tube 38 en direction de la paroi de fond de la cuve 2. La descente de l’organe de perforation 36 est ainsi contrôlé par l’utilisateur tournant la manivelle 72. Pour éviter tout largage prématuré de l’organe de perforation 36 lors de sa descente dans le tube 38, le tambour 69 comporte un système de freinage limitant la vitesse de rotation du tambour 68 et empêchant ainsi l’organe de perforation 36 d’être largué et de défoncer l’une des parois de la pluralité de parois 4 de la cuve 2. Ce système de freinage est réversible de sorte que l’utilisateur puisse le retirer lorsqu’il souhaite larguer l’organe de perforation 36. La descente contrôlée de l’organe de perforation 36 se réalise jusqu’à ce la pointe perforante 158 de l’organe de perforation 36 entre en contact avec la zone plane 64 du plot 62 du fond de cuve 50. When a leak of the fluid contained in the tank 2 through the primary sealing membrane 12 has been identified, a user places the perforation device 32 at the level of the inlet mouth of the tube 38 of the tank 2, thus constituting a first step of the perforation process. The perforation device 32 is positioned at the level of the outer mouth of the tube 38 so that the space 116 of the frame 66 is in contact with the outer mouth 56 of the tube 38 and that part of the cable 70 and the perforation 36 are disposed in the recess 54 of the tube 38 at the level of the outer end 44 of the tube 38. The cable 70 is then wound around the drum 68 to keep the perforator 36 at the level of the outer end 44 of tube 38. A second step consists in positioning the perforating member 36 at the level of the inner end 42 of the tube 38. For this, the user turns the crank 72 so that the drum 68 unwinds the cable 70 causing the descent of the cable. perforation member 36 in the tube 38 in the direction of the bottom wall of the tank 2. The descent of the perforation member 36 is thus controlled by the user turning the crank 72. To avoid any premature release of the member 36 during its descent into the tube 38, the drum 69 comprises a braking system limiting the rotational speed of the drum 68 and thus preventing the perforating member 36 from being released and breaking through one of the walls of the plurality of walls 4 of the tank 2. This braking system is reversible so that the user can remove it when he wishes to release the perforating member 36. The controlled descent of the perforating member 36 is carried out up to 'to this the piercing point 158 of the perforation member 36 comes into contact with the flat area 64 of the stud 62 of the tank bottom 50.
Une troisième étape du procédé de perforation consiste à hisser l’organe de perforation 36 dans le tube 38 à une hauteur de largage puis de bloquer le tambour 68 une fois l’organe de perforation 36 positionné à ladite hauteur. Ainsi, l’utilisateur remonte l’organe de perforation 36 à une hauteur déterminée qui dépend de facteurs comme l’épaisseur de membrane d’étanchéité primaire, ou encore la présence fluide dans le tube 38. A titre d’exemple, cette hauteur est de trois mètres, mesurée le long de l’axe vertical A. A third step of the perforation process consists of hoisting the perforating member 36 in the tube 38 to a release height and then blocking the drum 68 once the perforating member 36 is positioned at said height. Thus, the user raises the perforation member 36 to a determined height which depends on factors such as the thickness of the primary waterproofing membrane, or even the presence of fluid in the tube 38. By way of example, this height is three meters, measured along the vertical axis A.
Grâce à l’encoche 160, l’utilisateur peut compter le nombre de tours que le tambour 68 fait lorsque ce dernier est hissé avant largage. Dans l’exemple illustré ici, la dimension du tambour 68 est configurée pour que la circonférence du tambour 60 corresponde à environ un mètre, de sorte qu’un tour du tambour 68 en rotation entraîne l’enroulement ou le déroulement d’un mètre du câble 70. With the notch 160, the user can count the number of revolutions that the drum 68 makes when the latter is hoisted before release. In the example shown here, the size of the drum 68 is configured so that the circumference of the drum 60 is approximately one meter, so that one turn of the rotating drum 68 causes the winding or unwinding of one meter of the drum. cable 70.
Pour hisser l’organe de perforation 36 à trois mètres de la bouche intérieure 58 du tube 38, l’utilisateur entraîne en rotation le tambour 68 grâce à la manivelle 72 et compte, grâce à l’encoche 160, le nombre de tours effectués par le tambour 68 jusqu’à atteindre le nombre de trois. Lorsque l’organe de perforation 36 a atteint cette hauteur, l’utilisateur loge le moyen de blocage 92 dans le tambour 68 afin de bloquer la rotation du tambour 68. Une quatrième étape du procédé consiste à larguer l’organe de perforation 36. L’utilisateur libère ainsi le tambour 68 du moyen de blocage 92, l’organe de perforation 36 étant entraîné par son poids vers la zone plane 64 du plot 62 du fond de cuve 50. To hoist the perforating member 36 to three meters from the inner mouth 58 of the tube 38, the user drives the drum 68 in rotation thanks to the crank 72 and counts, thanks to the notch 160, the number of turns made by the drum 68 until it reaches the number of three. When the perforation member 36 has reached this height, the user accommodates the blocking means 92 in the drum 68 in order to block the rotation of the drum 68. A fourth step of the method consists in releasing the perforating member 36. The user thus releases the drum 68 from the locking means 92, the perforating member 36 being driven by its weight towards the flat area 64 of the stud 62 of the bottom. tank 50.
Le poids de l’organe de perforation 36 propulse à une vitesse suffisante la pointe perforante 158 de l’organe de perforation 158 vers la zone plane 64 du plot 62 du fond de cuve 50, générant ainsi une énergie cinétique. Lorsque la pointe perforante 158 entre en contact avec la zone plane 64, l’énergie cinétique est convertie en énergie mécanique pour que la pointe perforante 158 perfore la membrane d’étanchéité primaire 12 au niveau de la zone plane 64 du plot 62. Une fois la membrane d’étanchéité primaire 12 perforée, l’organe de perforation 36 est remonté par l’utilisateur jusqu’à l’extrémité extérieure 44 du tube 38. The weight of the perforator 36 propels at a sufficient speed the perforating tip 158 of the perforating member 158 towards the flat area 64 of the stud 62 of the tank bottom 50, thus generating kinetic energy. When the piercing tip 158 contacts the planar area 64, kinetic energy is converted into mechanical energy so that the piercing tip 158 perforates the primary waterproofing membrane 12 at the planar area 64 of the pad 62. Once the perforated primary waterproofing membrane 12, the perforation member 36 is raised by the user to the outer end 44 of the tube 38.
Une cinquième étape du procédé de perforation consiste à hisser ensuite l’organe de perforation 36 dans le tube 38. Si l’organe de perforation 36 n’a pas percé suffisamment la membrane d’étanchéité primaire 12 à la suite d’un premier essai, l’utilisateur recommence le procédé de perforation en positionnement de l’organe de perforation 36 à la hauteur déterminée depuis la bouche intérieure 58 du tube 38 et larguant à nouveau de l’organe de perforation 36 sur la membrane d’étanchéité primaire 12, constituant ainsi une cinquième étape du procédé de perforation. A fifth step of the perforation process then consists in hoisting the perforating member 36 into the tube 38. If the perforating member 36 has not sufficiently pierced the primary waterproofing membrane 12 following a first test , the user starts the perforation process again by positioning the perforation member 36 at the determined height from the interior mouth 58 of the tube 38 and again releasing from the perforation member 36 onto the primary waterproofing membrane 12, thus constituting a fifth step of the perforation process.
L’utilisateur peut ainsi recommencer le procédé de perforation, et plus particulièrement les deuxième, troisième et quatrième étapes, jusqu’à ce que la membrane d’étanchéité primaire 12 soit perforée. En d’autres termes, l’utilisateur répète ces trois étapes tant que le trou dans la membrane d’étanchéité primaire 12 n’est pas d’une surface suffisante pour que le fluide sorte très rapidement de couche d’isolation thermique primaire et rejoigne le volume interne 15 de la cuve 2. The user can thus start the perforation process again, and more particularly the second, third and fourth steps, until the primary waterproofing membrane 12 is perforated. In other words, the user repeats these three steps as long as the hole in the primary waterproofing membrane 12 is not of a sufficient area for the fluid to very quickly exit the primary thermal insulation layer and join the internal volume 15 of the tank 2.
Une fois la membrane d’étanchéité perforée, le déchargement du fluide contenu dans la cuve 2 peut être effectuée sans dégrader la paroi de la cuve 2. En effet, le gaz naturel liquide infiltré dans au moins une des parois 4 rejoint le volume interne 15 de la cuve 2 via la perforation réalisée par l’organe de perforation 36 dans la membrane d’étanchéité primaire 12. De plus, le fluide infiltré dans la barrière d’isolation thermique primaire 10 peut ainsi être récupérer, évitant ainsi tout risque de surpression à l’intérieur de la paroi de la cuve qui a été infiltrée. Une fois l’ensemble du gaz naturel liquide déchargé, la réparation de la fuite ainsi que la réparation de la perforation peuvent être assurées pour conférer à la cuve une nouvelle étanchéité. L’invention ne saurait toutefois se limiter aux moyens et configurations décrits et illustrés ici, et elle s’étend également à tout moyen ou configuration équivalents décrits et illustrés ici, et elle s’étend également à tout moyen ou configuration équivalents et à toute combinaison technique opérant de tels moyens. En particulier, le moyen d’actionnement 34 de l’organe de perforation peut être au moins partiellement motorisé, voire totalement automatisé sans pour autant sortir du cadre de l’invention. Once the waterproofing membrane has been perforated, the unloading of the fluid contained in the tank 2 can be carried out without damaging the wall of the tank 2. In fact, the liquid natural gas infiltrated into at least one of the walls 4 joins the internal volume 15. of the tank 2 via the perforation produced by the perforation member 36 in the primary waterproofing membrane 12. In addition, the fluid infiltrated into the primary thermal insulation barrier 10 can thus be recovered, thus avoiding any risk of overpressure inside the wall of the tank which has been infiltrated. Once all the liquid natural gas has been discharged, repair of the leak as well as repair of the perforation can be carried out to give the vessel a new seal. The invention cannot however be limited to the means and configurations described and illustrated here, and it also extends to any equivalent means or configuration described and illustrated here, and it also extends to any equivalent means or configuration and to any combination. technique operating such means. In particular, the actuating means 34 of the perforation member can be at least partially motorized, or even fully automated without departing from the scope of the invention.

Claims

REVENDICATIONS
1. Dispositif de perforation (32) pour une cuve (2) étanche et thermiquement isolante configurée pour contenir un fluide, caractérisé en ce que le dispositif de perforation (32) comprend un moyen d’actionnement (34) et un organe de perforation (36) de la cuve (2), le moyen d’actionnement (34) étant configuré pour générer un mouvement de l’organe de perforation (36). 1. Perforation device (32) for a sealed and thermally insulating vessel (2) configured to contain a fluid, characterized in that the perforation device (32) comprises an actuating means (34) and a perforation member ( 36) of the tank (2), the actuating means (34) being configured to generate a movement of the perforating member (36).
2. Dispositif de perforation (32) selon la revendication 1, dans lequel le moyen d’actionnement (34) comporte au moins un bâti (66), un tambour (68) et un câble (70) reliant l’organe de perforation (36) au tambour (68), le tambour (68) étant configuré pour être mis en rotation autour d’un axe de rotation (B) et entraîner l’enroulement ou le déroulement du câble (70) autour du tambour (68). 2. Perforation device (32) according to claim 1, wherein the actuating means (34) comprises at least a frame (66), a drum (68) and a cable (70) connecting the perforation member ( 36) to the drum (68), the drum (68) being configured to be rotated about an axis of rotation (B) and to drive the winding or unwinding of the cable (70) around the drum (68).
3. Dispositif de perforation (32) selon l’une quelconque des revendications précédentes, dans lequel l’organe de perforation (36) comprend au moins une tête de perforation (122) et un corps (124), chacun s’étendant longitudinalement l’un à la suite de l’autre. 3. A perforating device (32) according to any preceding claim, wherein the perforating member (36) comprises at least one perforating head (122) and a body (124), each extending longitudinally. 'one after the other.
4. Dispositif de perforation (32) selon la revendication 3, dans lequel le corps (124) présente une première extrémité longitudinale (126) solidaire de la tête de perforation (122) et une deuxième extrémité longitudinale (128) solidaire du câble (70). 4. Perforation device (32) according to claim 3, wherein the body (124) has a first longitudinal end (126) integral with the perforation head (122) and a second longitudinal end (128) integral with the cable (70). ).
5. Dispositif de perforation (32) selon l’une quelconque des revendications 3 ou 4, dans lequel le corps (124) comprend une pluralité d’ailes (132) et un arbre (128) duquel émerge radialement la pluralité d’ailes (132). A perforating device (32) according to any one of claims 3 or 4, wherein the body (124) comprises a plurality of wings (132) and a shaft (128) from which emerges the plurality of wings radially ( 132).
6. Dispositif de perforation (32) selon la revendication 5, dans lequel au moins une aile de la pluralité d’ailes (132) comprend une extrémité libre (138) délimitant au moins en partie une circonférence du corps (124) et possédant un revêtement (140) favorisant un glissement du corps (124). A perforating device (32) according to claim 5, wherein at least one wing of the plurality of wings (132) comprises a free end (138) defining at least in part a circumference of the body (124) and having a. coating (140) promoting sliding of the body (124).
7. Dispositif de perforation (32) selon l’une quelconque des revendications 4 à 6, dans lequel le corps (124) porte un disque (142) au niveau de sa deuxième extrémité longitudinale (128).7. Perforation device (32) according to any one of claims 4 to 6, wherein the body (124) carries a disc (142) at its second longitudinal end (128).
8. Dispositif de perforation (32) selon la revendication 7, dans lequel le disque (142) comporte au moins une ouverture traversante (146). 8. A perforation device (32) according to claim 7, wherein the disc (142) has at least one through opening (146).
9. Dispositif de perforation (32) selon l’une quelconque des revendications 7 ou 8, dans lequel le disque (142) est au moins en partie en matière favorisant son glissement. 9. Perforation device (32) according to any one of claims 7 or 8, wherein the disc (142) is at least partly made of material promoting its sliding.
10. Dispositif de perforation (32) selon l’une quelconque des revendications 7 à 9, dans lequel le disque (142) présente un diamètre inférieur ou égal à un diamètre dans lequel s’inscrivent les extrémités libres (138) de la pluralité d’ailes (132). 10. A perforation device (32) according to any one of claims 7 to 9, wherein the disc (142) has a diameter less than or equal to a diameter in which the free ends (138) of the plurality of fit. 'wings (132).
11. Dispositif de perforation (32) selon l’une quelconque des revendications précédentes en combinaison avec la revendication 2, dans lequel le moyen d’actionnement (34) comprend un moyen de blocage (92) de la rotation du tambour (68), le moyen de blocage (92) étant configuré pour libérer une chute de l’organe de perforation (36). 11. A perforation device (32) according to any one of the preceding claims in combination with claim 2, wherein the actuating means (34) comprises means (92) for blocking the rotation of the drum (68), the locking means (92) being configured to release a drop from the puncture member (36).
12. Cuve (2) étanche et thermiquement isolante configurée pour contenir un fluide, la cuve (2) comprenant une pluralité de parois (4), caractérisée en ce que la cuve (2) comporte un tube (38) traversant au moins l’une des parois de la cuve (2) et s’étendant entre une première extrémité (42) ménagée à l’intérieur de la cuve (2) et une deuxième extrémité (44) ménagée à l’extérieur de la cuve (2), la cuve (2) comprenant un dispositif de perforation (32) selon l’une quelconque des revendications précédentes. 12. Tank (2) sealed and thermally insulating configured to contain a fluid, the tank (2) comprising a plurality of walls (4), characterized in that the tank (2) comprises a tube (38) passing through at least the one of the walls of the tank (2) and extending between a first end (42) formed inside the tank (2) and a second end (44) formed outside the tank (2), the tank (2) comprising a perforation device (32) according to any one of the preceding claims.
13. Cuve (2) selon la revendication 12 en combinaison avec la revendication 2, dans lequel l’organe de perforation (36) est disposé dans le tube (38), le tambour (68) enroulant le câble (70) pour hisser l’organe de perforation (36). 13. Tank (2) according to claim 12 in combination with claim 2, wherein the perforating member (36) is disposed in the tube (38), the drum (68) winding the cable (70) to hoist the 'perforation member (36).
14. Cuve (2) selon l’une quelconque des revendications 12 ou 13 en combinaison avec la revendication 6, dans lequel l’organe de perforation (36) et le tube (38) sont configurés pour que l’organe de perforation (36) coulisse dans le tube (38). 14. The vessel (2) according to any one of claims 12 or 13 in combination with claim 6, wherein the perforating member (36) and the tube (38) are configured so that the perforating member (36 ) slides in the tube (38).
15. Cuve (2) selon l’une quelconque des revendications 12 à 14, dans lequel chaque paroi de la pluralité de parois (4) comporte successivement dans le sens de l’épaisseur depuis l’extérieur vers l’intérieur de la cuve (2), une barrière d’isolation thermique secondaire (6), une membrane d’étanchéité secondaire (8), une barrière d’isolation thermique primaire (10) et une membrane d’étanchéité primaire (12) et destinée à être en contact avec le fluide contenu dans le cuve (2), la membrane d’étanchéité primaire (12) présentant une zone de perforation (60) disposée en regard de l’extrémité du tube (38) débouchant à l’intérieur de la cuve (2). 15. Tank (2) according to any one of claims 12 to 14, wherein each wall of the plurality of walls (4) comprises successively in the direction of the thickness from the outside towards the inside of the tank ( 2), a secondary thermal insulation barrier (6), a secondary waterproofing membrane (8), a primary thermal insulation barrier (10) and a primary waterproofing membrane (12) and intended to be in contact with the fluid contained in the tank (2), the primary sealing membrane (12) having a perforation zone (60) arranged opposite the end of the tube (38) opening inside the tank (2) ).
16. Navire comprenant au moins une cuve (2) selon l’une quelconque des revendications 12 à16. Vessel comprising at least one tank (2) according to any one of claims 12 to
15. 15.
17. Procédé de perforation d’une cuve (2) équipant un navire selon la revendication précédente, caractérisé en ce qu’une première étape consiste à installer le dispositif de perforation (32) au niveau de la deuxième extrémité (44) du tube (38). 17. A method of perforating a tank (2) fitted to a ship according to the preceding claim, characterized in that a first step consists in installing the perforating device (32) at the level of the second end (44) of the tube ( 38).
18. Procédé de perforation d’une cuve (2) selon la revendication 17, dans lequel une deuxième étape consiste à coulisser l’organe de perforation (36) dans le tube (38) pour l’amener contre une paroi de fond (50) de la cuve (2). 18. A method of perforating a tank (2) according to claim 17, wherein a second step consists in sliding the perforating member (36) in the tube (38) to bring it against a bottom wall (50). ) of the tank (2).
19. Procédé de perforation d’une cuve (2) selon la revendication 18, dans lequel une troisième étape consiste à hisser l’organe de perforation (36) dans le tube (38) à une hauteur de largage, puis à bloquer un tambour (68) constitutif du dispositif de perforation (32) une fois l’organe de perforation (36) positionné à ladite hauteur de largage. 19. A method of perforating a tank (2) according to claim 18, wherein a third step consists in hoisting the perforating member (36) in the tube (38) to a release height, then in blocking a drum. (68) constituting the perforation device (32) once the perforation member (36) is positioned at said release height.
20. Procédé de perforation d’une cuve (2) selon la revendication 17 ou 19, dans lequel une quatrième étape consiste à larguer l’organe de perforation (36). 20. A method of perforating a tank (2) according to claim 17 or 19, wherein a fourth step consists in releasing the perforating member (36).
21. Procédé de perforation d’une cuve (2) selon la revendication 20, la cuve comprenant successivement dans le sens de l’épaisseur depuis l’extérieur vers l’in rérieur de la cuve (2), une barrière d’isolation thermique secondaire (6), une membrane d’étanchéité secondaire (8), une barrière d’isolation thermique primaire (10) et une membrane d’étanchéité primaire (12) et destinée à erre en contact avec le fluide contenu dans le cuve (2), procédé dans lequel la deuxième étape, la troisième étape, la quatrième étape sont répétées jusqu’à ce que la membrane d’étanchéité primaire (12) soir perforée. 21. A method of perforating a tank (2) according to claim 20, the tank comprising successively in the direction of the thickness from the outside towards the inside of the tank (2), a thermal insulation barrier secondary (6), a secondary waterproofing membrane (8), a primary thermal insulation barrier (10) and a primary waterproofing membrane (12) and intended to wander in contact with the fluid contained in the tank (2 ), a process in which the second step, the third step, the fourth step are repeated until the primary waterproofing membrane (12) is perforated.
PCT/FR2021/050444 2020-03-18 2021-03-18 Perforation means for a tank of natural gas in the liquid state WO2021186133A1 (en)

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KR1020217024511A KR102586601B1 (en) 2020-03-18 2021-03-18 Means for drilling tanks of liquid natural gas
KR1020237033428A KR102654638B1 (en) 2020-03-18 2021-03-18 Means for perforating a tank of natural gas in the liquid state
CN202180022932.4A CN115836177A (en) 2020-03-18 2021-03-18 Device for perforating a liquid natural gas tank

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FR2002626A FR3108384B1 (en) 2020-03-18 2020-03-18 Means of perforating a natural gas tank in the liquid state

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FR3138180A1 (en) * 2022-07-21 2024-01-26 Gaztransport Et Technigaz Waterproof tank comprising a perforation device

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FR3138180A1 (en) * 2022-07-21 2024-01-26 Gaztransport Et Technigaz Waterproof tank comprising a perforation device

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WO2021186133A4 (en) 2021-12-02
CN115836177A (en) 2023-03-21
KR20230143628A (en) 2023-10-12
FR3108384A1 (en) 2021-09-24
KR102586601B1 (en) 2023-10-06
FR3108384B1 (en) 2022-09-09
KR102654638B1 (en) 2024-04-03

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