WO2021122152A1 - Système de transfert de carburant en mer entre deux navires - Google Patents
Système de transfert de carburant en mer entre deux navires Download PDFInfo
- Publication number
- WO2021122152A1 WO2021122152A1 PCT/EP2020/085060 EP2020085060W WO2021122152A1 WO 2021122152 A1 WO2021122152 A1 WO 2021122152A1 EP 2020085060 W EP2020085060 W EP 2020085060W WO 2021122152 A1 WO2021122152 A1 WO 2021122152A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- tank
- watercraft
- inlet
- nozzle
- valve
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B27/00—Arrangement of ship-based loading or unloading equipment for cargo or passengers
- B63B27/24—Arrangement of ship-based loading or unloading equipment for cargo or passengers of pipe-lines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B27/00—Arrangement of ship-based loading or unloading equipment for cargo or passengers
- B63B27/30—Arrangement of ship-based loading or unloading equipment for transfer at sea between ships or between ships and off-shore structures
- B63B27/34—Arrangement of ship-based loading or unloading equipment for transfer at sea between ships or between ships and off-shore structures using pipe-lines
Definitions
- the invention relates to a system for transferring liquids, in particular fuel, from one watercraft to another watercraft, in particular to an unmanned watercraft.
- Refueling by means of a rigid boom system or by means of a probe and collecting funnel are known from aviation and have been in use for a long time.
- the takeover of fuel is also known in the shipping industry.
- task force suppliers are used to supply other ships in the fleet with fuel, among other things.
- a tank hose is laid between the ships so that the ship to be refueled can bunker fuel.
- the fuel can be for the watercraft itself or for aircraft used on the watercraft.
- a tank adapter is known from US 2010/0236657 A1.
- a device for occupying a ship is known from DE 2745927 A1.
- a boom for catching and refueling a smaller watercraft is known from US Pat. No. 10,053,195 B1.
- the object of the invention is to create a tank valve and a tank nozzle with which refueling can be carried out on the ship to be refueled even without human interaction.
- the tank valve according to the invention is used to seal a tank nozzle from the environment and to close the tank.
- the aim is to prevent water from entering the tank from the outside so that the tank valve can be used on a watercraft.
- the tank valve has an inlet chamber.
- the inlet chamber has an inlet opening for filling.
- the inlet opening is surrounded by an inlet edge of the inlet chamber.
- the inlet chamber further has an outlet opening, the outlet opening being connected to a tank.
- a liquid can be conveyed from the outside via the inlet opening, in particular from a tank nozzle into the inlet chamber and via the outlet opening into the tank.
- the tank valve has an inlet closure, the inlet closure being designed to close the inlet opening.
- the inlet opening is closed with the inlet seal when no refueling is being carried out.
- the inlet seal thus also closes the tank from the environment.
- the inlet closure is arranged in the inlet chamber.
- the tank valve has a force element, the force element pressing the inlet closure against the inlet edge with a first force from the inside towards the outside and sealing the inlet opening from the inside of the inlet chamber. So is the inlet opening is closed and the inlet chamber is sealed off from the environment in an unloaded case, i.e. without refueling.
- the inlet closure is connected to an outer seal via a spacer element, the outer seal being arranged outside the inlet chamber. The spacer element thus protrudes through the inlet opening.
- the outer seal can be pressed sealingly against the inlet edge with a second force from the outside in the direction of the inside, which is greater than the first force.
- the outer seal therefore preferably has an opening into which a tank nozzle can preferably be inserted.
- a force element can be a spring. It can also be about two magnets repelling each other, at least one of which, preferably both, are permanent magnets.
- the force element can additionally have an active element which activates the force element when a force is applied that is greater than the first force.
- the force element has a first permanent magnet and a current-carrying coil as a second magnet. The coil can be switched off or reversed so that no counterforce is generated or even a helping force is generated.
- the advantage of the tank valve according to the invention is that the tank valve has a self-closing inlet chamber which can be switched into an open state with a tank nozzle.
- the outer seal ensures that no liquid can get into the environment from the inlet chamber during the refueling process or, for example, that ambient water cannot get into the tank. Since the tank valve and the tank nozzle are shaped to match, the inlet chamber can only open when the tank nozzle is in contact. The tank valve cannot be opened, for example, by a wave strike.
- the inlet closure and the outer seal are connected to one another via an instruction funnel.
- the instruction funnel thus forms the spacer element.
- the instruction funnel has openings through which liquid, in particular fuel, can be passed into the inlet chamber.
- the second force is less than twice as great as the first force. This enables the inlet chamber to be reliably sealed during refueling in a simple manner. If the second force were much greater than the first force, a half-open intermediate position could easily be created.
- the tank valve has at least one first fixing element.
- the first fixing element is designed to fix a tank nozzle and to press the tank nozzle against the inlet closure and thus to press the outer seal against the inlet edge.
- the tank valve preferably has at least three fixing elements which are arranged around the inlet opening.
- the tank valve particularly preferably has four to eight fixing elements.
- the fixing element is designed in the shape of a hook and can be folded laterally.
- the first fixing element is moved hydraulically. If there are several fixing elements, these are preferably moved together.
- the tank valve has at least one proximity sensor, the proximity sensor being designed to detect a tank nozzle.
- the tank valve particularly preferably has a proximity sensor and at least one fixing element.
- the proximity of a tank nozzle detected by the proximity sensor triggers the mechanism with which the fixing element detects the tank nozzle and presses it against the inlet closure.
- the inlet chamber has lateral slots as outlet openings.
- a collecting line for forwarding the liquid, in particular the fuel is preferably arranged around the circumference. In this way, an optimum of flow area and stability can be achieved.
- the inlet chamber has a cylindrical basic shape. The inlet opening thus preferably has a rotationally symmetrical shape, particularly preferably a round shape
- the invention relates to a first watercraft with a tank and a tank valve according to the invention connected to the tank.
- the tank valve is arranged with the inlet opening facing upwards on the deck of the first watercraft.
- a vertical arrangement is preferred. The surface of the deck always moves when there is a swell. If the tank valve is arranged vertically, this movement is approximately symmetrical and can best be compensated for. Also, the fleas compensation by the up and down of the wave movement can be better balanced.
- the first watercraft is an unmanned watercraft.
- the first unmanned watercraft can be autonomous or remote-controlled.
- An autonomous watercraft can also be switched to a remote-controlled mode for the refueling process.
- the invention relates to a fuel nozzle for refueling a first watercraft by a second watercraft.
- the tank nozzle is used to be connected to the tank valve according to the invention in order to refuel.
- the tank nozzle and tank valve are like a lock and key, two interlocking and interacting components, which are, however, installed separately.
- a watercraft only has a tank nozzle according to the invention or a tank valve according to the invention, even if it is possible that a watercraft has both in order to both actively refuel and to be passively refueled.
- the tank nozzle has an outflow opening.
- a trunk valve is arranged above the outflow opening. The trunk valve is designed to close the fluid feed-through.
- a spring hose is arranged above the trunk valve.
- the spring hose is used to compensate for changes in fleas, tilting and relative movements to one another.
- a connection unit is arranged above the spring hose, the connection unit having a first connection device and a second connection device.
- the first connecting device can be connected to a lifting device, for example an on-board crane, and is used to support the tank nozzle in the center of gravity, that is to say to hold it.
- the second connecting device can be connected to a stabilizing device which is used, for example, to reduce or prevent the tank nozzle from swinging on the lifting device.
- a spring hose is preferably rolled into a spiral. This allows the hose to change its length very well. Lateral deflections can also be compensated for this way.
- the hose is preferably connected to a steel spring. The steel spring prevents the hose from kinking when the hose moves.
- the spring hose has a length of 1 m to 3 m.
- the tank nozzle has a camera.
- the camera is preferably directed towards the tank valve to be controlled.
- the camera can help an operator establish a connection. This can also enable automation of the coupling process.
- the image from the camera can also be used to align the swell compensation of the lifting device with the movements of the watercraft with the tank valve.
- the tank nozzle has a clamping ring, the clamping ring being designed so that the fixing element or the fixing elements can grasp the tank nozzle on the clamping ring and can press against the tank valve.
- the tank nozzle has a centering cone.
- the centering cone has the outflow opening.
- the centering cone can be introduced into the tank valve according to the invention.
- the centering cone of the tank nozzle and the guide funnel of the tank valve have shapes that fit into one another.
- the centering cone of the tank nozzle and the guide funnel of the tank valve fit into one another in a non-positive and liquid-tight manner.
- the invention relates to a second watercraft with a tank nozzle according to the invention and a lifting device and a storage tank.
- the tank nozzle is connected to the storage tank via a tank hose.
- the lifting device is connected to the first connection device of the tank nozzle and holds the tank nozzle, a stabilizing line being arranged between the second connection device and the second watercraft.
- the invention in a further aspect, relates to a system comprising a tank valve according to the invention and a tank nozzle according to the invention that fits into the tank valve.
- the tank nozzle and tank valve preferably fit into one another in a non-positive and liquid-tight manner.
- the mating elements of the tank nozzle and the tank valve have a truncated conical shape.
- a line with a valve is arranged below the tank valve.
- the valve opens before refueling and closes after refueling.
- the valve is a two-way valve which can be switched between a first position and a second position. In the first position, the inlet to a "disposal container" is open and a connection to the tank is closed. For example, water or other contaminants can be safely stored and disposed of later. In the second position, the connection to the tank is open and the connection to the disposal container is closed.
- the two-way valve is in the first position when the trunk is coupled and is then brought into the second position after a small volume has flowed through so that fuel can get into the tank. A contamination with seawater in the fuel can therefore be excluded. This also prevents water from collecting in or on the valve and running into the tank.
- the invention relates to a system comprising a first watercraft and a second watercraft.
- the invention relates to a method for refueling a first watercraft with a second watercraft, the method having the following steps: a) attaching the tank nozzle to the lifting device, b) pivoting the lifting device so that the tank nozzle is laterally next to the second watercraft and is arranged above the first watercraft, c) lowering the tank nozzle, d) connecting the tank nozzle and the tank valve, e) refueling the first watercraft by the second watercraft, f) disconnecting the connection between the tank nozzle and the tank valve, g) retrieving the tank nozzle by the second vessel.
- the lifting device is tracked at least during steps c) to f).
- connection in step d) comprises the following steps: h) detecting the nozzles with the first proximity sensor, i) detecting the nozzles with the first fixing element, j) pressing the nozzles against the inlet closure with a force, which is greater than the first force, k) pressing the inlet closure against the inlet rim.
- the first force is the force with which the force element presses the inlet closure against the inlet edge from the inside towards the outside.
- the first watercraft has a level control of the tank, the level control triggering the disconnection in step f) when the maximum level is reached.
- all operations of the first watercraft are remotely controlled from the second watercraft. This is preferred when the first watercraft is an unmanned watercraft.
- FIG. 1 tank valve closed in cross section.
- Fig. 2 tank valve open in cross section.
- Fig. 3 tank nozzle in side view.
- Fig. 4 system from the rear
- Fig. 1 the tank valve 10 is shown in the closed position and in Fig. 2 in the open position (with connected tank nozzle 170 during refueling).
- the tank nozzle 170 is only indicated because it is not part of the tank valve 10.
- the tank valve 10 has an inlet chamber 30.
- the inlet opening of the inlet chamber 30 is closed by the inlet closure 60, which is pressed against the inlet edge 40 by the force element 70, a spring.
- the inlet closure 60 is connected to the outer seal 90 via a spacer element 80 in the form of an instruction funnel.
- the outer seal 90 stands above the inlet opening, but, as shown in FIG. 2, can be pressed down against the inlet edge 40 by a tank nozzle 170.
- a liquid for example fuel, can be conveyed through the tank nozzle 170 and the opening 100 in the spacer element 80 into the inlet chamber 30 and through the outlet openings 50 and further via the tank nozzle 20 into the tank.
- the tank valve 10 has guide 320. These are, for example, disk-shaped and approximately triangular. For example, six directors 320 are arranged around the inlet opening offset from one another at an angle of 60 °. Furthermore, the tank valve 10 has fixing elements 10 which, in a first approximation, grip in the shape of a hook over a clamping ring 290 of a tank nozzle 170 and can thus pull the tank nozzle 170 down and hold it in place. The fixing elements are preferably arranged between the directors 320.
- each director 320 there are also six fixing elements 110, which are likewise spaced apart from one another by 60 ° and preferably by 30 ° in each case from the respective adjacent directors 320.
- any number between three and twelve, preferably from five to eight, of directors 320 and fixing elements 110 is preferred, as is a rotationally symmetrical arrangement of these elements.
- the fixing elements 110 In order to move the fixing elements 110, they are connected to a hydraulic cylinder 120 via a linkage 130. In the example shown, the fixing elements 110 are guided via a slotted hole in each case, which is in the fixing elements 110.
- any drive for example a central electric drive or separate individual drives for each fixing element 110, can also be used.
- the tank valve 10 also has two proximity sensors 140. One is arranged next to the inlet edge 40 and aligned such that this proximity sensor 140 can detect the approach of a tank nozzle 170. For safety reasons, a second proximity sensor 140 is arranged inside the tank valve 10, which can detect the movement of the inlet closure 60 or components connected to it. As a result of the arrangement in the interior, this proximity sensor 140 is not exposed to environmental influences and its failure probability is thus reduced.
- the tank valve 10 also has a plurality of seals 300.
- the tank valve 10 is installed in the deck 310 of a first watercraft 150.
- the tank nozzle 170 is shown.
- the tank hose 280 through which the liquid is conveyed is located at the upper end of the tank nozzle 170.
- This then flows on through the spiral hose 200, which has a length of 1 m, for example, and can be extended to 3 m, for example, if the spiral can be pulled apart. In this way, a movement between the upper end and the lower end can be compensated for.
- a trunk valve 190 with which the tank trunk 170 can be closed is arranged at the lower end of the spiral hose 200.
- a centering cone 270 with outflow openings 180 is arranged below the trunk valve 190. The centering cone 270 can be introduced into the spacer element 80 of the tank valve 10, which is designed as a guide funnel.
- the tank nozzle 170 has a clamping ring 290.
- the tank nozzle 170 has a camera 260 with which the position relative to a tank valve 10 and / or a deck 310 can be detected.
- a connecting unit 210 is arranged at the upper end of the tank nozzle 170 in order to support the tank nozzle 170 in its center of gravity and to keep it as stable as possible.
- the connection unit 170 has a first connection device 210. In the case shown, this is designed as a recess and a tether of a lifting device 240 can be arranged here.
- the connection unit 170 has a second connection device 220. This is also designed as a recess in the case shown.
- the second connecting device 220 can be connected to a stabilizing device 250, which brings about additional stability, in particular against swinging open in the free state.
- FIG. 4 shows a second watercraft 160, for example a utility.
- This second watercraft 160 refuels a first watercraft 150.
- the tank nozzle 170 and the tank valve 10 are shown enlarged in FIG. 5 from this illustration.
- the tank nozzle 170 can be held and moved via a lifting device 240, for example an on-board crane.
- the tank trunk is further over one Stabilization device 250 stabilized, in particular to make movements transverse to the direction of travel more difficult.
- An additional support rope 330 is used to hold the tank hose 280.
- the circle marked with Z from FIG. 4 is shown enlarged in FIG.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
La présente invention concerne un système de transfert de carburant d'un navire à un autre, en particulier vers un navire sans équipage.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP20820913.0A EP4077117B1 (fr) | 2020-12-08 | Système de transfert de carburant en mer entre deux navires |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102019220037.0 | 2019-12-18 | ||
DE102019220037.0A DE102019220037B4 (de) | 2019-12-18 | 2019-12-18 | System zur Übergabe von Treibstoff auf See zwischen zwei Wasserfahrzeugen |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2021122152A1 true WO2021122152A1 (fr) | 2021-06-24 |
Family
ID=73748136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2020/085060 WO2021122152A1 (fr) | 2019-12-18 | 2020-12-08 | Système de transfert de carburant en mer entre deux navires |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102019220037B4 (fr) |
WO (1) | WO2021122152A1 (fr) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2745927A1 (de) | 1976-10-15 | 1978-04-27 | Emh | Verbesserungen zu einrichtungen zum belegen von schiffen, insbesondere tankschiffen an offshorebohrungsplattformen |
US4483359A (en) * | 1982-09-27 | 1984-11-20 | Railhead Corp. | Pull away spill guard |
EP0863037A2 (fr) * | 1997-03-07 | 1998-09-09 | Daimler-Benz Aktiengesellschaft | Bouchon pour la canalisation de remplissage d'un réservoir de véhicule automobile |
GB2451711A (en) | 2007-08-09 | 2009-02-11 | John George Bend | Anti-spill restrictor device for a fuel tank |
US20100236657A1 (en) | 2009-03-23 | 2010-09-23 | Lockheed Martin Corporation | Fuel Fill Adaptor |
WO2013132215A2 (fr) * | 2012-03-09 | 2013-09-12 | Remfry Leigh Maxwell | Raccord de ravitaillement en carburant |
US10053195B1 (en) | 2016-01-29 | 2018-08-21 | The United States Of America As Represented By The Secretary Of The Navy | Shipboard side-mounted extending articulated boom for fueling and maintenance operations |
-
2019
- 2019-12-18 DE DE102019220037.0A patent/DE102019220037B4/de active Active
-
2020
- 2020-12-08 WO PCT/EP2020/085060 patent/WO2021122152A1/fr unknown
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2745927A1 (de) | 1976-10-15 | 1978-04-27 | Emh | Verbesserungen zu einrichtungen zum belegen von schiffen, insbesondere tankschiffen an offshorebohrungsplattformen |
US4483359A (en) * | 1982-09-27 | 1984-11-20 | Railhead Corp. | Pull away spill guard |
EP0863037A2 (fr) * | 1997-03-07 | 1998-09-09 | Daimler-Benz Aktiengesellschaft | Bouchon pour la canalisation de remplissage d'un réservoir de véhicule automobile |
GB2451711A (en) | 2007-08-09 | 2009-02-11 | John George Bend | Anti-spill restrictor device for a fuel tank |
US20100236657A1 (en) | 2009-03-23 | 2010-09-23 | Lockheed Martin Corporation | Fuel Fill Adaptor |
WO2013132215A2 (fr) * | 2012-03-09 | 2013-09-12 | Remfry Leigh Maxwell | Raccord de ravitaillement en carburant |
US10053195B1 (en) | 2016-01-29 | 2018-08-21 | The United States Of America As Represented By The Secretary Of The Navy | Shipboard side-mounted extending articulated boom for fueling and maintenance operations |
Also Published As
Publication number | Publication date |
---|---|
DE102019220037A1 (de) | 2021-06-24 |
DE102019220037B4 (de) | 2021-10-28 |
EP4077117A1 (fr) | 2022-10-26 |
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