NO20221199A1 - Four‐lobe cargo tank for transporting and / or storage of liquified gases - Google Patents
Four‐lobe cargo tank for transporting and / or storage of liquified gases Download PDFInfo
- Publication number
- NO20221199A1 NO20221199A1 NO20221199A NO20221199A NO20221199A1 NO 20221199 A1 NO20221199 A1 NO 20221199A1 NO 20221199 A NO20221199 A NO 20221199A NO 20221199 A NO20221199 A NO 20221199A NO 20221199 A1 NO20221199 A1 NO 20221199A1
- Authority
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- Norway
- Prior art keywords
- lobe
- vessel
- tank
- cargo tank
- liquefied
- Prior art date
Links
- 239000007789 gas Substances 0.000 title claims description 21
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 112
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 56
- 239000001569 carbon dioxide Substances 0.000 claims description 56
- 239000003949 liquefied natural gas Substances 0.000 claims description 40
- 230000003014 reinforcing effect Effects 0.000 claims description 10
- 239000003351 stiffener Substances 0.000 claims description 7
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
- 229910021529 ammonia Inorganic materials 0.000 claims description 3
- 239000003345 natural gas Substances 0.000 claims description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 239000007788 liquid Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910000617 Mangalloy Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000004078 cryogenic material Substances 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- QFGIVKNKFPCKAW-UHFFFAOYSA-N [Mn].[C] Chemical compound [Mn].[C] QFGIVKNKFPCKAW-UHFFFAOYSA-N 0.000 description 1
- 239000004035 construction material Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 230000009919 sequestration Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/002—Storage in barges or on ships
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
- F17C1/08—Integral reinforcements, e.g. ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B25/00—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby
- B63B25/02—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods
- B63B25/08—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid
- B63B25/12—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed
- B63B25/14—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed pressurised
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D88/00—Large containers
- B65D88/02—Large containers rigid
- B65D88/12—Large containers rigid specially adapted for transport
- B65D88/128—Large containers rigid specially adapted for transport tank containers, i.e. containers provided with supporting devices for handling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J12/00—Pressure vessels in general
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0152—Lobes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0166—Shape complex divided in several chambers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
TITLE: Four‐lobe cargo tank for transporting and / or storage of liquified gases
Field and background of the invention
The present invention relates to the field of transporting and / or storage of liquified gases in a tank, more specifically in a four-lobe cargo tank. Pipelines may provide a possible transport for short runs, but the for long distances the capital cost will be prohibitively high, so an alternative transport of captured CO2 from an initial source to a facility of usage or long-term isolation of captured CO2 is needed.
The applicant has been working with development of carbon capture systems for decades and within this field there are missing facilitties for storage and transportation of the captured Carbon Dioxide (CO2). To transport the captured CO2 in an efficient and economical manner initiated the present invention. As an example, Carbon capture plants may be located in South Korea and recipients for using CO2 for enhanced oil recovery (EOR) may be located in USA and / or Persian Gulf. An efficient and economical trade for such a long haul advantageously also includes cross trades to utilize the cargo transport capacity in both directions. An efficient cross trade can be to ship the CO2 from South Korea to USA and / or Persian Gulf and return with e.g. liquid natural gas (LNG).
Prior art
European patent application, EP3318791 A1, describes a multi-lobe tank for containing liquefied gas, for mounting into a hull of a vessel. The tank comprises at least a first longitudinally extending multi-lobe tank part having a center line A and a second longitudinally extending multi-lobe tank part having a center line B that are positioned one behind the other resulting in a forward multi-lobe tank part and a rear multi-lobe tank part with aligned center lines A, B. More specifically the patent application claims a multi-lobe tank for containing pressurized liquids, such as liquefied gas, for mounting into a ships hull, wherein the tank comprises at least a first longitudinally extending multi-lobe tank part having a center line and a second longitudinally extending multi-lobe tank part having a center line that are positioned one behind the other resulting in a forward multi-lobe tank part and a rear multi-lobe tank part with aligned center lines, wherein the first part is tapered towards an end of the first part. The invention in EP3318791 A1 is initiated to reduce the gravity center of said multi-lobe tank and therefor increase the stability of the vessel, a three-lobe cargo tank with two lobes at the tank top and one on the top of those two is therefor a preferred embodiment for that invention.
Another patent application, US2021348719 A1, describes a storage tank having a generally cubic configuration. The storage tank includes four vertically oriented cylindrical walls positioned approximately 90 degrees apart from one another and an outer support structure is coupled to the outer surface of the storage tank. The tank has an internal bulkhead structure between the four vertical cylinders where a membrane inner portion is configured to partially obstruct a flow of liquid.
The present invention is generally concerned with solving one problem related to the prior art.
Brief summary of the invention
The invention is defined by the attached independent claim 1 which is a four‐lobe cargo tank for transporting and/or storage of liquified gases, wherein the tank comprises four main lobes each with a cylinder sector outer shell and main lobe axis, said four main lobes arranged with said four main lobe axis axial‐parallel with and about a common main central axis, said four main lobes joined by four web frames with four corresponding diagonally arranged perforated bulkheads directed outwardly from said main central axis, said tank further comprises first and second end covers each end cover comprising four quarter spherical shell portions each forming an end portion of said cylinder sector outer shell, said quarter spherical shell portions of said first and second end covers respectively, joined and closing toward said main central axis by first and second four diagonally arranged cylindrical 45‐degree cut pipe ‐portions each arranged with its axis transverse to said main axis.
In an embodiment of the present invention it also relates to a method of transporting gas, comprising a vessel with at least one four-lobe cargo tank, for loading liquefied natural gas (LNG) under cryogenic conditions to said one or more four-lobe tanks at an LNG loading terminal, and sailing said vessel to an LNG unloading terminal for unloading said liquefied natural gas (LNG) at said unloading terminal for consumption and if necessary, sailing said vessel (0) to a loading terminal for liquefied carbon Dioxide (CO2) for loading captured liquefied Carbon Dioxide (CO2) into said one or more four-lobe tanks, for then sailing said captured liquefied Carbon Dioxide (CO2) to a liquefied Carbon Dioxide (CO2) unloading terminal,
- for permanent storage,
- or for industrial consumption.
An advantage of this embodiment solves problems related to transport of combined cargo e.g. high density pressurized cargo during one voyage and cryogenic temperature performance down to liquefied natural gas on the return voyage, increasing the efficiency of the vessel and indirectly reduces the costs.
Further inventive embodiments of the invention are set out in the dependent claims.
Figure descriptions
Embodiments of the present invention will now be described, by way of example only, with reference to the following figures, wherein:
Figure 1a shows in a isometric view an embodiment of the four-lobe cargo tank (1), with its four main lobes (11), as seen towards its second end cover (13b) to make the common main central axis (a1) and mail lobe axis' (a11) more apparent. As illustrated in the Figure the common main central axis (a1) is in the center of the four-lobe cargo tank (1). The Figure further shows that the main lobe axes (a11) in the cylinder-sector center of each of the main lobes (11), respectively. Each of the four lobes (11) has its own main lobe axis (a11).
Figure 1b shows an embodiment of the four-lobe cargo tank (1), with its four main lobes (11), in an isometric view as seen towards its first end cover (13a), which is the top end cover (13a) in an upright configuration of the common main central axis (a1). Figure 1b shows the cylinder sector outer shell (12) of each main lobes (11), which holds a form like a half part of a cylindrical tube and extend from the first end cover (13a) to the second end cover (13b). Figure 1b shows the first end cover (13a) comprising:
- four of quarter-spherical shell portions (14a)
- four of cylindrical 45-degree cut pipe portions (15a)
- a central common pipe (20).
Figure 1c shows an end view of an embodiment of second end cover (13b) of the four-lobe cargo tank (1). Figure 1c shows the second end cover (13b) comprising: - four of quarter spherical shell portions (14b)
- four of cylindrical 45-degree cut pipe portions (15b)
- a central common pipe (20).
Figure 2a shows in an end view an embodiment of the first end cover (13a) of the four-lobe cargo tank (1). Figure 2a shows a diagonally extending transverse axis (a15) between two of the four cylindrical 45-degree cut pipe portion (15a), indicated by a dotted line K-K. Said transverse axis (a15) is a diagonal centerline across the first and also the second end cover (13a, 13b) between those two mutually facing cylindrical 45-degree cut pipe portions. Figure 2a also show a centerline, marked N-N, that divides the four main-lobe cargo tank (1) said first end cover (13a) into two halves.
Figure 2b shows a combined elevation and section view of an embodiment of the four-lobe cargo tank (1) cross-section at said centerline N-N, as indicated in Figure 2a, wherein the internal structure, such as perforated bulkheads (16) and web frames (17) are shown, including the central pipe (20). As shown in the Figure, said web frame (17) extends between a first and a second end portion of said central pipe (20), and said perforated bulkhead (16) is arranged enveloped in the area between said web frame (17) and said central pipe (20) as shown. Another embodiment [not shown] is to arrange the perforated bulkheads (16) between said web frames (17) and are join them together at the common main central axis (a1) wihtout any central pipe (20).
Figure 2c shows in a combined elevation and section view an embodiment of a cross-section of the four-lobe cargo tank (1) at said dotted line K-K, as indicated in Figure 2a, wherein one of said transverse axes (a15) of said second end cover (13b), is indicated with an inclining angle α, from a baseline which is orthogonal to said common main central axis (a1). The Figure further shows said first and second end covers (13a, 13b) comprising their quarter spherical shell portions (14a, 14b) and cylindrical 45-degree cut pipe portions (15a,15b). A cross-section of said central pipe (20) is also shown in the Figure.
Figure 2d shows a combined isometric view and diagonal cross section of an embodiment of the same cross-section as in Figure 2b of the four-lobe cargo tank (1), for providing an overview of the internal space of the four-lobe cargo tank (1) and its internal structures comprising a perforated bulkhead (16) and a web frame (17) and a cross-section of the central pipe (20).
Figure 3a shows an elevation side view of the four-lobe cargo tank (1) comprising main lobes (11) arranged with reinforcing ribs (18). The Figure further shows that the web frames (17) partly protrude between said main lobes (11) near said central pipe (20) at said first and second end covers (13a, 13b) and jointhe main lobes (11) cylindrical 45-degree cut pipe portions (15a,15b) which furether join said quarter spherical shell portions (14a, 14b). Figure 3a shows an embodiment wherein said reinforcing ribs extends about said cylinder sector outer shells (12). A dotted an axistransverse line, marked L-L, is marked across a portion (which may in an embodiment be an upper portion) of the Figure, as a mark for where the crosssection plane in the isometric section view in next Figure, Figure 3b is taken.
Figure 3b shows an isometric view and and part section along the plane as marked by the line L-L in Figure 3a. Figure 3b shows an embodiment of the four-lobe cargo tank (1) cross-section L-L, in an isometric view , such that part of the internal structure of all four main lobes (11) are shown. Figure 3b also shows a dotted circle marked M, indicating a portion of the drawing which is enlarged to show in more detail in Figure 3c.
Figure 3c shows the enlarged details from said dotted circle marked M from Figure 3b. The Figure shows an embodiment of the four-lobe tank comprising an arrangement on assembly of said web frame (17) joining between two adjacent of said cylinder sector outer shells (12) and an arrangement for said web frame (17) and said reinforcing rib (18) (which is below the plane L-L). The Figure also shows an arrangement for said web frame (17) and said perforated bulkhead (16).
Figure 4a shows an arrangement of said four-lobe cargo tanks (1) arranged as cargo tanks shown placed in a transverse section of a vessel hull (2), such as a hull of a ship, wherein said four-lobe cargo tanks (1) are arranged with each their common main central axis (a1) in a vertical position [Vertical position, as in said main central axis (a1) is mainly perpendicular on said vessel hulls tank top]. Figure 4a shows an embodiment comprising two four-lobe cargo tanks (1) arranged side-by-side in said vessel hulls (2) breadth. Figure 4 also shows a dotted line marked P-P, which indicates a plane of a cross-section view shown in Figure 4b.
Figure 4b shows in a top view an embodiment of the four-lobe cargo tanks (1), arranged as cargo tanks in a plane section P-P of the vessel hull (2) above. The Figure shows a plane section of a vessel hull (2) comprising the top view of two fourlobe cargo tanks (1) arranged port and starboard side by side other and in rows of three, a total number of six four four-lobe cargo tanks.
Figures 5a and 5b show another view of the embodiments shown in Figures 4a and 4b.
Figures 6a, 6b and 6c, show an embodiment of the four-lobe cargo tanks (1) arranged as cargo tanks onboard a vessel (0). Figure 6a shows the vessel (0) section in center line, comprising vertically installed four-lobe cargo tanks (1) on vessel tank top (3). Figure 6b shows an embodiment wherein an upper deck is arranged above the four-lobe cargo tanks (1). Figure 6c shows a midship section view of said vessel (0) comprising two four-lobe cargo tanks (1) arranged with vertical-common main central axis (a1) within the vessel hull (2).
Figure 7a shows an embodiment of the invention wherein said four-lobe cargo tanks (1) are installalled onboard a vessel (0). Figure 7a shows a plane view at main deck comprising 20 four-lobe cargo tanks (1) that are arranged then in two rows in the breadth onboard said vessel (0). Figure 7b shows an embodiment of said vessel (0) in a section below tank top.
Figure 8a shows an embodiment of the invention wherein four-lobe cargo tanks (1) are arranged onboard a vessel (0) with combi cargo tanks (4, 1, 30), from a center line section view. Said vessel (0) with combi cargo tanks (4) comprises both said four-lobe cargo tanks (1) and further comprises cryogenic cargo tanks (30) such as LNG-tanks. Figures 8a and 8b show an embodiment wherein said four-lobe cargo tanks (1) are horizontally arranged onboard said vessel (0), horizontally arranged in the meaning that said common main central axis (a1) is mainly parallel with the combi cargo tank vessel tank top (6), and with combi cargo tanks (4, 1, 30), .
Figure 8b shows an embodiment of the inveniton wherein said four-lobe cargo tanks (1) and said cryogenic cargo tanks (30) installation onboard said vessel (0) with combi cargo tanks (4, 1, 30). Figure 8b shows a plane view at main deck comprising ten four-lobe cargo tanks (1) and five cryogenic cargo tanks (30) that are arranged seven in a row and two in the breadth, and one fore cryogenic cargo tank (30) in forward portion of said vessel (0) with combi cargo tanks (4, 1, 30).
Figure 9a shows a cross-section view of of a vessel (0) with combi cargo tanks (4) with axial (20)-transverse sections through two four-lobe cargo tanks (1) arranged onboard said vessel (0) with combi cargo tanks (4). The Figure shows longitudinally oriented horizontally installed four-lobe cargo tanks (1) on said combi cargo tank vessel tank top (6) in said combi cargo tank vessel hull (5).
Figure 9b shows a cross-section view of said vessel (0) with combi cargo tanks (4) with a cross-section view of vertical-axis embodiments of two cryogenic cargo tanks (30) arranged onboard said vessel (0) with combi cargo tanks (4, 1, 30).
Embodiments of the invention
The present invention provides a four‐lobe cargo tank (1) for transporting and/or storage of liquified gases,
wherein the tank (1) comprises four main lobes (11) each with a cylinder sector outer shell (12) and main lobe axis (a11),
‐ said four main lobes (11) arranged with said four main lobe axis (a11) axial‐parallel with and about a common main central axis (a1),
‐ said four main lobes (11) joined by four web frames (17) with four corresponding diagonally arranged perforated bulkheads (16) directed outwardly from said main central axis (a1),
‐ said tank (1) further comprises first and second end covers (13a, 13b) each end cover (13a, 13b) comprising four quarter spherical shell portions (14a, 14b) each forming an end portion of said cylinder sector outer shell (12),
‐ said quarter spherical shell portions (14a, 14b) of said first and second end covers (13a, 13b) respectively, joined and closing toward said main central axis (a1) by first and second four diagonally arranged cylindrical 45‐degree cut pipe portions (15a, 15b) each arranged with its axis (a15) transverse to said main axis (a1).
The invention provides a four-lobe cargo tank (1) for transporting liquified CO2 to e.g. enhanced oil recovery sequestration, based on CO2 gas injection, one way, and which in a further embodiment is arranged to return with other kinds of liquified or pressurized gas, such as LNG, LPG or Ammonia. Due to the utilization of the tank for transport of gases in both directions the trade will be lucrative, both economically and environmentally, as the cargo tanks can be utilized both ways and the returning voyage is profitable over an empty return.
An advantage with the four-lobe tank (1) is that the structural features of four main lobes (11) increases the overall strength qualities' over a regular cylindrical tank.
The four-lobe tank (1) with same cargo conditions, as pressure, will have an about four times increased volume over a regular cylindrical tank with same shell thickness. This is a benefit as the four-lobe tank (1) can hold more cargo with same design criterias than an individual regular cylindrical tank, thus take up less space onboard a vessel. In other words, the footprint of the four-lobe tank (1), when installed with vertical axis, is only 66% of the footprint of four individual cylindrical tanks of equal radii as the lobes (11) radii.
An other advantage with the four-lobe tank (1), is that the internal structure joined by four web frames (17) with four corresponding diagonally arranged perforated bulkheads (16) directed outwardly from said main central axis (a1), increases the strength with regard to holding cargo with relatively high density during transport, such as holding as liquefied CO2.
In an embodiment of the invention the four‐lobe cargo tank (1) further comprises a central pipe (20) that is arranged co‐axial with said main central axis (a1), wherein ‐ said central pipe (20) joining said first and second four diagonally arranged cylindrical 45‐degree cut pipe portions (15a, 15b), respectively, and said four web frames (17), near either end portions of said central pipe (20),
‐ said four perforated bulkheads (16) extending radially out from said central pipe (20). In other words, the four perforated bulkheads are joined by said central pipe (20).
The reason behind this arrangement is to arrange cargo pipes for loading and unloading said four-lobe cargo tank (1) with liquified gases through said central pipe (20). Another benefit is that cables, such as for instrumentation and power, can also be run through said central pipe (20), and when said four-lobe cargo tanks (1) are built in large scale, then even passages for manual human inspection and manholes into to the main lobes (11) can be arranged through the central pipe (20). Another benefit is that the weld joint between the four diagonally arranged perforated bulkheads (16) and the four web frames (17) can be connected at said central pipe (20), the same applies for the said central pipe (20) joining said first and second four diagonally arranged cylindrical 45‐degree cut pipe portions (15a, 15b) which can be welded towards the central pipe (20).
In an embodiment of the invention, wherein said four-lobe cargo tank (1), further comprises at least one circumferential reinforcing ring stiffener (18) to reinforce said cylinder sector outer shell (12). Said circumferential reinforcing ring stiffener (18) prevents buckling on said outer shell (12). Another benefit is that said four-lobe cargo tank (1) can resist higher internal pressure without increasing thicknesses of said cylinder sector outer shell. Such reinforcing ring stiffeners (18) can also be used as structural support for the arrangement onboard a vessel (0). Said reinforcing ring stiffener(s) (18) can be arranged on the outside of said four-lobe cargo tank (1) [as shown on Figures 3a-3c], or on the inside of said four-lobe cargo tank (1). If said reinforcing ring stiffener (18) is arranged on the inside of said four-lobe cargo tank (1), said reinforcing ring stiffener (18) becomes a part of the internal structure of said four-lobe cargo tank (1).
In an embodiment of the invention, each said second four diagonally arranged cylindrical 45‐degree cut pipe portions (15b) with its transversely arranged axis (a15) is inclined toward the corresponding end portion of said central common pipe (20). Such an arrangement in order to enable liquid draining of the tank towards and into a drain in the central common pipe (20) when installed in a vertical position. In an embodiment of the invention the inclination angle α is 5 degrees.
In an embodiment of the invention said liquefied gases comprise liquefied carbon dioxide.
In an another embodiment of the invention, said liquefied gases comprise liquefied natural gas, liquefied ammonia, or compressed natural gas.
In an embodiment of the invention the four-lobe cargo tank (1) is a pressure vessel for pressure up to 12 barg [bar=bar gauge]. In another embodiment of the invention the four-lobe cargo tank (1) is a pressure vessel for pressure up to 8 barg. In another embodiment of the invention the four-lobe cargo tank (1) is a pressure vessel for pressure above 5,2 barg.
In a further embodiment of the invention said pressure vessel is also cryogenic arranged for holding liquefied Carbon Dioxide (CO2).
In a further embodiment of the invention said pressure vessel is also arranged for holding liquefied natural gas (LNG) at ambient pressure.
In an embodiment of the invention the four-lobe cargo tank (1) is arranged to be installed onboard a vessel (0).
In an embodiment of the invention the four-lobe cargo tank (1) is arranged to be installed with cryogenic cargo tanks (30) onboard a vessel (0) with combi cargo tanks (4).
In an embodiment of the invention, wherein said web frames (17) protrude out between said four main lobes (11), so that said web frames (17) also serve as flanges for connection said four main lobes (11) and reinforce said four-lobe cargo tank (1). This will reinforce the structure of the cargo tank (1) and is useful especially when the cargo tank serve as a pressure vessel.
In an embodiment of the invention said four-lobe cargo tank (1) construction materials have qualification with enhanced mechanical properties for low temperature service.
In an embodiment of the invention said central pipe (20) protrude beyond each end cover (13). In a further embodiment of the inventionsaid central pipe (20) protrusions are arranged as main being bearing points of said four-lobe cargo tank (1).
In an embodiment of the invention said central pipe (20) protrude from one or more end cover (13) and said central pipe (20) protrusion(s) is/are arranged as lifting point(s) of said four-lobe cargo tank (1).
In an embodiment of the invention said four-lobe cargo tank(1) material is low temperature steel, such as carbon manganese steel, nickel steel, stainless steel.
In an embodiment of the invention said four-lobe cargo tank(1) material comprises cryogenic materials, such as nickel steel e.g.9% Ni, stainless steel, high manganese steel e.g. NV-Mn400.
In an embodiment of the invention said four-lobe tank(1) material is a combination of low temperature steel and cryogenic materials.
In an embodiment of the invention, related to a method of transporting gas, comprising
- using a vessel (0) according to the above,,
- loading liquefied natural gas (LNG) under cryogenic conditions to said one or more four-lobe tanks (1) at an LNG loading terminal,
- sailing said vessel (0) to an LNG unloading terminal,
- unloading said liquefied natural gas (LNG) at said unloading terminal for consumption,
- if necessary, sailing said vessel (0) to a loading terminal for liquefied carbon Dioxide (CO2)
- loading captured liquefied Carbon Dioxide (CO2) into said one or more four-lobe tanks (1),
- sailing said captured liquefied Carbon Dioxide (CO2) to a liquefied Carbon Dioxide (CO2) unloading terminal,
- for permanent storage,
- or for industrial consumption.
In an other embodiment of the invention, related to a method of transporting gas, comprising
- using a vessel (0) according to any of the embodiments above,
- loading liquefied natural gas (LNG) under cryogenic conditions to one or more cryogenic cargo tanks (30) at an LNG loading terminal,
- sailing said vessel (0) to an LNG unloading terminal,
- unloading said liquefied natural gas (LNG) at said unloading terminal for storage, further transport or consumption,
- if necessary, sailing said vessel (0) to a loading terminal for liquefied carbon Dioxide (CO2),
- loading captured liquefied Carbon Dioxide (CO2) into said one or more four-lobe tanks (1),
- sailing said captured liquefied Carbon Dioxide (CO2) to a liquefied Carbon Dioxide (CO2) unloading terminal,
- for permanent storage,
- or for industrial consumption.
Reference table
Claims (12)
1. A four‐lobe cargo tank (1) for transporting and/or storage of liquified gases, wherein the tank (1) comprises four main lobes (11) each with a cylinder sector outer shell (12) and main lobe axis (a11),
‐ said four main lobes (11) arranged with said four main lobe axis (a11) axial‐parallel with and about a common main central axis (a1),
‐ said four main lobes (11) joined by four web frames (17) with four corresponding diagonally arranged perforated bulkheads (16) directed outwardly from said main central axis (a1),
‐ said tank (1) further comprises first and second end covers (13a, 13b) each end cover (13a, 13b) comprising four quarter spherical shell portions (14a, 14b) each forming an end portion of said cylinder sector outer shell (12),
‐ said quarter spherical shell portions (14a, 14b) of said first and second end covers (13a, 13b) respectively, joined and closing toward said main central axis (a1) by first and second four diagonally arranged cylindrical 45‐degree cut pipe portions (15a, 15b) each arranged with its axis (a15) transverse to said main axis (a1).
2. The four‐lobe cargo tank (1) of claim 1, further comprising a central pipe (20) that is arranged co‐axial with said common main central axis (a1), wherein
‐ said central pipe (20) joining said first and second four diagonally arranged cylindrical 45-degree cut pipe portions (15a, 15b) and said four web frames (17) at either end portion of said central pipe (20),
‐ said four perforated bulkheads (16) extending radially out from said central pipe (20).
3. The four-lobe cargo tank (1) of claim 1, further comprising at least one circumferential reinforcing ring stiffener (18) to reinforce said cylinder sector outer shell (12).
4. The four-lobe cargo tank (1) of claim 1, wherein said second four diagonally arranged cylindrical 45‐degree cut pipe portions (15b) with its transversely arranged axis (a15) inclined toward the corresponding end portion of said central common pipe (20).
5. The four-lobe cargo tank (1) of claim 1,
wherein said liquefied gases comprise liquefied carbon dioxide.
6. The four-lobe cargo tank (1) of claim 5, further arranged for said liquefied gases to comprise liquefied natural gas, liquefied ammonia, or compressed natural gas.
7. The four-lobe cargo tank (1) of claim 1, is a pressure vessel for pressure up to 12 barg [barg=bar gauge].
8. The four-lobe cargo tank (1) of claim 6, wherein said pressure vessel is also cryogenic arranged for holding liquefied Carbon Dioxide (CO2).
9. The four-lobe cargo tank (1) of claim 1, further arranged for holding liquefied natural gas (LNG) at ambient pressure.
10. A vessel (0) comprising at least one four-lobe cargo tank (1), according to any of claims 1-9.
11. A method of transporting gas, comprising
- using a vessel (0) according to claim 10,
- loading liquefied natural gas (LNG) under cryogenic conditions to said one or more four-lobe tanks (1) at an LNG loading terminal,
- sailing said vessel (0) to an LNG unloading terminal,
- unloading said liquefied natural gas (LNG) at said unloading terminal for consumption,
- if necessary, sailing said vessel (0) to a loading terminal for liquefied carbon Dioxide (CO2)
- loading captured liquefied Carbon Dioxide (CO2) into said one or more four-lobe tanks (1),
- sailing said captured liquefied Carbon Dioxide (CO2) to a liquefied Carbon Dioxide (CO2) unloading terminal,
- for permanent storage,
- or for industrial consumption.
12. A method of transporting gas, comprising
- using a vessel (0) according to claim 10,
- loading liquefied natural gas (LNG) under cryogenic conditions to one or more cryogenic cargo tanks (30) at an LNG loading terminal,
- sailing said vessel (0) to an LNG unloading terminal,
- unloading said liquefied natural gas (LNG) at said unloading terminal for consumption,
- if necessary, sailing said vessel (0) to a loading terminal for liquefied carbon Dioxide (CO2)
- loading captured liquefied Carbon Dioxide (CO2) into said one or more four-lobe tanks (1),
- sailing said captured liquefied Carbon Dioxide (CO2) to a liquefied Carbon Dioxide (CO2) unloading terminal,
- for permanent storage,
- or for industrial consumption.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO20221199A NO348169B1 (en) | 2022-11-09 | 2022-11-09 | Four‐lobe cargo tank for transporting and / or storage of liquified gases and a method of transporting gas |
| PCT/NO2023/060086 WO2024101999A1 (en) | 2022-11-09 | 2023-11-09 | Four‐lobe cargo tank for transporting and / or storage of liquified gases |
| AU2023378282A AU2023378282A1 (en) | 2022-11-09 | 2023-11-09 | Four‐lobe cargo tank for transporting and / or storage of liquified gases |
| KR1020247023819A KR20240123830A (en) | 2022-11-09 | 2023-11-09 | Four-lobe cargo tank for transporting and/or storing liquefied gases |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO20221199A NO348169B1 (en) | 2022-11-09 | 2022-11-09 | Four‐lobe cargo tank for transporting and / or storage of liquified gases and a method of transporting gas |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NO20221199A1 true NO20221199A1 (en) | 2024-05-10 |
| NO348169B1 NO348169B1 (en) | 2024-09-16 |
Family
ID=91335162
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO20221199A NO348169B1 (en) | 2022-11-09 | 2022-11-09 | Four‐lobe cargo tank for transporting and / or storage of liquified gases and a method of transporting gas |
Country Status (1)
| Country | Link |
|---|---|
| NO (1) | NO348169B1 (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1037900A (en) * | 1951-05-30 | 1953-09-23 | Chicago Bridge & Iron Co | Advanced pressure vessel for liquid and gas |
| DE1229048B (en) * | 1962-07-28 | 1966-11-24 | Stahlbau Michael Lavis Soehne | Pressure vessel |
| DE3125963A1 (en) * | 1981-07-01 | 1983-02-10 | Gerhard KG, 5241 Weitefeld | Pressure-resistant container for materials capable of flow |
| DE3606247C1 (en) * | 1986-02-26 | 1987-05-14 | Westerwaelder Eisen Gerhard | Pressure vessel |
| US4840282A (en) * | 1987-08-10 | 1989-06-20 | Westerwaelder Eisenwerk Gerhard Gmbh | Pressure-resistant tank |
| KR200388093Y1 (en) * | 2005-04-01 | 2005-06-29 | 인하대학교 산학협력단 | Pressure Vessel |
| KR20120034391A (en) * | 2010-10-01 | 2012-04-12 | 현대중공업 주식회사 | Liquified gas carriage and/or storage tank |
| US20140117163A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Cryogenic tank |
| US20190331296A1 (en) * | 2006-10-26 | 2019-10-31 | Altair Engineering, Inc. | Storage tank containment system |
-
2022
- 2022-11-09 NO NO20221199A patent/NO348169B1/en unknown
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1037900A (en) * | 1951-05-30 | 1953-09-23 | Chicago Bridge & Iron Co | Advanced pressure vessel for liquid and gas |
| DE1229048B (en) * | 1962-07-28 | 1966-11-24 | Stahlbau Michael Lavis Soehne | Pressure vessel |
| DE3125963A1 (en) * | 1981-07-01 | 1983-02-10 | Gerhard KG, 5241 Weitefeld | Pressure-resistant container for materials capable of flow |
| DE3606247C1 (en) * | 1986-02-26 | 1987-05-14 | Westerwaelder Eisen Gerhard | Pressure vessel |
| US4840282A (en) * | 1987-08-10 | 1989-06-20 | Westerwaelder Eisenwerk Gerhard Gmbh | Pressure-resistant tank |
| KR200388093Y1 (en) * | 2005-04-01 | 2005-06-29 | 인하대학교 산학협력단 | Pressure Vessel |
| US20190331296A1 (en) * | 2006-10-26 | 2019-10-31 | Altair Engineering, Inc. | Storage tank containment system |
| KR20120034391A (en) * | 2010-10-01 | 2012-04-12 | 현대중공업 주식회사 | Liquified gas carriage and/or storage tank |
| US20140117163A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Cryogenic tank |
Also Published As
| Publication number | Publication date |
|---|---|
| NO348169B1 (en) | 2024-09-16 |
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