CN117585121A - Three-face corner area arrangement structure of film type enclosure system - Google Patents
Three-face corner area arrangement structure of film type enclosure system Download PDFInfo
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- CN117585121A CN117585121A CN202311521316.0A CN202311521316A CN117585121A CN 117585121 A CN117585121 A CN 117585121A CN 202311521316 A CN202311521316 A CN 202311521316A CN 117585121 A CN117585121 A CN 117585121A
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- 230000007704 transition Effects 0.000 claims abstract description 63
- 230000000149 penetrating effect Effects 0.000 claims abstract description 41
- 239000007788 liquid Substances 0.000 claims abstract description 9
- 238000003860 storage Methods 0.000 claims abstract description 6
- 238000009413 insulation Methods 0.000 claims description 90
- 239000002184 metal Substances 0.000 claims description 47
- 238000003466 welding Methods 0.000 claims description 41
- 238000009434 installation Methods 0.000 claims description 24
- 230000006835 compression Effects 0.000 claims description 20
- 238000007906 compression Methods 0.000 claims description 20
- 230000003014 reinforcing effect Effects 0.000 claims description 19
- 239000003292 glue Substances 0.000 claims description 17
- 239000000463 material Substances 0.000 claims description 17
- 238000004321 preservation Methods 0.000 claims description 15
- 238000003825 pressing Methods 0.000 claims description 14
- 239000003822 epoxy resin Substances 0.000 claims description 12
- 229920000647 polyepoxide Polymers 0.000 claims description 12
- 239000007769 metal material Substances 0.000 claims description 9
- 239000010964 304L stainless steel Substances 0.000 claims description 5
- 229910001374 Invar Inorganic materials 0.000 claims description 5
- 238000004021 metal welding Methods 0.000 claims description 5
- 238000005452 bending Methods 0.000 claims description 3
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 239000011120 plywood Substances 0.000 claims description 3
- 238000010008 shearing Methods 0.000 claims description 3
- 238000005728 strengthening Methods 0.000 claims description 2
- 239000012528 membrane Substances 0.000 claims 11
- 239000010408 film Substances 0.000 description 78
- 239000010409 thin film Substances 0.000 description 16
- 230000002787 reinforcement Effects 0.000 description 10
- 239000007789 gas Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000011491 glass wool Substances 0.000 description 1
- 239000012774 insulation material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000003252 repetitive effect Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B73/00—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms
- B63B73/20—Building or assembling prefabricated vessel modules or parts other than hull blocks, e.g. engine rooms, rudders, propellers, superstructures, berths, holds or tanks
-
- 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
- B63B25/16—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed heat-insulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B73/00—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms
- B63B73/40—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms characterised by joining methods
- B63B73/43—Welding, e.g. laser welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B73/00—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms
- B63B73/40—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms characterised by joining methods
- B63B73/46—Gluing; Taping; Cold-bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B73/00—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms
- B63B73/40—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms characterised by joining methods
- B63B73/49—Building or assembling vessels or marine structures, e.g. hulls or offshore platforms characterised by joining methods by means of threaded members, e.g. screws, threaded bolts or nuts
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
- F16L59/029—Shape or form of insulating materials, with or without coverings integral with the insulating materials layered
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Structural Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Thermal Insulation (AREA)
Abstract
The embodiment of the invention provides a three-sided corner area arrangement structure of a film type enclosure system, which comprises a main film layer, a fastening clamping plate, a main insulating layer, a secondary film layer and a secondary insulating layer which are sequentially connected and fixed on a ship body structure through penetrating fasteners, and the main film layer, the fastening clamping plate, the main insulating layer, the secondary film layer and the secondary insulating layer are enclosed to form a low-temperature liquid cargo storage tank for accommodating ultralow-temperature medium; the corner area where the three side surfaces meet in the film type enclosure system is provided with a triangular area module, the triangular area module comprises a triangular area main layer insulating layer module and a triangular area sub-layer insulating layer module, the triangular area main layer insulating layer module comprises three main layer insulating surface structures which are respectively arranged corresponding to three cabin wall surfaces of the triangular area of the ship body structure, and a gap at a contact position of the triangular area main layer insulating layer module and the main insulating transition module of the plane area of the main layer insulating layer and a gap at a contact position of the triangular area sub-layer insulating layer module and the sub-insulating transition module of the plane area of the sub-layer insulating layer are positioned in different planes.
Description
Technical Field
The invention relates to the technical field of equipment for transporting and storing low-temperature liquid, in particular to a three-face corner area arrangement structure of a film type enclosure system.
Background
In transporting a gas such as natural gas or ethane gas, it is common to cool the gas to a low temperature and transport the liquefied gas for more economical long-distance transportation. The volume of the liquefied gas is greatly reduced, and the transportation cost is reduced. The liquefied cryogenic liquid is stored and transported by a special cryogenic liquid cargo storage tank.
In the current shipbuilding industry, cryogenic liquid cargo containment systems are primarily concerned with the manufacturing of LNG vessels. For LNG vessels, the international bulk transport liquefied gas vessel construction and equipment regulations (IGC regulations) define 4 broad classes of containment systems, type a, type B, type C and thin film containment systems, respectively. The thin film type enclosure system is widely applied due to the advantages of high cabin capacity utilization rate, good heat preservation performance, small wind resistance area and the like.
The existing thin film containment system technology mainly comprises Mark III type and NO 96 type, which are both from French GTT company. However, for the NO 96 type, as the main insulating modules and the secondary insulating modules are overlapped up and down, gaps between the main insulating modules and gaps between the secondary insulating modules are directly communicated to the ship body structure, and heat insulation materials such as glass wool are uniformly distributed at the gaps, but larger heat leakage exists at the gaps; for Mark III type, as the main layer insulating module, the secondary layer insulating module and the secondary layer film are mutually fixed and adhered into a whole through glue, and are fixed on the ship body structure through epoxy resin, the relative movement between the main layer insulating module and the secondary layer insulating module is limited, and the whole ship body movement resistance and liquid cargo sloshing resistance are poor; in addition, due to the fact that a large amount of glue is used, the construction period is long, and due to the fact that requirements on construction environment (humidity and temperature) and working procedures are strict, the period of the ship is prolonged.
Disclosure of Invention
In view of the above-mentioned problems in the prior art, the embodiment of the present invention provides a three-sided area structure of a film enclosure system, which is used for accommodating an ultralow temperature medium, and includes a main layer film layer, a fastening clamping plate, a main layer insulating layer, a sub layer film layer and a sub layer insulating layer that are sequentially connected and fixed to a hull structure through penetrating fasteners, that is, the main layer insulating layer and the fastening clamping plate are disposed between the main layer film layer and the sub layer film layer, the sub layer insulating layer is disposed between the sub layer film layer and the hull structure, and the main layer film layer, the fastening clamping plate, the main layer insulating layer, the sub layer film layer and the sub layer insulating layer are all connected and fixed to the hull structure through penetrating fasteners, and meanwhile, the main layer insulating structure and the gap between the main layer film layer and the sub layer film layer form a main layer shielding space, and the sub layer insulating structure and the gap between the sub layer film layer and the hull structure form a sub layer shielding space, thereby effectively solving the problems of storage and leakage prevention of the ultralow temperature medium.
The embodiment of the invention provides a three-sided corner area arrangement structure of a film type enclosure system, which comprises a main layer film layer, a fastening clamping plate, a main layer insulating layer, a sub-layer film layer and a sub-layer insulating layer which are sequentially connected and fixed on a ship body structure through penetrating fasteners, wherein the main layer film layer, the main layer insulating layer, the sub-layer film layer and the sub-layer insulating layer are enclosed to form a low-temperature liquid cargo storage tank for accommodating ultralow-temperature medium, and the main layer film layer is in contact with the ultralow-temperature medium; the corner areas where the three side surfaces are connected in the film type enclosure system are provided with triangular area modules, the triangular area modules comprise triangular area main insulating layer modules and triangular area secondary insulating layer modules, wherein,
The three-face-area sub-layer insulating layer module comprises three sub-layer insulating surface structures which are respectively arranged corresponding to three cabin wall surfaces of a three-face-area of a ship body structure, wherein the included angle between any two sub-layer insulating surface structures in the three sub-layer insulating surface structures is determined based on the included angle between corresponding cabin wall surfaces on two sides in the ship body structure, and each three-face-area sub-layer insulating layer module consists of three layers of structures;
the main insulating layer module of the triangular area comprises three main insulating layer structures which are respectively arranged corresponding to three cabin wall surfaces of the triangular area of the hull structure, wherein the included angle between any two main insulating layer structures in the three main insulating layer structures is determined based on the included angle between the cabin wall surfaces of the two corresponding sides in the hull structure, and each main insulating layer module of the triangular area consists of four layers of structures;
the gap at the contact position of the main insulating layer module of the triangular region and the main insulating transition module of the plane region of the main insulating layer and the gap at the contact position of the sub insulating transition module of the triangular region and the plane region of the sub insulating layer are positioned in different planes.
In some embodiments of the present invention, each of the triangular region sub-layer insulating layer modules includes a first bottom plate, a heat insulation block and a metal welding plate, which are sequentially adhered and fixed inwards by a cabin wall surface, wherein an inward concave step notch groove is formed at an upper edge of a side, which is connected with the triangular region sub-layer planar transition insulating module, of the heat insulation block, an inward concave installation notch groove is formed at an upper edge of a side, which is connected with the heat insulation block, of the triangular region sub-layer planar transition insulating module, and the installation notch groove is arranged corresponding to the step notch groove, and when the triangular region sub-layer planar transition insulating module is adhered and fixed with the heat insulation block, the heat insulation block is adhered and fixed through the step notch groove and a tabletting plate at the top of the installation notch groove; the plane transition insulation module of the triangular region sublayer comprises a second top plate, four heat preservation blocks, a cross reinforcing structure, four central supporting structures and a second bottom plate, wherein the four heat preservation blocks are respectively arranged in four spaces between the second top plate and the second bottom plate, the four spaces are formed by the cross reinforcing structures, and through holes for installing penetrating fasteners are formed in the middle parts of the four central supporting structures.
In some embodiments of the present invention, each of the main insulating layer modules in the dihedral zone includes a first top plate, an upper insulating block, a middle plate and a lower insulating block, which are sequentially disposed from an inner side far from the bulkhead surface to an outer side near the bulkhead surface, wherein the main insulating layer module in the dihedral zone is provided with a mounting notch at a corner connected with the main insulating layer module in the dihedral zone, each mounting notch is provided with a fixing cushion block fixedly connected with the middle plate, the fixing cushion block is adapted to the shape of the mounting notch, and the mounting notch is specifically formed on the lower insulating block of the main insulating layer module in the dihedral zone.
In some embodiments of the present invention, a width dimension of each of the three main insulating surface structures of the three main insulating surface module is greater than a width dimension of the sub-insulating surface structures of the three main insulating surface module.
In some embodiments of the present invention, a distance plunger hole for installing a distance plate of the third-angle zone sub-layer planar transition insulation module is arranged on a step plane parallel to a bulkhead surface where the step notch groove is located and at one end of the third-angle zone main-layer insulation module.
In some embodiments of the present invention, the triple-angle zone sublayer plane transition insulation module further comprises a sublayer welded metal sheet, a sublayer welded plate, a tabletting insulation block and a tabletting plate, wherein the second top plate is provided with a welded plate groove and a welded plate groove, and after the sublayer welded plate groove and the sublayer welded metal sheet are respectively installed in the welded plate groove and the welded plate groove, the upper surfaces of the sublayer welded plate and the sublayer welded metal sheet are flush with the upper surface of the second top plate, and the sublayer welded metal sheet is provided with a connecting hole for installing a penetrating fastener;
the utility model discloses a laminated sheet material, including the second top panel, the second bottom panel, the second top panel, the second bottom panel is last all be equipped with the installation fixed orifices that corresponds the through-hole of central bearing structure on the cross additional strengthening set up, the installation breach groove with the ladder breach groove corresponds the setting when the regional sublayer insulating layer module of three faces with the regional sublayer plane transition insulating module of three faces is connected, ladder breach groove with the bottom preforming panel bonding in installation breach groove is fixed, the preforming heat preservation piece with preforming panel ladder breach groove with the installation breach groove bonding is fixed, the upper portion of preforming heat preservation piece with the second top panel bonding is fixed.
In some embodiments of the present invention, when the triple-angle zone sub-layer planar transition insulation module is adhered and fixed to the cabin wall surface of the hull structure by the second bottom plate, a strip-shaped epoxy resin is adhered to the cabin wall surface of the hull structure at a distance between the second bottom plate and the cabin wall surface of the hull structure, and the height of the epoxy resin between the second bottom plate and the cabin wall surface of the hull structure is set to be greater than 12mm and less than 20mm according to the distance between the epoxy resins.
In some embodiments of the present invention, the distance plate is made of plywood or plastic substitute material meeting the rigidity requirement, the thickness of the plate is set to be at least one of 1mm, 2mm, 5mm or 10mm, the distance plate is used for leveling, and the distance plate overlapping combination with different thickness is adopted, so that the distance between the bottom of the three-face-area sub-layer planar transition insulation module and the cabin wall surface is 10mm;
the aperture of the through hole on the distance plate is 0.5-2mm larger than the outer diameter of the thread on the stud.
In some embodiments of the invention, the through fastener comprises: a through fastener upper section portion and a through fastener lower section portion, wherein,
The upper section part comprises a cap rod structure, a compression block, a double-head screw rod and a metal sealing cap, wherein the compression block is arranged in a triangular region main layer insulating layer module, a planar region main layer insulating layer module and mounting notches formed in the adjacent planar region main layer insulating layer module and the adjacent dihedral region main insulating layer module, a bottom metal plate of the compression block is attached to a fixed cushion block, and long bolts on the compression block lock the compression block;
the lower section part of the penetrating fastener comprises a cylindrical welding base and a metal connecting rod with threads at two ends, one end of the metal connecting rod penetrates through the sublayer welding metal sheet to be fixedly connected with the cap rod structure, the other end of the metal connecting rod is fixedly welded with the hull structure through the cylindrical welding base, and the metal connecting rod penetrates through a through hole of a central supporting structure of the cross-shaped reinforcing structure on the triangular region sublayer plane transition insulating module.
In some embodiments of the invention, each of the three cabin wall surfaces in the three corner areas of the hull structure is disposed perpendicular to at least one of the fixed blocks, and the fixed blocks are flush with the sides of the lower thermal block and the side of the middle panel.
In some embodiments of the present invention, the first top sheet, the middle sheet, the first bottom sheet, the second top sheet, the cross reinforcement structure, and the second bottom sheet are all made of a low temperature resistant non-metallic material having a set strength, wherein the low temperature resistant non-metallic material is capable of withstanding temperatures of at least 196 degrees celsius below zero, the strength is required to meet the following requirements, in particular,
the vertical compression strength is more than or equal to 4Mpa, the bending strength is more than or equal to 20Mpa, the horizontal tensile strength is more than or equal to 25Mpa, the vertical tensile strength is more than or equal to 1.5Mpa, and the shearing strength is more than or equal to 2.5Mpa.
The heat insulation block, the upper heat insulation block, the lower heat insulation block, the tabletting heat insulation block and the heat insulation block are all made of materials meeting the set heat conductivity coefficient requirement, wherein the set heat conductivity coefficient requirement is that the heat conductivity coefficient is not more than 0.1W/m.K;
the main layer film and the secondary layer film are both made of invar steel or 304L stainless steel or other low-temperature-resistant metal materials which are prefabricated into a set corrugated shape.
In some embodiments of the invention, the cross reinforcement structure is overlapped with the second top plate except the pressed plate, and is connected with the second top plate through glue or rivets;
The periphery of the second bottom plate is overlapped with the cross reinforcing structure except for the mounting notch groove, and is connected with the cross reinforcing structure through glue or rivets;
the contact parts of the heat preservation block, the second top plate, the second bottom plate and the cross reinforcing structure are all fixed by glue;
the tabletting plates are positioned at the bottoms of the mounting notch grooves and are adhered and fixed with the adjacent heat insulation blocks through glue, and the tabletting plates extend out of the second bottom plate in the direction of the wall surface of the ship cabin parallel to the tabletting plates at the position close to the sub-layer insulating layer module in the triangular area;
the tabletting heat insulation block is positioned between the second top plate and the tabletting plate;
the pressing sheet heat-insulating block is fixedly connected with the contact part of the second top plate, the pressing sheet plate and the heat-insulating block through glue.
Compared with the prior art, the three-face corner area structure of the film type enclosure system provided by the embodiment of the invention has the beneficial effects that: the main insulating layer modules of the triangular region and the secondary insulating layer modules of the triangular region are arranged in a staggered manner, so that the overall heat leakage at the gap is reduced; simultaneously, the insulating layer module of the third-face area sub-layer is adhered to the hull structure by epoxy resin, and the main insulating layer module of the third-face area is connected by a penetrating fastener.
Drawings
FIG. 1 is a schematic diagram of a configuration of a triangular region of a thin-film containment system according to an embodiment of the present invention;
FIG. 2 is a schematic cross-sectional view of a configuration of a triangular region of a thin-film containment system according to an embodiment of the present disclosure;
FIG. 3 is a schematic view of a transition structure of a triangular region structure of a thin-film containment system according to an embodiment of the present invention;
fig. 4 is a schematic layout view of a triangular region module of a triangular region structure of a thin film containment system in a ship structure according to an embodiment of the present invention;
fig. 5 is a schematic diagram of a triangular region insulation module structure of a triangular region structure of a thin film containment system according to an embodiment of the present invention;
FIG. 6 is a schematic view of an explosion diagram of a triangular region insulation module structure of a triangular region structure of a thin film containment system according to an embodiment of the present invention;
FIG. 7 is an exploded view of a through fastener of a three-sided corner structure of a thin film containment system according to an embodiment of the present invention;
FIG. 8 is a schematic diagram of a planar transition insulation module of a triangular region sub-layer of a triangular region structure of a thin film containment system according to an embodiment of the present invention;
FIG. 9 is an exploded schematic view of a planar transition insulation module structure of a triangular region sub-layer of a triangular region structure of a thin film containment system according to an embodiment of the present invention;
FIG. 10 is a schematic view of the installation of a sub-layer insulating layer and a sub-layer film layer of a three-sided corner region structure of a film containment system according to an embodiment of the present invention;
FIG. 11 is a schematic diagram illustrating installation of a main insulating layer of a three-sided corner region structure of a thin film containment system according to an embodiment of the present invention;
fig. 12 is a schematic view of installing a main thin film layer of a triple-sided corner structure of a thin film containment system according to an embodiment of the present invention.
Reference numerals
1. Welding a base; 2. a nut; 3. a metal connecting rod; 4. a sub-layer is welded with a metal sheet; 10. penetrating the lower section of the fastener; 11. a cap rod structure; 12. a bottom metal plate; 19. a long bolt; 21. a compaction block; 22. a double-ended screw; 23. a metal sealing cap; 24. welding a metal sheet on the main layer; 25. penetrating the upper section of the fastener; 26. a hull structure; 27. a bulkhead surface; 28. penetrating the fastener; 29. an epoxy resin; 31. a sub-layer insulating layer; 31a, a planar region sub-layer insulating layer module; 32. a sub-layer film layer; 32a, a sublayer film; 33. a main layer insulating layer; 33a, a planar region main layer insulating layer module; 34. a main layer film layer; 34a, a main layer film; 35. fastening a clamping plate; 35c, corner transition clamping plates; 36. a distance plate; 37. a stud; 38. a primary layer welding plate; 48. a primary insulating surface structure 49 and a secondary insulating surface structure; 50. a secondary insulating layer module in the two-sided corner region; a 50a, 90 DEG dihedral region sub-insulating layer module; 50b, 135 DEG dihedral region sub-insulating layer modules; 51. a first bottom sheet; 52. a heat insulating block; 53. a metal welding plate; 54. spacing the plunger holes; 55. distance bolt holes; 56. a step notch groove; 60. a main insulating layer module in the two-sided corner region; 60a, 90 DEG dihedral region main insulating layer modules; 60b, 135 DEG dihedral region main insulating layer modules; 61. an upper thermal insulation block; 62. a lower thermal insulation block; 63. a first top sheet; 64. a middle plate; 65. fixing the cushion block; 69. a mounting notch; 70. a planar transition sublayer insulating layer module in the two-sided corner region; 71. a secondary layer welding plate; 72. a second top sheet; 73. welding tab grooves; 74. a welding plate groove; 75. tabletting and insulating blocks; 76. a heat preservation block; 77. a cross reinforcement structure; 78. a through hole; 79. a central support structure; 80. a second bottom sheet; 81. tabletting the plate; 82. mounting a notch groove; 83. a transition film in the corner region of the sublayer; 84. a main layer corner transition film; 85. a film seal head in a sub-layer corner area; 90. the plane transition insulation module of the sublayer of the triangular area; 100. a dihedral region module; 101. a main insulating layer module in a triangular area; 102. a triangular region sub-layer insulating layer module;
Detailed Description
The present invention will be described in detail below with reference to the drawings and detailed description to enable those skilled in the art to better understand the technical scheme of the present invention.
Various aspects and features of the present application are described herein with reference to the accompanying drawings.
These and other characteristics of the present application will become apparent from the following description of a preferred form of embodiment, given as a non-limiting example, with reference to the accompanying drawings.
It is also to be understood that, although the present application has been described with reference to some specific examples, a person skilled in the art will certainly be able to achieve many other equivalent forms of the present application, having the characteristics as set forth in the claims and hence all coming within the field of protection defined thereby.
The foregoing and other aspects, features, and advantages of the present application will become more apparent in light of the following detailed description when taken in conjunction with the accompanying drawings.
Specific embodiments of the present application will be described hereinafter with reference to the accompanying drawings; however, it is to be understood that the disclosed embodiments are merely exemplary of the application, which can be embodied in various forms. Well-known and/or repetitive functions and constructions are not described in detail to ascertain the true intent of the present application, based on the historical operations of the user, to avoid obscuring the application with unnecessary or redundant detail. Therefore, specific structural and functional details disclosed herein are not intended to be limiting, but merely serve as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present application in virtually any appropriately detailed structure.
The specification may use the word "in one embodiment," "in another embodiment," "in yet another embodiment," or "in other embodiments," which may each refer to one or more of the same or different embodiments as per the application.
The embodiment of the invention provides a three-sided area arrangement structure of a film type enclosure system, as shown in fig. 1 to 12, wherein the film type enclosure system comprises a main layer film layer 34, a fastening clamping plate 35, a main layer insulating layer 33, a sub layer film layer 32 and a sub layer insulating layer 31 which are sequentially connected and fixed on a ship structure 26 through penetrating fasteners 28, the main layer film layer 34, the sub layer film layer 32 and the sub layer insulating layer 31 enclose to form a low-temperature liquid cargo storage tank for containing ultra-low temperature medium, the main layer film layer 34 is in contact with the ultra-low temperature medium, in particular, the main layer insulating layer 33 and the fastening clamping plate 35 are arranged between the main layer film layer 34 and the sub layer film layer 32, the sub layer insulating layer 31 is arranged between the sub layer film layer 32 and the ship structure, the main layer insulating structure and a gap between the main layer film layer 34 and the sub layer film layer 32 form a main layer shielding space, the sub layer insulating structure and the gap between the sub layer film layer 32 and the ship structure 26 form a sub layer shielding space, and the ultra-low temperature medium is effectively sealed, and the ultra-low temperature medium leakage is effectively solved.
The corner areas where the three sides meet in the thin film enclosure system are all provided with a triangular area module 100, and the triangular area module 100 comprises a triangular area main insulating layer module 101 and a triangular area sub-insulating layer module 102, specifically,
the triangular region sub-layer insulating layer module 102 comprises three sub-layer insulating surface structures 49 which are respectively arranged corresponding to the three cabin wall surfaces 27 of the triangular region of the hull structure 26, and the included angle between any two sub-layer insulating surface structures in the three sub-layer insulating surface structures 49 is determined based on the included angle between the cabin wall surfaces 27 on the corresponding two sides in the hull structure 26.
As an example, if the included angle between the two cabin wall surfaces 27 is 90 degrees, the included angle between the two sub-layer insulating surface structures 49 corresponding to the two cabin wall surfaces 27 may be 90 degrees, and correspondingly, the sub-insulating layer modules 50a in the 90 ° dihedral angle region are correspondingly disposed; of course, the included angle between the two cabin wall surfaces 27 may be between 85 degrees and 95 degrees, if the included angle between the two cabin wall surfaces 27 is 135 degrees, the included angle between the two sub-layer insulating surface structures 49 corresponding to the two cabin wall surfaces may be 135 degrees, and correspondingly, the sub-insulating layer module 50b with a 135-degree dihedral angle region may be disposed between 130 degrees and 140 degrees, that is, the included angle between the two sub-layer insulating surface structures 49 may have an angle difference within a certain range with the included angle between the corresponding two cabin wall surfaces.
Further, each of the triangular region sub-layer insulating layer modules 102 is composed of a three-layer structure, and each of the triangular region sub-layer insulating layer modules comprises a first bottom plate 51, a heat insulation block 52 and a metal welding plate 53 which are adhered and fixed to each other by the inner side of the cabin wall surface, wherein an inward concave stepped notch groove 56 is formed in the upper edge of one side, connected with the triangular region sub-layer planar transition insulating module 90, of the heat insulation block 52, and an inward concave mounting notch groove 82 is formed in the upper edge of the side, connected with the heat insulation block 52, of the triangular region sub-layer planar transition insulating module 90 and is arranged corresponding to the stepped notch groove 56.
When the triangular region sublayer plane transition insulating module 90 is fixedly bonded with the heat insulation block 52, the step notch groove 56 and the pressed sheet 81 at the top of the mounting notch groove 82 are fixedly bonded.
In this embodiment, a distance plunger hole 54 for installing the distance plate 36 of the third-angle-zone sub-layer planar transition insulation module 90 is provided on one end of the third-angle-zone main-layer insulation module away from the third-angle-zone main-layer insulation module on a step plane parallel to the wall surface of the ship cabin where the step notch groove 56 is located in the step notch groove 56.
The triangular region sublayer plane transition insulation module 90 comprises a second top plate 72, four insulation blocks 76, a cross reinforcement structure 77, four central support structures 79 and a second bottom plate 80, wherein the four insulation blocks 76 are respectively arranged in four spaces between the second top plate 72 and the second bottom plate 80, which are formed by the cross reinforcement structures 77, and the middle parts of the four central support structures 79 are provided with through holes 78 for installing penetrating fasteners 28.
In this embodiment, the second bottom plate 80 is further provided with a distance bolt hole 55 concentrically arranged with the through hole on the distance plate 36, and the second top plate 72 and the heat insulation block 76 are provided with distance plunger holes 54 concentrically arranged corresponding to the through hole of the distance plate 36 and having a hole diameter 2-4 times that of the corresponding through hole, so that the spacer, the fastening nut and the tool lock the distance plate 36 are facilitated. Further, after the four studs 37 penetrating through each distance plate 36 are locked by the nuts 2, the distance stud holes 54 formed on each triangular region sub-layer planar transition insulating module 90 are plugged by plungers made of the same material as the heat preservation blocks 76, so that the effect of interconnection between each triangular region sub-layer planar transition insulating module 90 and the adjacent planar region sub-layer insulating module 31a or the triangular region sub-layer insulating module 50 and the triangular region sub-layer insulating module 102 is realized, and an auxiliary anchoring effect is achieved on the triangular region sub-layer planar transition insulating module 90 and the adjacent planar region sub-layer insulating module 31a or the triangular region sub-layer insulating module 50.
Further, the distance plate 36 is made of plywood or plastic substitute material meeting the rigidity requirement, the thickness of the plate is set to be at least one of 1mm, 2mm, 5mm or 10mm, the distance plate 36 is used for leveling, and the distance plate 36 with different thicknesses is used for superposition combination, so that the distance between the bottom of the triangular region sub-layer planar transition insulation module 90, the adjacent planar region sub-layer insulation module 31a or the adjacent two-sided angular region sub-insulation module 50 and the cabin wall surface 27 is 10mm; the aperture of the through hole on the distance plate 36 is 0.5-2mm larger than the outer diameter of the thread on the stud.
In this embodiment, the main insulating layer module 101 in the triangular region includes three main insulating layer structures 48 corresponding to and fixedly adhered to the three bulkhead faces 27 in the triangular region of the hull structure 26, the included angle between any two main insulating layer structures in the three main insulating layer structures 48 is determined based on the included angle between the corresponding two bulkhead faces 27 in the hull structure 26, each main insulating layer module 101 in the triangular region is composed of four layers of structures, and each main insulating layer module 101 in the triangular region includes a first top plate 63, an upper insulating block 61, a middle plate 64 and a lower insulating block 62 sequentially adhered and fixed from the inner side far from the bulkhead face to the side near the bulkhead face, the main insulating layer module 101 in the triangular region is provided with a mounting notch 69 at the corner connected with the main insulating layer module in the triangular region, and each mounting notch 69 is provided with a fixing cushion 65 fixed with the middle plate 64 and adapted to the shape of the lower insulating block 62 in the mounting notch 69;
wherein, the gap at the connection position of the main insulating layer module 101 of the triangular region and the main insulating layer module 33a of the planar region and the gap at the connection position of the sub insulating layer module 102 of the triangular region and the sub insulating layer module 90 of the triangular region are located in different planes, and as an example, in the triangular region, the length of the main insulating layer module 101 of the triangular region on each side line is shorter than that of the sub insulating layer module of the triangular region in the three tank side line directions between the corresponding three tank wall surfaces 27 of the main insulating layer module 101 of the triangular region, so as to ensure that the gap between the sub insulating layer module of the triangular region and the adjacent sub insulating layer module of the triangular region and the gap between the main insulating module of the triangular region and the main insulating module of the adjacent two corner regions are not overlapped.
In some embodiments of the present invention, the width dimension of each of the three main insulating surface structures 48 of the three main insulating surface structures 101 of the three main insulating surface modules is greater than the width dimension of the sub-insulating surface structures 49 of the three sub-insulating surface structures 102 of the three main insulating surface structures 48.
In this embodiment, the third-face area sub-layer planar transition insulation module 90 further includes a sub-layer welded metal sheet 4, a sub-layer welded plate 71, a pressed thermal insulation block 75 and a pressed sheet material 81, wherein the second top sheet material 72 is provided with a welded plate slot 74 and a welded plate slot 73, and after the sub-layer welded metal sheet 4 and the sub-layer welded plate 71 are respectively installed in the welded plate slot 73 and the welded plate slot 74, the upper surface of the sub-layer welded metal sheet 71 and the upper surface of the sub-layer welded metal sheet 4 are flush with the upper surface of the second top sheet material 72, and the sub-layer welded metal sheet 4 is provided with a connection hole for installing a penetrating fastener 28;
the second top plate 72 and the second bottom plate 80 are respectively provided with a mounting fixing hole corresponding to the through hole 78 of the central supporting structure 79 on the cross reinforcing structure 77, the mounting notch groove 82 and the step notch groove 56 are correspondingly arranged, when the triangular region sub-layer insulating layer module 102 and the triangular region sub-layer plane transition insulating module 90 are connected, the step notch groove 56 and the bottom pressing plate 81 of the mounting notch groove 82 are fixedly bonded, the pressing heat preservation block 75 and the pressing plate 81, the cabin wall surface of the step notch groove 56 and the cabin wall surface of the mounting notch groove 82 are fixedly bonded, and the upper part of the pressing heat preservation block 75 and the second top plate 72 are fixedly bonded.
Further, in the present embodiment, when the triple-angle zone sub-layer planar transition insulation module 90 is adhesively fixed to the hold wall 27 of the hull structure 26 by the second bottom plate 80, a strip-shaped epoxy resin 29 is adhered to the space between the second bottom plate 80 and the hold wall 27 of the hull structure 26, and the height of the epoxy resin 29 between the second bottom plate 80 and the hold wall 27 of the hull structure 26 is set to be greater than 12mm and less than 20mm according to the space between the epoxy resins 29.
In some embodiments of the present invention, the through fastener 28 includes: through fastener upper section 25 and through fastener lower section 10, wherein,
the upper section 25 of the penetrating fastener comprises a lower end cap rod structure 11, a compression block 21, a double-ended screw rod 22 and a metal sealing cap 23, wherein the compression block 21 is arranged on a dihedral zone main insulating layer module 101, an adjacent main insulating layer module 33a and a dihedral zone main insulating layer module 60, the dihedral zone main insulating layer module 60 comprises a 90-degree dihedral zone main insulating layer 60a and a 135-degree dihedral zone main insulating layer 60b, a bottom metal plate 12 of the compression block 21 is attached to a fixed cushion block 65, and a long bolt 19 on the compression block 21 locks the compression block 21;
The lower section 10 of the penetrating fastener comprises a cylindrical welding base 1 and a metal connecting rod 3 with threads at two ends, one end of the metal connecting rod passes through the sublayer welding metal sheet 4 to be fixedly connected with the lower end cap rod structure 11, the other end of the metal connecting rod is fixedly welded with the hull structure 26 through the cylindrical welding base 1, and the metal connecting rod 3 is arranged in a penetrating hole 78 of a central supporting structure 79 of a cross reinforcing structure 77 on the triangular region sublayer plane transition insulating module 90 in a penetrating mode.
In this embodiment, each of the three cabin wall surfaces 27 in the triangular region of the hull structure 26 is disposed vertically to at least one of the fixing pads 65, and the fixing pads 65 are flush with the side surfaces of the lower thermal insulation block 62 and the side of the middle plate 64.
In some embodiments of the present invention, the first top sheet 63, the middle sheet 64, the first bottom sheet 51, the second top sheet 72, the cross reinforcement structure 77, and the second bottom sheet 80 are all made of a low temperature resistant non-metallic material having a set strength, wherein the low temperature resistant non-metallic material is capable of withstanding temperatures of at least 196 degrees celsius below zero, the strength being required to meet the following requirements, in particular,
The vertical compression strength is more than or equal to 4Mpa, the bending strength is more than or equal to 20Mpa, the horizontal tensile strength is more than or equal to 25Mpa, the vertical tensile strength is more than or equal to 1.5Mpa, and the shearing strength is more than or equal to 2.5Mpa.
The heat insulation block 52, the upper heat insulation block 61, the lower heat insulation block 62, the tabletting heat insulation block 75 and the heat insulation block 76 are made of materials meeting the set heat conductivity requirement, wherein the set heat conductivity requirement is that the heat conductivity is not more than 0.1W/m.K;
the primary film layer 34 and the secondary film layer 32 are made of invar steel or 304L stainless steel or other low temperature resistant metal materials prefabricated into a set corrugated shape.
In some embodiments of the present invention, the cross reinforcement structure 77 is overlapped with the second top plate 72 at the periphery of the rest except for the sheet 81, and is connected to the second top plate 72 by glue or rivets;
the periphery of the second bottom plate 80 is overlapped with the cross reinforcing structure 77 except for the pressed plate 81, and is connected with the cross reinforcing structure 77 through glue or rivets;
the contact parts of the heat insulation blocks 76, the second top plate 72, the second bottom plate 80 and the cross reinforcing structures 77 are all fixed by glue;
The pressing sheet 81 is positioned at the bottom of the installation notch groove and is adhered and fixed with the adjacent heat insulation block 76 through glue, and the pressing sheet 81 extends out of the second bottom sheet 80 towards the direction of the cabin wall surface 27 parallel to the pressing sheet 81 at the position close to the insulating layer module 102 of the sub-layer in the triangular area;
the tabletting insulation 75 is located between the second top sheet 72 and the tabletting sheet 81;
the pressed sheet heat insulation block 75 is fixedly connected with the contact part of the second top plate 72, the pressed sheet 81 and the heat insulation block 76 through glue.
Specifically, when the above-mentioned three-sided corner area arrangement structure of the film enclosure system is installed, the installation method includes:
scribing the cabin wall 27 of the hull structure 26, and welding the welding base 1 penetrating the lower section 10 of the fastener at the position of the cabin wall 27 for placing the penetrating fastener 28 according to the scribing, wherein the welding base 1 needs to embed the nut 2 in the welding base 1 before welding operation, and further welds the stud 37 of the distance plate 36 connected with the triangular region sub-layer insulation module 102 and the triangular region sub-layer planar transition insulation module 90, and of course, welding the welding base 1 penetrating the lower section 10 of the fastener for positioning the planar region sub-layer insulation module 31a and the corresponding stud 37 according to the scribing on the cabin wall in the actual operation process; four through holes are symmetrically arranged at four corners of the distance plate 36 about the central line of the distance plate 36, and each through hole is internally provided with a stud 37 in a penetrating manner;
After the stud 37 and the welding base 1 are installed, the metal connecting rod 3 of the penetrating fastener 28 fixedly connected with the welding base 1 and the installation distance plate 36 on the stud are installed, of course, in the actual operation process, if the installation of the three-angle-zone sub-layer insulation layer module 102 may be affected after the metal connecting rod 3 of the penetrating fastener 28 is completely installed, the metal connecting rod 3 of the penetrating fastener 28 may be installed afterwards or only part of the metal connecting rod 3 of the penetrating fastener 28 is installed, so that the installation of the three-angle-zone sub-layer insulation layer module 102 is not affected, wherein the other corner zones of the corner zone of one side where the three-angle-zone sub-layer insulation layer module 102 is connected are all provided with the distance bolt holes 55 for penetrating the stud 37, and the connection with the plane-angle-zone sub-layer transition layer module 70 is further realized through the distance plate 36.
After the distance plate 36 is sleeved on the stud 37, the stud 37 penetrating through the distance plate 36 is inserted into the distance stud hole 54 formed on the triangular region sublayer plane transition insulating module 90.
After the installation of the stud 37 is completed and the triple-angle zone sub-layer insulation module 102 is installed at the triple-angle zone of the hull structure 26 and is adhered and fixed, the installation of the penetrating fastener 28 is performed, the metal connecting rod 3 of the penetrating fastener 28 is penetrated into the penetrating holes 78 of the four central supporting structures 79 arranged on the triple-angle zone sub-layer plane transition insulation module 90, and the cap rod structure 11 penetrating the upper section 25 of the fastener is screwed and fixed with the upper end of the metal connecting rod 3 and welded to the sub-layer welding metal sheet 4 which is embedded on the second top plate 72.
In this embodiment, one of the four center support structures 79 is located at the center of the cross reinforcement structure 77, two of the four center support structures are respectively located at the extending ends of two adjacent vertical plates in the cross of the cross reinforcement structure 77, the other one of the four center support structures 79 is arranged in a rectangular shape with the three center support structures 79, and is located at one end of the rectangular shape closest to the main insulating layer module 101 in the triangular region, and the four center support structures 79 may be formed by a structural member directly fixedly connected to the cross reinforcement structure 77 or by a center support structure 79 member directly fixedly connected to the bottom plate of the sub-planar transition insulating module 90 in the triangular region;
After the three-sided area sub-insulation layer module 102 and the three-sided area sub-layer planar transition insulation module 90 are installed, the sub-layer film layer 32 is installed, and of course, in the actual process, before the sub-layer film layer 32 is installed, the two-sided area sub-insulation layer module 50 and the two-sided area planar transition sub-layer insulation layer module 70 are completed, the two-sided area sub-insulation layer module 50 comprises a 90 ° two-sided area sub-insulation layer module 50a and a 135 ° two-sided area sub-insulation layer module 50b, and then, simultaneously, the planar area sub-layer insulation layer module 31a is installed, so that the complete sub-layer insulation layer 31 is formed, and then, the sub-layer film layer 32 is installed.
In this embodiment, the sub-layer film layer 32 is made of invar steel or 304L stainless steel or other low temperature resistant metal material prefabricated into a corrugated shape, and the sub-layer film layer 32 may include a plurality of sub-layer films 32a with preset dimensions connected in a splicing manner, specifically, in the corner region where the three sides meet, the sub-layer film 32a is provided with a sub-layer corner region film seal 85, and by sealing and welding the sub-layer corner region film seal 85 onto the metal welding plate 53 of the three-surface corner region sub-layer insulating layer module 102, so that the sub-layer film 32a provided on the planar region sub-layer insulating layer module 31a can overlap the sub-layer film seal 85 to form a complete and sealed sub-layer film layer 32, and then sequentially install the sub-layer films provided on the planar region sub-layer insulating layer module 31a, and in the same manner, for the corner region where the two sides meet, the edge of the corner region transition film 83 of the two-surface corner region sub-layer insulating layer module 50 can be finished first, and then the sub-layer film layer 32 is formed, and the final film layer 32 is formed;
After the installation of the sub-layer film layer 32 is completed, the installation of the main insulating layer module 101 in the triangular area is performed, wherein the main insulating layer module 101 in the triangular area is tightly pressed and fixed with the main insulating layer module 33 in the adjacent planar area or the main insulating layer module 60 in the triangular area through the pressing blocks 21 penetrating through the upper section 25 of the fastening piece, 4 penetrating fastening pieces 28 are configured on the main insulating layer module 101 in the triangular area for pressing connection, and 4 penetrating fastening pieces 28 are respectively arranged at four corners of the main insulating layer module 101 in the triangular area;
after the triangular region main insulating layer module 101, the adjacent two-sided angular region main insulating layer module 60 and the plane region main insulating layer module 33a at the same corner are installed in place, corresponding compression blocks 21 penetrating through fasteners 28 are installed in the corner region, and the bottom metal plates 12 of the compression blocks 21 are simultaneously pressed on a fixed cushion block 65 fixedly arranged on a middle plate 64 of the triangular region main insulating layer module 101, a fixed cushion block 65 fixedly arranged on a middle plate 64 of the two-sided angular region main insulating layer module and a fixed cushion block 65 fixedly arranged on a middle plate 64 of the plane region main insulating layer module 33a, and are fixedly connected with the upper ends of the metal connecting rods 3 and locked and fixed;
After the main insulating layer module 101 in the dihedral corner region is mounted, the main film layer 34 is mounted, and of course, before the main film layer 34 is mounted in the actual operation process, the main insulating layer module in the dihedral corner region and the main insulating layer module 33a in the planar region are mounted, so that the complete main insulating layer 33 is formed, and then the main film layer 34 is mounted.
In this embodiment, the main layer film 34a is made of invar steel or 304L stainless steel or other low-temperature resistant metal material prefabricated into a corrugated shape, when the main layer film 34a in the corner region where three sides meet is mounted, the main layer film 34a adopts a full-coverage mode of the transition film, three corner region main layer corner region transition films 84 which are respectively arranged in parallel with the three mutually upper surfaces of the three corner region main layer insulating layer modules and form included angles, are respectively welded and fixed with each other, and a main layer welding plate 38 for fixing the main layer corner region transition film 84 is arranged below the overlapping position, the main layer welding plate 38 is arranged on the corner region transition clamping plate 35c, before lap welding, one main layer corner region transition film 84 is spot welded on the main layer welding plate 38 on the corner region transition clamping plate 35c, then, two other main layer corner region transition films 84 are welded in sequence, after that, the main layer film on the main layer insulating layer module in the plane region is lapped on the main layer corner region 84, the same circle is formed on the main layer transition region 84, and the two corner region insulating layer modules are welded, and the same edge of the two corner region can be welded, and the two corner region insulating layer modules are completely welded, and the two corner region side regions are completely, and the edge region insulating layer modules are completely welded, and the corner region is completely arranged on the main layer module is formed, and the edge region is completely, and the edge region is welded, and the corner region is completely, and the corner region is sealed, and the corner region is completely sealed, and the edge region is welded.
The above embodiments are only exemplary embodiments of the present invention and are not intended to limit the present invention, the scope of which is defined by the claims. Various modifications and equivalent arrangements of this invention will occur to those skilled in the art, and are intended to be within the spirit and scope of the invention.
Claims (12)
1. The three-face corner area arrangement structure of the film type enclosure system is characterized by comprising a main layer film layer, a fastening clamping plate, a main layer insulating layer, a sub-layer film layer and a sub-layer insulating layer which are sequentially connected and fixed to a ship body structure through penetrating fasteners, wherein the main layer film layer, the main layer insulating layer, the sub-layer film layer and the sub-layer insulating layer are enclosed to form a low-temperature liquid cargo storage tank for accommodating ultralow-temperature medium, and the main layer film layer is in contact with the ultralow-temperature medium; the corner areas where the three side surfaces are connected in the film type enclosure system are provided with triangular area modules, the triangular area modules comprise triangular area main insulating layer modules and triangular area secondary insulating layer modules, wherein,
the three-face-area sub-layer insulating layer module comprises three sub-layer insulating surface structures which are respectively arranged corresponding to three cabin wall surfaces of a three-face-area of a ship body structure, wherein the included angle between any two sub-layer insulating surface structures in the three sub-layer insulating surface structures is determined based on the included angle between corresponding cabin wall surfaces on two sides in the ship body structure, and each three-face-area sub-layer insulating layer module consists of three layers of structures;
The main insulating layer module of the triangular area comprises three main insulating layer structures which are respectively arranged corresponding to three cabin wall surfaces of the triangular area of the hull structure, wherein the included angle between any two main insulating layer structures in the three main insulating layer structures is determined based on the included angle between the cabin wall surfaces of the two corresponding sides in the hull structure, and each main insulating layer module of the triangular area consists of four layers of structures;
the gap at the contact position of the main insulating layer module of the triangular region and the main insulating transition module of the plane region of the main insulating layer and the gap at the contact position of the sub insulating transition module of the triangular region and the plane region of the sub insulating layer are positioned in different planes.
2. The membrane containment system tri-planar angular region arrangement of claim 1, wherein,
each triangular region sub-layer insulating layer module comprises a first bottom plate, a heat insulation block and a metal welding plate which are sequentially adhered and fixed inwards by the wall surface of a ship cabin, wherein an inwards concave stepped notch groove is formed in the upper edge of one side, connected with the triangular region sub-layer planar transition insulating module, of the heat insulation block, an inwards concave installation notch groove which is arranged corresponding to the stepped notch groove is formed in the upper edge of the side, connected with the heat insulation block, of the triangular region sub-layer planar transition insulating module, and when the triangular region sub-layer planar transition insulating module is adhered and fixed with the heat insulation block, the heat insulation block is adhered and fixed with the pressing plate at the top of the installation notch groove through the stepped notch groove; the plane transition insulation module of the triangular region sublayer comprises a second top plate, four heat preservation blocks, a cross reinforcing structure, four central supporting structures and a second bottom plate, wherein the four heat preservation blocks are respectively arranged in four spaces between the second top plate and the second bottom plate, the four spaces are formed by the cross reinforcing structures, and through holes for installing penetrating fasteners are formed in the middle parts of the four central supporting structures.
3. The membrane containment system tri-planar angular region arrangement of claim 2, wherein,
each triangular region main layer insulating layer module comprises a first top plate, an upper heat-insulating block, a middle plate and a lower heat-insulating block, wherein the first top plate is sequentially arranged from the inner side far away from the wall surface of the ship bulkhead to the side close to the wall surface of the ship bulkhead, the triangular region main layer insulating layer module is provided with a mounting notch at the corner connected with the triangular region main insulating layer module, each mounting notch is internally provided with a fixed cushion block fixedly connected with the middle plate, the fixed cushion block is matched with the shape of the mounting notch, and the mounting notch is specifically formed in the lower heat-insulating block of the triangular region main layer insulating layer module.
4. The membrane containment system tri-planar angular region arrangement of claim 3, wherein,
the width dimension of each main layer insulating surface structure in the three main layer insulating surface structures of the main layer insulating surface module in the triangular area is larger than the width dimension of each sub layer insulating surface structure in the sub layer insulating surface module in the triangular area, which is respectively and correspondingly arranged with the three main layer insulating surface structures.
5. The membrane containment system tri-planar angular region arrangement of claim 4, wherein,
And a distance plunger hole for installing a distance plate of the triangular region sub-layer plane transition insulation module is formed in one end of the triangular region main layer insulation module on a step plane parallel to the wall surface of the ship where the step notch groove is positioned.
6. The membrane containment system tri-planar angular region arrangement of claim 5, wherein,
the third-face-area secondary-layer plane transition insulation module further comprises a secondary-layer welding metal sheet, a secondary-layer welding plate, a tabletting heat-insulating block and a tabletting plate, wherein the second top plate is provided with a welding plate groove and a welding plate groove, after the secondary-layer welding plate and the secondary-layer welding metal sheet are respectively installed in the welding plate groove and the welding plate groove, the upper surface of the secondary-layer welding plate and the upper surface of the secondary-layer welding metal sheet are flush with the upper surface of the second top plate, and the secondary-layer welding metal sheet is provided with a connecting hole for installing a penetrating fastener;
the utility model discloses a laminated sheet material, including the second top panel, the second bottom panel, the second top panel, the second bottom panel is last all be equipped with the installation fixed orifices that corresponds the through-hole of central bearing structure on the cross additional strengthening set up, the installation breach groove with the ladder breach groove corresponds the setting when the regional sublayer insulating layer module of three faces with the regional sublayer plane transition insulating module of three faces is connected, ladder breach groove with the bottom preforming panel bonding in installation breach groove is fixed, the preforming heat preservation piece with preforming panel ladder breach groove with the installation breach groove bonding is fixed, the upper portion of preforming heat preservation piece with the second top panel bonding is fixed.
7. The membrane containment system tri-planar angular region arrangement of claim 6, wherein,
when the plane transition insulation module of the sublayer of the triangular area is adhered and fixed with the cabin wall surface of the hull structure through the second bottom plate, strip-shaped epoxy resin is adhered to the cabin wall surface of the hull structure at intervals between the second bottom plate and the cabin wall surface of the hull structure, and the height of the epoxy resin between the second bottom plate and the cabin wall surface of the hull structure is set to be more than 12mm and less than 20mm according to the intervals between the epoxy resins.
8. The membrane containment system tri-planar angular region arrangement of claim 7, wherein,
the distance plate is made of plywood or plastic substitute materials meeting the rigidity requirement, the thickness of the distance plate is at least one of 1mm, 2mm, 5mm or 10mm, the distance plate is used for leveling, and the distance plate overlapping combination with different thickness is adopted, so that the distance between the bottom of the triangular region sub-layer plane transition insulation module and the cabin wall surface is 10mm;
the aperture of the through hole on the distance plate is 0.5-2mm larger than the outer diameter of the thread on the stud.
9. The membrane containment system tri-planar angular region arrangement of claim 8, wherein,
the through fastener includes: a through fastener upper section portion and a through fastener lower section portion, wherein,
the upper section part comprises a cap rod structure, a compression block and an upper end cap rod structure, wherein the compression block is arranged in a triangular region main layer insulating layer module, a planar region main layer insulating layer module and a mounting notch formed in the two-sided region main insulating layer module, a bottom metal plate of the compression block is attached to a fixed cushion block, and a long bolt on the compression block locks the compression block;
the lower section part of the penetrating fastener comprises a cylindrical welding base and a metal connecting rod with threads at two ends, one end of the metal connecting rod penetrates through the sublayer welding metal sheet to be fixedly connected with the cap rod structure, the other end of the metal connecting rod is fixedly welded with the hull structure through the cylindrical welding base, and the metal connecting rod penetrates through a through hole of a central supporting structure of the cross-shaped reinforcing structure on the triangular region sublayer plane transition insulating module.
10. The membrane containment system tri-planar angular region arrangement of claim 9, wherein,
Each cabin wall surface of three cabin wall surfaces in a three-sided corner area of the ship body structure is perpendicular to at least one fixed cushion block, and the fixed cushion blocks are flush with the side surface of one side of the middle plate of the lower heat insulation block.
11. The membrane containment system tri-planar angular region arrangement of claim 10, wherein,
the first top plate, the middle plate, the first bottom plate, the second top plate, the cross reinforcing structure and the second bottom plate are all made of low-temperature-resistant nonmetallic materials with set strength, wherein the low-temperature-resistant nonmetallic materials can at least resist the temperature of 196 ℃ below zero, the strength needs to meet the following requirements, in particular,
the vertical compression strength is more than or equal to 4Mpa, the bending strength is more than or equal to 20Mpa, the horizontal tensile strength is more than or equal to 25Mpa, the vertical tensile strength is more than or equal to 1.5Mpa, and the shearing strength is more than or equal to 2.5Mpa.
The heat insulation block, the upper heat insulation block, the lower heat insulation block, the tabletting heat insulation block and the heat insulation block are all made of materials meeting the set heat conductivity coefficient requirement, wherein the set heat conductivity coefficient requirement is that the heat conductivity coefficient is not more than 0.1W/m.K;
The primary film of the primary film layer and the secondary film of the secondary film layer are made of invar steel or 304L stainless steel or other low-temperature resistant metal materials which are prefabricated into a set corrugated shape.
12. The membrane containment system tri-planar angular region arrangement of claim 11, wherein,
the periphery of the rest parts of the cross reinforcing structure except the pressed sheet material is overlapped with the second top sheet material and is connected with the second top sheet material through glue or rivets;
the periphery of the second bottom plate is overlapped with the cross reinforcing structure except for the mounting notch groove, and is connected with the cross reinforcing structure through glue or rivets;
the contact parts of the heat preservation block, the second top plate, the second bottom plate and the cross reinforcing structure are all fixed by glue;
the tabletting plates are positioned at the bottoms of the mounting notch grooves and are adhered and fixed with the adjacent heat insulation blocks through glue, and the tabletting plates extend out of the second bottom plate in the direction of the wall surface of the cabin parallel to the tabletting plates at the position close to the sub-layer insulating layer module in the triangular area;
the tabletting heat insulation block is positioned between the second top plate and the tabletting plate;
The pressing sheet heat-insulating block is fixedly connected with the contact part of the second top plate, the pressing sheet plate and the heat-insulating block through glue.
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| CN202311521316.0A CN117585121A (en) | 2023-11-14 | 2023-11-14 | Three-face corner area arrangement structure of film type enclosure system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117818820A (en) * | 2024-03-06 | 2024-04-05 | 沪东中华造船(集团)有限公司 | Film type liquid cargo containment system and LNG ship |
| CN117818822A (en) * | 2024-03-06 | 2024-04-05 | 沪东中华造船(集团)有限公司 | Corner area module of film type low-temperature liquid cargo containment system |
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2023
- 2023-11-14 CN CN202311521316.0A patent/CN117585121A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117818820A (en) * | 2024-03-06 | 2024-04-05 | 沪东中华造船(集团)有限公司 | Film type liquid cargo containment system and LNG ship |
| CN117818822A (en) * | 2024-03-06 | 2024-04-05 | 沪东中华造船(集团)有限公司 | Corner area module of film type low-temperature liquid cargo containment system |
| CN117818822B (en) * | 2024-03-06 | 2024-06-11 | 沪东中华造船(集团)有限公司 | Corner area module of film type low-temperature liquid cargo containment system |
| CN117818820B (en) * | 2024-03-06 | 2024-06-11 | 沪东中华造船(集团)有限公司 | Film type liquid cargo containment system and LNG ship |
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