CN102388258B - Improved sealed heat insulation cabin integrated with supporting structure - Google Patents
Improved sealed heat insulation cabin integrated with supporting structure Download PDFInfo
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- CN102388258B CN102388258B CN201080015036.7A CN201080015036A CN102388258B CN 102388258 B CN102388258 B CN 102388258B CN 201080015036 A CN201080015036 A CN 201080015036A CN 102388258 B CN102388258 B CN 102388258B
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- 238000009413 insulation Methods 0.000 title claims abstract description 47
- 238000007789 sealing Methods 0.000 claims abstract description 40
- 239000002184 metal Substances 0.000 claims abstract description 11
- 238000013016 damping Methods 0.000 claims description 23
- 239000000463 material Substances 0.000 claims description 9
- 230000002401 inhibitory effect Effects 0.000 claims description 7
- 230000004888 barrier function Effects 0.000 claims description 6
- 239000012528 membrane Substances 0.000 claims description 6
- 239000002131 composite material Substances 0.000 claims description 5
- 239000002023 wood Substances 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 claims 5
- 239000002390 adhesive tape Substances 0.000 claims 4
- 238000000034 method Methods 0.000 claims 1
- 239000011359 shock absorbing material Substances 0.000 description 6
- 238000010276 construction Methods 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000004964 aerogel Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 239000002648 laminated material Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
Images
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
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/02—Special adaptations of indicating, measuring, or monitoring equipment
-
- 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
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/025—Bulk storage in barges or on ships
- F17C3/027—Wallpanels for so-called membrane tanks
-
- 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
- F17C2201/05—Size
- F17C2201/052—Size large (>1000 m3)
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0358—Thermal insulations by solid means in form of panels
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
-
- 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
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/228—Assembling processes by screws, bolts or rivets
-
- 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
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/23—Manufacturing of particular parts or at special locations
- F17C2209/232—Manufacturing of particular parts or at special locations of walls
-
- 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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
-
- 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
-
- 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/016—Preventing slosh
-
- 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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0102—Applications for fluid transport or storage on or in the water
- F17C2270/0105—Ships
- F17C2270/0107—Wall panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Building Environments (AREA)
- Laminated Bodies (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Thermal Insulation (AREA)
Abstract
The invention provides a cabin body, which comprises two sealing layers, a main sealing layer (10) and a secondary sealing layer (5), and at least one heat insulation layer, wherein the heat insulation layer is formed by at least one module similar to a cuboid shape, a first laminated plate panel (3) is formed by covering a first heat insulation layer film (4), the secondary sealing layer (5) is covered on the first heat insulation layer film, a second heat insulation layer film (6) is arranged on the secondary sealing layer, a second laminated plate panel (7) is arranged on the second heat insulation layer film, the main sealing layer (10) is arranged on the second laminated plate panel, and the main sealing layer is made of metal ferrules or metal plates. The second laminate panel consists of two bulkheads, the first bulkhead supporting the primary seal and the second bulkhead with a layer of cushioning means therebetween. The invention is particularly suitable for shipbuilding.
Description
The invention relates to an improved structure of a sealed heat-insulation cabin integrated with a supporting structure.
Documents FR-2527544-A, FR-1376525-A, FR-1379651-A, FR-2724623-a and FR-2798902-a disclose an insulated sealed cabin integrated with a support structure, in particular a cabin of a marine vessel, having two continuous sealing layers, wherein the cabin inner wall contains a primary sealing layer and a secondary sealing layer is located between the primary sealing layer and the support structure. Between the two sealing layers or between the secondary sealing layers, there is at least one insulating layer. According to the publication, the primary sealing layer is made of metal or a composite material containing a metal core. The insulation layer is formed by juxtaposed, polygonal modules or panels, the thickness of which depends on the required insulation capacity. These modules have a cover layer and a base layer, also commonly referred to as "panels". Wherein primary insulation layer refers to the layer below the primary seal layer and secondary insulation layer refers to the layer below the secondary seal layer.
During use, the main seal made of metal ferrules is damaged most of the time by sloshing, in particular on the top of the hold or in the bearing area above the hold. In addition, the primary insulation layer is subject to wear from the rigid panels that support it.
However, wear of the secondary seal layer or secondary insulation is often reported.
It is therefore an object of the present invention to provide an improved structure of a sealed and insulated cabin integrated with a support structure, such as the hull of a navigation vessel, to avoid or at least reduce damage to the cabin.
It is a further object of the invention to provide an improved structure with as few structural modifications as possible.
An additional object of this improved structure is to not significantly increase the cost of the hold.
It is a further object of the present invention to provide an improved structure for providing a sealed insulated compartment integrated with a support structure at an acceptable cost.
These objects and others which will be mentioned below, are all due to the improved structure of the sealed and thermally insulated cabin integrated with the supporting structure. The support structure comprises a double wall, the enclosure comprising two sealing layers, a primary sealing layer and a secondary sealing layer, and at least one insulating layer integrally formed with the support structure, the secondary sealing layer being disposed within the insulating layer and the primary sealing layer being disposed over the insulating layer. The improvement of the invention is that a damping device consisting of a layer of damping material is arranged between the two cabin walls.
A basic embodiment of the invention is that the insulation layer consists of one cuboid shaped module comprising a first laminated panel. For example, it may be made of a laminate. The top surface of the heat insulation layer is provided with a first heat insulation layer film, a secondary sealing layer is arranged on the first heat insulation layer film and connected with a secondary heat insulation layer arranged on the secondary sealing layer, and a second heat insulation film is arranged on the secondary heat insulation layer to support the second laminated panel. In the known art, a primary seal consisting of a ferrule or sheet metal is provided on a second laminated panel, under which a damping device is provided, consisting of a second laminated panel consisting of two bulkheads. Wherein, a layer of shock-absorbing material is arranged between two layers of bulkheads.
A second embodiment of the invention is that the insulation is composed of a module shaped like a cuboid, for example a laminate. This module constitutes a first laminate panel. On the top surface of the first laminate panel is a first insulation film, on top of which is a secondary sealing layer, on top of which is arranged a second insulation film supporting a second laminate panel, for example a laminate structure. In the known art, a primary seal layer is provided on top of the second heat insulation layer film, the primary seal layer being supported by a metal collar or sheet but the damping means being provided below the secondary seal layer.
A third embodiment of the invention is where the damping means is arranged between the secondary sealing layer and the second heat barrier film.
A fourth embodiment of the invention is where the cushioning means is disposed between the first laminate panel and the first insulation layer membrane.
Preferably, a deflection-inhibiting device is provided between the first and second bulkheads, through the membrane of shock-absorbing material.
Preferably, the deflection-inhibiting means are T-shaped and inserted into upper and lower holes provided in the two bulkheads respectively, the vertical free ends of the T of the two bulkheads being opposite one another, forming an H-shaped fence in the space between the two bulkheads.
Alternatively, the deflection-inhibiting means are inserted into holes in the bulkhead and in the second insulation-layer film, respectively, to form a T-shape, the vertical free ends of the T-shape being opposite one another to form an H-shaped barrier.
Preferably, the junction of the first deck bulkhead is complementary to the junction of the second deck bulkhead.
Preferably, the joints of the first layer bulkheads are of exactly the same construction as the joints of the slats of a parquet floor in the uk.
Preferably, the second deck wall has an elasticity index at least 10% less than the elasticity of the current material.
Preferably, the two layers of the bulkhead have a thickness of between 9 and 21 mm.
In a preferred embodiment of the invention, the two bulkheads are made of fir-wood laminate or of composite material.
Preferably, the first laminate panel is secured to the bulkhead of the support structure by a row of adhesive strips having an elasticity index at-25 ℃ of at most 500MPA and at 25 ℃ of about 150 MPA.
The invention is discussed in detail below with reference to the drawings, but the invention is not limited in any way.
Fig. 1 is a sectional view taken perpendicular to the bulkhead of a support structure comprising double walls or double transverse compartments, the sectional view briefly depicting the collection of parts of the hold described in the previous embodiment, the sectional view being taken away from the corners of the hold.
Fig. 2 is a sectional view taken perpendicular to the bulkhead of the support structure comprising double walls or double transverse compartments, the sectional view briefly depicting the collection of parts of the hold described in the previous embodiment, the sectional view being taken away from the corners of the hold.
Fig. 3 is a schematic view of an alternative embodiment of the invention according to fig. 2.
Fig. 4 is a schematic view of a second embodiment of the present invention.
Fig. 5 is a schematic view of a third embodiment of the present invention.
Fig. 6 is a schematic view of a fourth embodiment of the present invention.
Like parts are indicated by like numerals in the drawings.
And in particular to fig. 1, reference numeral 1 refers to the wall of a double hull of a ship on which the hold provided by the invention is mounted. It is known that the hull of a ship also has transverse bulkheads, which are also double-layered, subdividing the hull into a number of partitions. In this description, "double wall 1" is used to indicate the double wall of the hull and the double wall of the transverse bulkhead, which enclose the individual chambers. The double wall 1 forms the supporting structure of the hold.
The sealed and heat-insulated cabin comprises two sealing layers, a main sealing layer 10 and another secondary sealing layer 5, at least one heat-insulating layer consisting of similar cuboid modules, and a first laminated plate panel 3, wherein the top surface of the first laminated plate panel is provided with a first heat-insulating layer film 6, and the first heat-insulating layer film supports a second laminated plate panel. In the known art, a primary seal layer 10 is provided on the second laminate panel. The secondary seal 5 and the primary seal 10 are made of metal ferrules, preferably of non-expanding steel, or of adjustable metal plates. The first laminated panel 3 and the first heat insulation layer film 4 are combined to form a secondary heat insulation layer module 2 b; the second laminate panel 7 and the second insulation layer film 6 combine to form the primary insulation module 2 a.
From an aesthetic point of view, it is clear that the modules 2a and 2b are approximately rectangular in shape. The module 2a is a rectangle having sides parallel to the module 2b as viewed in a plan view; from a plan view point, modules 2, 2a and 2b, employ a compensating rectangular design to suppress heat leakage and ensure better force sharing.
In a first embodiment of the invention, shown in figures 2 and 3, the damping device is constituted by a second laminated panel 7, positioned below the primary sealing layer 10, which itself is of sandwich construction, comprising:
the first bulkhead 8 is made of laminate or composite material, for supporting the primary seal layer;
-a membrane 11 of shock-absorbing material;
the second tank wall 9, made of laminate, is located above the second insulation film 6.
The laminate thickness of the first bulkhead 8 and the second bulkhead 9 is between 9 and 21 mm. The second deck wall 9 has a cold bend elasticity index of 10000-13000 MPA. The laminate of the present invention is made of, for example, a fir wood laminate or a composite material. The elasticity index of the second layer of the cabin wall is at least 10% smaller than that of the current material.
The membrane 11 of cushioning material is located between two bulkheads 8 and 9 and has a thickness of 2-15mm, for example 8 mm. The thickness is selected to be convenient for absorbing shock on one hand and the shock absorbing material is extruded and cannot be damaged on the other hand under the shaking impact. This material may be felt, a textile fibre material, such as aerogel, with or without insulation. Such materials may be compounds or mixtures.
In a second embodiment of the invention, the damping means is located below the secondary sealing layer 5. As previously described, it is made up of two bulkheads 8 'and 9', between which a film of shock absorbing material is inserted. In this case, one of the two bulkheads, for example 9', is above the first film of insulating material 4 and the bulkhead 8' is below the secondary sealing layer 5.
The junction of the first layer of bulkhead 8 or 8 'is in face-to-face abutment with the junction of the second layer of bulkhead 9 or 9', thus ensuring better mechanical continuity of the insulating module. The joints of the first layer bulkheads 8 or 8' are of the same construction as the joints of the slats of the parquet floor in the uk.
As shown in the alternative embodiment of the invention, the deflection-inhibiting means are interposed between the first bulkhead 8 and the second bulkhead 9 and pass through the membrane 11 of shock-absorbing material. In this exemplary embodiment, the bulkhead has two holes, an upper hole 12a and a lower hole 12b, forming a T-shape, interconnected by the vertical free ends of the T-shape, forming an H-shaped barrier between the two bulkheads.
In an alternative embodiment of the invention, as shown in fig. 3, the holes 12b are not in the second deck wall 9, but in the second insulation layer film 6 of the 2a module, constituting the primary insulation.
The same approach can be used when the damping means is located below the secondary sealing layer 5.
In a third embodiment, shown in figure 5, the damping means 7 are located above the secondary sealing layer 5 and below the second heat barrier film 6.
In a fourth embodiment, shown in figure 6, the damping means are located between the first laminated panel 3 of the secondary insulation 2b and the first insulation film 4 of the module 2 b.
In order to increase the damping capacity, the first laminated panel 3 is fixed to the bulkhead 1 of the supporting structure by a row of adhesive strips 14 having an elasticity index at-25 ℃ of at most 500MPA and at 25 ℃ of about 150 MPA.
The improved structure of the hold provided by the invention has the shock resistance at least 3 times that of the common structure, and therefore, can be applied to marine liquid.
Claims (11)
1. An improved structure of a sealed and thermally insulated cabin integrated with a supporting structure (1), said supporting structure (1) comprising a double wall, said sealed and thermally insulated cabin comprising:
an insulating layer manufactured integrally with the support structure,
a secondary sealing layer (5) placed in the insulating layer, and a primary sealing layer (10) supported by the insulating layer,
wherein the heat insulation layer is composed of parallel modules, each module is respectively in a cuboid shape and comprises a first laminated panel (3), a first heat insulation layer film (4) is arranged on the upper portion of the first laminated panel, a secondary sealing layer (5) is arranged on the upper portion of the first heat insulation layer film, a second heat insulation layer film (6) is arranged on the upper portion of the secondary sealing layer, the second heat insulation layer film supports a second laminated panel (7), the second laminated panel supports a main sealing layer (10), and the main sealing layer is composed of a metal ferrule or a metal plate,
the method is characterized in that: the sealed heat insulation cabin comprises a row of adhesive tapes (14), the elastic coefficient of the adhesive tapes is 500MPa at the highest at-25 ℃, and is 150MPa at 25 ℃, the adhesive tapes are arranged between the double walls of the first laminated panel (3) and the supporting structure (1) to enable the first laminated panel (3) to be attached to the supporting structure (1), wherein the first damping device is formed by the row of adhesive tapes arranged between the first laminated panel (3) and the double walls of the supporting structure (1) and used for buffering the vibration caused by shaking, and the sealed heat insulation cabin further comprises at least one second damping device formed by damping material films arranged between the first layer cabin wall (8, 8') and the second layer cabin wall (9, 9') and used for buffering the vibration caused by shaking.
2. The improved structure of the sealed and insulated compartment of claim 1, wherein: the second damping device is arranged below the main sealing layer (10).
3. The improved structure of the sealed and insulated compartment of claim 1, wherein: and the second damping device is arranged at the lower part of the secondary sealing layer (5) and is used for buffering the vibration caused by shaking.
4. The improved structure of the sealed and insulated compartment of claim 1, wherein: and the second damping device is arranged between the secondary sealing layer (5) and the second heat insulation layer film (6) and is used for buffering vibration caused by shaking.
5. The improved structure of the sealed and insulated compartment of claim 1, wherein: the second damping device is arranged between the first laminated panel (3) and the first heat insulation layer film (4) and is used for buffering vibration caused by shaking.
6. The improved structure of the sealed and insulated cabin according to any one of claims 2 to 5, characterized in that: the deflection-inhibiting means are arranged between the first (8, 8') and second (9, 9') bulkheads in the second damping means and pass through the damping-material membrane (11,11') in the second damping means.
7. The improved structure of the sealed and insulated compartment of claim 6, wherein: the deflection-inhibiting means are inserted in the upper holes (12a) of the first deck walls (8, 8') and the lower holes (12b) of the second deck walls (9, 9') respectively in the second shock-absorbing means, forming a T-shape, and are connected to each other by the vertical free ends of the T-shape, forming an H-shaped barrier (13) between the first deck walls (8, 8') and the second deck walls (9, 9').
8. An improved structure of a sealed and insulated compartment according to claim 6, characterized in that the deflection-inhibiting means are inserted in the upper holes (12a) in the first compartment wall (8, 8') and in the lower holes (12b) in the secondary insulation layer film (6) in the second shock-absorbing means, forming a T-shape, interconnected by the vertical free ends of the T-shape, forming an H-shaped barrier (13) between the first compartment wall (8, 8') and the second compartment wall (9, 9 ').
9. The improvement of a sealed and insulated cabin according to any of claims 3 to 5, characterized in that the junction of the first deck wall (8; 8') and the junction of the second deck wall (9; 9') of the second damping device are in face-to-face abutment.
10. The improved structure of the sealed and insulated cabin according to any one of claims 3 to 5, characterized in that: the thickness of the first layer cabin wall (8; 8') and the second layer cabin wall (9; 9') in the second damping device is between 9 and 21 mm.
11. The improved structure of the sealed and insulated cabin according to any one of claims 3 to 5, characterized in that: the first (8; 8') and second (9; 9') bulkheads of the second damping device are made of a fir-wood laminate or a composite material.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710035583.5A CN107035961B (en) | 2009-04-03 | 2010-04-02 | Improved sealed heat insulation cabin integrated with supporting structure |
CN201410053547.8A CN103770905B (en) | 2009-04-03 | 2010-04-02 | A kind of improved sealing insulated hold integrated with supporting construction |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0901636(FR) | 2009-04-03 | ||
FR0901636A FR2944087B1 (en) | 2009-04-03 | 2009-04-03 | IMPROVEMENT FOR A WATERPROOF AND THERMALLY INSULATING TANK INTEGRATED IN A CARRIER STRUCTURE |
PCT/FR2010/000283 WO2010112715A1 (en) | 2009-04-03 | 2010-04-02 | Improvement for leaktight and thermally insulating tank integrated into a carrier structure |
Related Child Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710035583.5A Division CN107035961B (en) | 2009-04-03 | 2010-04-02 | Improved sealed heat insulation cabin integrated with supporting structure |
CN201410053547.8A Division CN103770905B (en) | 2009-04-03 | 2010-04-02 | A kind of improved sealing insulated hold integrated with supporting construction |
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CN102388258A CN102388258A (en) | 2012-03-21 |
CN102388258B true CN102388258B (en) | 2020-06-12 |
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CN201410053547.8A Active CN103770905B (en) | 2009-04-03 | 2010-04-02 | A kind of improved sealing insulated hold integrated with supporting construction |
CN201710035583.5A Active CN107035961B (en) | 2009-04-03 | 2010-04-02 | Improved sealed heat insulation cabin integrated with supporting structure |
CN201080015036.7A Active CN102388258B (en) | 2009-04-03 | 2010-04-02 | Improved sealed heat insulation cabin integrated with supporting structure |
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CN201410053547.8A Active CN103770905B (en) | 2009-04-03 | 2010-04-02 | A kind of improved sealing insulated hold integrated with supporting construction |
CN201710035583.5A Active CN107035961B (en) | 2009-04-03 | 2010-04-02 | Improved sealed heat insulation cabin integrated with supporting structure |
Country Status (13)
Country | Link |
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EP (3) | EP2733410A3 (en) |
JP (1) | JP5226152B2 (en) |
KR (3) | KR20140034943A (en) |
CN (3) | CN103770905B (en) |
AU (1) | AU2010231273B2 (en) |
BR (1) | BRPI1015110B1 (en) |
ES (1) | ES2789373T3 (en) |
FR (1) | FR2944087B1 (en) |
MY (2) | MY174989A (en) |
PH (1) | PH12014502160B1 (en) |
RU (1) | RU2498150C2 (en) |
SG (2) | SG2014012793A (en) |
WO (1) | WO2010112715A1 (en) |
Families Citing this family (8)
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FR2991660B1 (en) * | 2012-06-07 | 2014-07-18 | Gaztransp Et Technigaz | THERMALLY INSULATED, THERMALLY INSULATED TANK-INSULATING ELEMENT COMPRISING A REINFORCED COVER PANEL |
FR3000042B1 (en) * | 2012-12-21 | 2015-01-23 | Gaztransp Et Technigaz | SEALED AND THERMALLY INSULATED TANK |
CN104670425B (en) * | 2014-12-31 | 2017-02-22 | 浙江欣海船舶设计研究院有限公司 | Refrigeration and insulation arrangement process of fishery cargo ship |
FR3042843B1 (en) * | 2015-10-23 | 2018-04-27 | Gaztransport Et Technigaz | TANK COMPRISING INSULATION BLOCKS OF CORNER EQUIPPED WITH RELAXATION SLOTS |
MA43142B1 (en) * | 2015-11-02 | 2019-12-31 | Aislamientos Suaval S A | Thermal insulation system for tanks and industrial equipment at high temperatures |
CN107719584A (en) * | 2017-10-11 | 2018-02-23 | 德清德航游艇制造有限公司 | Pleasure-boat structure |
CN112498583A (en) * | 2020-10-30 | 2021-03-16 | 沪东中华造船(集团)有限公司 | Thin film type enclosure system and LNG ship |
CN113460222B (en) * | 2021-08-19 | 2024-02-02 | 大连船舶重工集团有限公司 | Split type secondary screen wall of B-type storage cabin |
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- 2010-04-02 SG SG2014012793A patent/SG2014012793A/en unknown
- 2010-04-02 WO PCT/FR2010/000283 patent/WO2010112715A1/en active Application Filing
- 2010-04-02 CN CN201410053547.8A patent/CN103770905B/en active Active
- 2010-04-02 KR KR1020147005292A patent/KR20140034943A/en active Application Filing
- 2010-04-02 EP EP14155237.2A patent/EP2733410A3/en not_active Withdrawn
- 2010-04-02 CN CN201710035583.5A patent/CN107035961B/en active Active
- 2010-04-02 MY MYPI2011004696A patent/MY174989A/en unknown
- 2010-04-02 CN CN201080015036.7A patent/CN102388258B/en active Active
- 2010-04-02 EP EP10714908A patent/EP2414723A1/en not_active Ceased
- 2010-04-02 EP EP16190487.5A patent/EP3156714B1/en active Active
- 2010-04-02 KR KR1020117026261A patent/KR20120004509A/en active Search and Examination
- 2010-04-02 SG SG2011072352A patent/SG175059A1/en unknown
- 2010-04-02 ES ES16190487T patent/ES2789373T3/en active Active
- 2010-04-02 MY MYPI2014000660A patent/MY172263A/en unknown
- 2010-04-02 BR BRPI1015110-9A patent/BRPI1015110B1/en not_active IP Right Cessation
- 2010-04-02 KR KR1020167004759A patent/KR102062837B1/en active IP Right Grant
- 2010-04-02 JP JP2012502732A patent/JP5226152B2/en not_active Expired - Fee Related
- 2010-04-02 RU RU2011144258/06A patent/RU2498150C2/en active
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Also Published As
Publication number | Publication date |
---|---|
KR20140034943A (en) | 2014-03-20 |
KR102062837B1 (en) | 2020-01-06 |
EP2733410A3 (en) | 2018-03-14 |
CN107035961B (en) | 2020-09-29 |
CN107035961A (en) | 2017-08-11 |
FR2944087A1 (en) | 2010-10-08 |
SG175059A1 (en) | 2011-11-28 |
ES2789373T3 (en) | 2020-10-26 |
EP3156714B1 (en) | 2020-03-25 |
EP3156714A1 (en) | 2017-04-19 |
FR2944087B1 (en) | 2011-04-08 |
EP2733410A2 (en) | 2014-05-21 |
MY174989A (en) | 2020-05-31 |
EP2414723A1 (en) | 2012-02-08 |
CN103770905A (en) | 2014-05-07 |
AU2010231273B2 (en) | 2013-11-14 |
RU2498150C2 (en) | 2013-11-10 |
BRPI1015110B1 (en) | 2020-08-25 |
MY172263A (en) | 2019-11-20 |
JP2012522944A (en) | 2012-09-27 |
CN102388258A (en) | 2012-03-21 |
AU2010231273A1 (en) | 2011-10-27 |
PH12014502160A1 (en) | 2016-09-26 |
KR20120004509A (en) | 2012-01-12 |
KR20160027248A (en) | 2016-03-09 |
WO2010112715A1 (en) | 2010-10-07 |
CN103770905B (en) | 2017-03-01 |
JP5226152B2 (en) | 2013-07-03 |
PH12014502160B1 (en) | 2016-09-26 |
BRPI1015110A2 (en) | 2016-04-12 |
RU2011144258A (en) | 2013-05-10 |
SG2014012793A (en) | 2014-06-27 |
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