CN107035961B - Improved sealed heat insulation cabin integrated with supporting structure - Google Patents

Improved sealed heat insulation cabin integrated with supporting structure Download PDF

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Publication number
CN107035961B
CN107035961B CN201710035583.5A CN201710035583A CN107035961B CN 107035961 B CN107035961 B CN 107035961B CN 201710035583 A CN201710035583 A CN 201710035583A CN 107035961 B CN107035961 B CN 107035961B
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China
Prior art keywords
layer
heat insulation
insulation layer
damping device
sealing layer
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CN201710035583.5A
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CN107035961A (en
Inventor
布鲁诺·古尔顿
拉斐尔·普鲁尼尔
克里斯多夫·乌昂·德·柯玛代克
布鲁诺·德莱特
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Gaztransport et Technigaz SA
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Gaztransport et Technigaz SA
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Classifications

    • 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
    • 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
    • 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

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

Improved sealed heat insulation cabin integrated with supporting structure
The application is a divisional application of No. 201080015036.7 Chinese application; the application numbers of the original applications are: 201080015036.7, filing date: 2010-04-02, invention name: an improved sealed insulated cabin integrated with a support structure.
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 made integral 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.
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-shape 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 diagram of a second embodiment useful for understanding the contents 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 perspective, the modules 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 and/or composite material, and supports the primary seal;
-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 deck wall 9 is at least 10% less than 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.
According to a second embodiment, which is advantageous for understanding the content of the invention, the damping means are located below the secondary sealing layer 5. As previously described, it is made up of two bulkheads 8 'and 9', between which a film 11 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 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 tank with the improved structure of the invention has at least 3 times greater shock resistance to liquid impact from the inboard side than the conventional structure.

Claims (8)

1. A hermetically insulated compartment integrated with a support structure (1), the support structure (1) comprising a double wall, the hermetically insulated compartment comprising:
a thermally insulating layer manufactured integrally with the support structure (1),
a secondary sealing layer (5) placed in the insulating layer, and a primary sealing layer (10) supported by the insulating layer,
the heat insulation layer comprises a secondary heat insulation layer arranged at the lower part of the secondary sealing layer (5) and a primary heat insulation layer arranged on the secondary sealing layer, the secondary sealing layer (5) consists of a metal ferrule or a metal plate, the primary sealing layer (10) consists of a metal ferrule or a metal plate, and the primary sealing layer depends on the primary heat insulation layer; the primary and secondary insulation layers are respectively built into parallel modules, one module of the secondary insulation layer is arranged in a cuboid shape and comprises a first laminated panel (3), and a first insulation layer film (4) is arranged on the upper part of the first laminated panel; a module of main insulating layer is set up to cuboid shape, its characterized in that: the module of the main heat insulation layer comprises a second heat insulation layer film (6), the upper part of the second heat insulation layer film is provided with a damping device (7) for reducing impact caused by shaking, and the damping device forms a sandwich structure; damping device upper portion is main sealing layer (10), sandwich structure includes first layer bulkhead (8) of making by china fir plywood or combined material, second floor bulkhead (9) of making by china fir plywood or combined material and locate damping material layer (11) between first layer bulkhead and the second floor bulkhead, the thickness of damping material layer (11) is 2-15mm, damping material layer (11) are made by felt or based on textile fiber's material.
2. The sealed, insulated compartment of claim 1, wherein: a deflection-inhibiting device is arranged between the first and second deck walls (8, 9') in the damping device, said deflection-inhibiting device passing through the layer (11) of damping material in the damping device.
3. The sealed, insulated compartment of claim 2, wherein: the deflection restraining device comprises: holes (12a, 12b) in the first (8, 8') and second (9, 9') bulkheads, respectively, in the damping device, and each hole forming a T-shape, respectively, wherein the vertical free ends of the T-shapes are arranged face to face, so that an H-shaped barrier (13) is formed between the bulkheads and inserted into the holes.
4. The sealed, insulated compartment of claim 2, wherein the means for inhibiting deflection comprises: an upper opening (12a) in a first bulkhead (8, 8') and a lower opening (12b) in a second insulation film (6) each arranged in a shock-absorbing device, each opening forming a T-shape, wherein the vertical free end faces of the T-shapes are arranged opposite each other, so that an H-shaped barrier (13) is formed between the two bulkheads and inserted into the upper and lower openings.
5. A sealed and insulated cabin according to any of claims 1 to 3, characterized in that the connection of the first deck walls (8, 8') of the damping device is in face-to-face abutment with the connection of the second deck walls (9, 9') of the damping device.
6. A sealed and insulated cabin according to any of claims 1 to 3, characterized in that: the thickness of the first layer of cabin wall (8, 8') and the second layer of cabin wall (9, 9') in the damping device is between 9 and 21 mm.
7. A sealed and insulated cabin according to any of claims 1 to 3, characterized in that: the first (8, 8') and second (9, 9') bulkheads of the damping device are made of fir wood laminate or composite material.
8. A sealed and insulated cabin according to any of claims 1 to 3, characterized in that: the first laminated panel (3) is fixed to the double wall (1) of the support structure by means of an adhesive strip (14) having an elasticity index of at most 500MPA at-25 ℃ and of about 150MPA at 25 ℃.
CN201710035583.5A 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure Active CN107035961B (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR0901636FR 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
CN201080015036.7A CN102388258B (en) 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CN201080015036.7A Division CN102388258B (en) 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure

Publications (2)

Publication Number Publication Date
CN107035961A CN107035961A (en) 2017-08-11
CN107035961B true CN107035961B (en) 2020-09-29

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Family Applications (3)

Application Number Title Priority Date Filing Date
CN201080015036.7A Active CN102388258B (en) 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure
CN201710035583.5A Active CN107035961B (en) 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure
CN201410053547.8A Active CN103770905B (en) 2009-04-03 2010-04-02 A kind of improved sealing insulated hold integrated with supporting construction

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Application Number Title Priority Date Filing Date
CN201080015036.7A Active CN102388258B (en) 2009-04-03 2010-04-02 Improved sealed heat insulation cabin integrated with supporting structure

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN201410053547.8A Active CN103770905B (en) 2009-04-03 2010-04-02 A kind of improved sealing insulated hold integrated with supporting construction

Country Status (13)

Country Link
EP (3) EP2414723A1 (en)
JP (1) JP5226152B2 (en)
KR (3) KR20120004509A (en)
CN (3) CN102388258B (en)
AU (1) AU2010231273B2 (en)
BR (1) BRPI1015110B1 (en)
ES (1) ES2789373T3 (en)
FR (1) FR2944087B1 (en)
MY (2) MY174989A (en)
PH (1) PH12014502160A1 (en)
RU (1) RU2498150C2 (en)
SG (2) SG2014012793A (en)
WO (1) WO2010112715A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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PH12014502160B1 (en) 2016-09-26
CN107035961A (en) 2017-08-11
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CN103770905B (en) 2017-03-01
SG175059A1 (en) 2011-11-28
KR20160027248A (en) 2016-03-09
EP2414723A1 (en) 2012-02-08
MY172263A (en) 2019-11-20
WO2010112715A1 (en) 2010-10-07
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AU2010231273A1 (en) 2011-10-27
BRPI1015110B1 (en) 2020-08-25
JP5226152B2 (en) 2013-07-03
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AU2010231273B2 (en) 2013-11-14
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SG2014012793A (en) 2014-06-27
PH12014502160A1 (en) 2016-09-26

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