WO2018130051A1 - Tank container - Google Patents

Tank container Download PDF

Info

Publication number
WO2018130051A1
WO2018130051A1 PCT/CN2017/117347 CN2017117347W WO2018130051A1 WO 2018130051 A1 WO2018130051 A1 WO 2018130051A1 CN 2017117347 W CN2017117347 W CN 2017117347W WO 2018130051 A1 WO2018130051 A1 WO 2018130051A1
Authority
WO
WIPO (PCT)
Prior art keywords
heat insulation
layer
tank
reflective
cylinder body
Prior art date
Application number
PCT/CN2017/117347
Other languages
French (fr)
Inventor
Xiaodong WEI
Xi Liu
Zhangquan Zhu
Chunrong YAO
Yujie SHI
Original Assignee
Nantong Cimc Tank Equipment Co., Ltd.
China Internationa Marine Containers (Group) Ltd.
Cimc Enric Investment Holdings (Shenzhen) Co., Ltd.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nantong Cimc Tank Equipment Co., Ltd., China Internationa Marine Containers (Group) Ltd., Cimc Enric Investment Holdings (Shenzhen) Co., Ltd. filed Critical Nantong Cimc Tank Equipment Co., Ltd.
Publication of WO2018130051A1 publication Critical patent/WO2018130051A1/en

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/12Arrangements or mounting of devices for preventing or minimising the effect of explosion ; Other safety measures
    • F17C13/123Arrangements or mounting of devices for preventing or minimising the effect of explosion ; Other safety measures for gas bottles, cylinders or reservoirs for tank vehicles or for railway tank wagons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/001Thermal insulation specially adapted for cryogenic vessels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0109Shape cylindrical with exteriorly curved end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05Size
    • F17C2201/054Size medium (>1 m3)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0308Radiation shield
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0308Radiation shield
    • F17C2203/032Multi-sheet layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0325Aerogel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0329Foam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0329Foam
    • F17C2203/0333Polyurethane
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0337Granular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0607Coatings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0617Single wall with one layer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0619Single wall with two layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0646Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • F17C2203/0673Polymers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0675Synthetics with details of composition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/068Special properties of materials for vessel walls
    • F17C2203/0692Special properties of materials for vessel walls transparent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/068Special properties of materials for vessel walls
    • F17C2203/0697Special properties of materials for vessel walls comprising nanoparticles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0103Exterior arrangements
    • F17C2205/0107Frames
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/2109Moulding
    • F17C2209/2136Moulding using wax moulds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/225Spraying
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/035Propane butane, e.g. LPG, GPL
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107Single phase
    • F17C2223/013Single phase liquid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/012Reducing weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/017Improving mechanical properties or manufacturing by calculation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/02Improving properties related to fluid or fluid transfer
    • F17C2260/021Avoiding over pressurising
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/03Dealing with losses
    • F17C2260/031Dealing with losses due to heat transfer
    • F17C2260/033Dealing with losses due to heat transfer by enhancing insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0171Trucks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0165Applications for fluid transport or storage on the road
    • F17C2270/0168Applications for fluid transport or storage on the road by vehicles
    • F17C2270/0173Railways

Definitions

  • the disclosure relates to the field of logistics transportation, more specifically to a storage and transportation container and even more specifically to a tank container.
  • a storage and transportation container is mainly used for storging and transporting material, eg. liquefied petroleum gas, ammonia, refrigerant and other non-refrigeration gas.
  • the storage and transportation container can be a tank container.
  • the tank container is usually designed to meet the standard of ISO tank container according to the international transport regulation (eg. IMDG-International Maritime Dangerous Goods Code, ADR-European Agreement on the international carriage of dangerous goods, China standard JB/T 4781- "liquefied gas tank container” , etc. ) .
  • IMDG-International Maritime Dangerous Goods Code e.g. IMDG-International Maritime Dangerous Goods Code
  • ADR-European Agreement on the international carriage of dangerous goods
  • China standard JB/T 4781- "liquefied gas tank container” e.g. IMDG-International Maritime Dangerous Goods Code, ADR-European Agreement on the international carriage of dangerous goods, China standard JB/T 4781- "liquefied gas tank container” , etc.
  • ISO tank container generally includes a frame and a tank located in the frame.
  • the tank includes a cylinder body and two sealing heads configured to seal two ends opening of the cylinder body respectively.
  • the tank itself and all the connecting piece and device must be arranged within the range of ISO standard specified size.
  • the size of outside frame of 20 feet tank container is 8 feet (2438 mm) in width, 20 feet in longth and 8.5 feet in height.
  • the cylinder body When the medium in the tank container is the liquefied gas, which is marked in domestic and international standards and specifications (international standards- “IMDG” , “ADR” , and China standard JB/T 4781) , eg. liquefied petroleum gas, refrigerant, ect, the cylinder body should have enough thickness to bear the maximum allowable working pressure (MAWP) .
  • MAWP maximum allowable working pressure
  • the minimum thickness of the cylinder body is usually calculated according to the standard of the pressure vessel (eg. according to ASME Section VIII, Division 2, AD 2000 Merkblatt, EN 13445, CODAP 2005 or others) .
  • the “t” represents minimum thickness of the cylinder body.
  • the “D” represents inner diameter of the cylinder body.
  • the “P” represents design pressure.
  • the “E” represents welding coefficient, with its value between 0.85 to 1.
  • the “S” represents the value of allovable stress under design temperature.
  • the design pressure “P” of the cylinder body should not be less than the maximum allowable working pressure (MAWP) .
  • the value of maximum allowable working pressure (MAWP) is related to absolute steam pressure of non refrigant liquiefied gas under the design reference temperature. The lower of the design reference temperature, the lower the absolute steam pressure of non refrigant liquiefied gas will be, the lower maximum allowable working pressure will be, and the lower the design pressure will be.
  • the design reference temperature of the cylinder body should be designed to 60°C. Having shading device, the design reference temperature of the cylinder body should be designed to 55°C. Having heating insulating layer, the design reference temperature of the cylinder body should be designed to 50°C.
  • a shading plate 102 is disposed on the top of the tank 101 to shade the tank 101 from direct sunshine and avoid the temperature rising in the tank.
  • the design reference temperature of the cylinder body should be designed to 55°C, that is, the design pressure of the cylinder body deceases compared with the cylinder body without shading device.
  • This design reference temperature can be reduced to 50 °C by employing a complete tank insulation.
  • the weight of the shading plate is more than 80kg, which increases the net weight of the tank container and a suitable insulation (including insulation and a insulation cladding) adds an additional weight of about 200 kg.
  • a storage and transportation container includes a tank and a heat insulation and reflective layer.
  • the tank includes a cylinder body and two sealing heads configured to seal two end openings of the cylinder body respectively;
  • the heat insulation and reflective layer is disposed on the outer surface of the tank.
  • the heat insulation and reflective layer at least covers an upper surface of the cylinder body including a top surface of the cylinder body and a part of side surface extending from the top surface.
  • the heat insulation and reflective layer covers an area of the cylinder body at least one third of the total area.
  • a heat insulation and reflective layer is coated on the tank, the heat insulation and reflective layer at least coveres the upper surface, the coverage area of the heat insulation and reflective layer at least covers one third of the total area of the cylinder body.
  • the heat insulation and reflective layer has high reflectivity to sunshine, the sunshine shining on the surface of the tank may be well reflected back. Whereby, the technical solution provided in this disclosure may totally replace the shading device used in the prior art. Meanwhile, the heat insulation and reflective layer has good heat insulating effect, which may obviously reduce heat transmission between the tank and outerspace, thereby reduce liquid vaporization as the rise of the temperature within the tank, keeping the pressure from rising, and avoiding potential risk caused by high pressure within the tank. Therefore, compared to the traditional shading plate, the heat insulation and reflective layer is thinner and lighter, accordingly the net weight of the storage and transportation container reduces obviously.
  • Fig. 1 is a perspective view showing a shading plate disposed on the top of a tank container in the prior art.
  • Fig. 2a is a perspective view of a tank container according to the first embodiment of the present disclosure.
  • Fig. 2b is a view showing partial enlargement of A district of Fig. 2a.
  • Fig. 3a is perspective view of a tank container according to the second embodiment of the present disclosure.
  • Fig. 3b is a view showing partial enlargement of B district of Fig. 3a.
  • Fig. 4a is perspective view of a tank container according to the third embodiment of the present disclosure.
  • Fig. 4b is a view showing partial enlargement of C district of Fig. 4a.
  • Fig. 5a is perspective view of a tank container according to the fourth embodiment of the present disclosure.
  • Fig. 5b is a view showing partial enlargement of D district of Fig. 5a.
  • the embodiment of the freight container comprises a vessel for retaining the pressurized liquid within a shell comprising a cylindrical section and heads enclosing opposite ends of the cylindrical section, a frame connected to the vessel to transmit operational loads between the vessel and handling devices at least one opening for filling and/or discharging the vessel, a thermal system covering not less than the upper third of an outer surface of the shell, wherein the thermal system provides an insulation effect which is at least equivalent to the insulation effect of a shield separated from the outer surface of the shell by an airspace of not less than 40 mm, and the thermal system comprises a thermal coating comprising a heat-reflective, heat-absorbing and/or insulating liquid based material containing insulating, heat-absorbing and/or reflecting particles.
  • the thermal system is provided which achieves an insulation effect which is at least equivalent to the insulation effect of a shield separated from the outer surface of the shell by an airspace of not less than 40 mm.
  • this thermal system is achieved by a thermal coating comprising a liquid based material containing insulating, heat-absorbing and/or reflective particles. Therefore the thermal properties are achieved by a material which is added and/or included into a painting material (matrix) .
  • the particles provide insulating, heat-absorbing and/or reflecting properties.
  • the particles comprise ceramic and/or nano-particles.
  • Such particles or nano-particles may comprise silicate or tombarthite particles which increase the insulating quality of such a coating.
  • the coating comprises irregular silicate particles 5 to 100 ⁇ m in seize.
  • the coating may comprise fine non-metallic hollow microspheres which have a high reflectivity for light and/or infrared radiation and form numerous small cavities inside the coating layers (similar to a foam structure) which decrease the thermal conduction of the coating.
  • hollow beads or spherical beads therefore combine reflecting and insulating features.
  • the insulating/reflecting particles may contain thermochromic dyes, particularly in the form of microcapsules, containing special dyes which changes its colour due to a change of temperature and/or radiation.
  • thermochromic dyes may for example change their colour from dark (low reflective) to bright (high reflective) under the influence of sun radiation and/or an increase of the surface temperature due to such radiation.
  • the insulating/reflecting/thermo-active particles may contain particles with a latent heat storage function by exploiting the enthalpy of a reversible thermodynamic state, in particular solid to liquid or vice versa. They take up a lot of heat energy (irradiated by the sun) and convert it into the so called “heat of fusion” without changing the temperature. This process is reversible and the storage medium releases the same amount of heat energy during solidification (e.g. during the night) .
  • Latent heat storage material is available in the form of microencapsulated particles containing a latent heat storing substance (e.g. based on a paraffin wax) .
  • thermal coating is based on a white or translucent matrix based on a component selected from epoxy resins, polyurethanes, acrylates, styrene acrylates, silicone polymers, polyester resins, and/or natural resins and other components suitable of forming a coating matrix.
  • the thermal insulating coating comprises an outer surface having a high emissivity which allows for a high irradiation of heat from the container vessel itself, i.e. from the container vessel surface.
  • a surface having a high emissivity can be formed by a special coating layer and/or may be formed by a sheet layer and/or a membrane layer which is applied to the coating in a wrapping and/or plating process.
  • Such a sheet layer may be formed by a thin, highly reflective metal foil (e.g. aluminium foil) and/or by a metalized plastic tape or foil. It may also be formed by a fiber reinforced foil or membrane having increased mechanically properties.
  • Such a membrane sheet and/or membrane layer may also contain an adhesive layer which is suitable to fix the layer or sheet onto the coating layer.
  • the outer surface may also be formed from a non-metallic bead coating with high reflective bead components.
  • the thermal system provides an insulation effect which is at least equivalent to the insulation effect of a complete cladding of the vessel having a thermal conductance of not more than 0,67 Wm -2 K -1 .
  • Such a thermal system is able to replace a complete thermal insulation which usually comprises an insulation layer of more than 20 mm. If the thermal system according to the present invention is designed accordingly it is possible to gain an diameter increasement which results in an additional volume for a 20’ISO container.
  • the storage and transportation container of the present disclosure may be applied to transportable pressure vessel, more specifically to the vessel for transporting non-refrigeration liquid gas.
  • transportable pressure vessel more specifically to the vessel for transporting non-refrigeration liquid gas.
  • the disclosure will be explained by exampling of a tank container for transporting liquefied petroleum gas.
  • Fig. 2a is a perspective view of a tank container according to the first embodiment of the present disclosure.
  • the tank container 10 includes a frame 11 and a tank 12 disposed in the frame 11.
  • the tank 12 includes a cylinder body 121 and two sealing heads 122 for sealing the two end openings of the cylinder body 121 respectively.
  • the upper surface of the cylinder body 121 is covered by a heat insulation and reflective layer 13.
  • the area of the upper surface represents one third of the total area of the cylinder body 121, that is, the coverage erea of the heat insulation and reflective layer 13 represents one third of the total area of the cylinder body 121.
  • the upper surface of the cylinder body includes a top surface of the cylinder body and a portion of side surface extending from the top surface. The total area of the top surface and the part of side surface represents one third of the total area of the cylinder body 121.
  • the heat insulation and reflective layer 13 has heat insulation and reflective function.
  • the heat insulation and reflective layer 13 is a single layer structure.
  • the single layer structure includes a plurality of non-metal hollow microspheres 131 having heat insulation and reflective function.
  • the matrix of the heat insulation and reflective layer 13 may be a high polymer material layer.
  • the heat insulation and reflective layer 13 may be composed of resin matrix and non-metal hollow microspheres filled in the resin matrix.
  • the non-metal hollow microspheres 131 may produce sphere prism reflection effect, which may reduce sunshine energy invading into the tank, thus achieving the reflecting effect to sunshine.
  • a large number of hollow structures of non-metal hollow microspheres 131 form a heat insulation layer to stop heat conduction, thereby achieving the heat insulation effect.
  • non-metal hollow microspheres 131 may reflect sunshine
  • the non-metal hollow microspheres 131 disposed on the upper surface of the cylinder body 121 may reflect visible light and infrared ray. Therefore the heat insulation and reflective layer 13 may have function of the shading plate.
  • the diameter of the non-metal hollow microsphere 131 may be between 5um to 100um.
  • the non-metal hollow microsphere 131 may be a glass hollow microsphere, a ceramic hollow microsphere or other non-metal hollow sphere. These hollow spheres 131 perform as insulating and reflecting particles.
  • the hollow space which is filled by a gas, increases the insulating capacity of the reflective layer 13 because the thermal conductance of gases is much lower than the thermal conductance of a solid or liquid.
  • the hollow spheres 131 also reflect visible light and/or infrared irradiation at their outer and/or inner surfaces and therefore keep the radiation away from the cylinder body 121 and therefore operate like an internal sunshield.
  • the heat insulation and reflective layer is a coating layer formed on the cylinder body 121 by brush coating or spray coating.
  • the thickness of the coating layer is between 0.1mm to 2mm.
  • the heat insulation and reflective layer may be a thin pasting-film or a thin blanket (e.g. a sheet layer or membrane layer formed from a metallic or metallized foil with high reflectivity/emissivity) .
  • the thin pasting-film or the thin blanket is bonded to the cylinder body 121 by pasting.
  • the thickness of the pasting-film or the thin blanket is between 0.1mm to 10mm.
  • titanium dioxide may be added into the resin matrix.
  • FIG. 3a is perspective view of a tank container according to the second embodiment of the present disclosure.
  • Fig. 3b is a view showing partial enlargement of B district of Fig. 3a.
  • the tank container 20 includes a frame 21 and a tank 22 disposed in the frame 21.
  • the tank 22 includes a cylinder body 221 and two sealing heads 222 configured to seal the two end openings of the cylinder body 221 respectively.
  • the upper surface of the cylinder body 221 is covered by a heat insulation and reflective layer 23.
  • the area of the upper surface represents one third of the total area of the cylinder body 221, that is, the coverage area of the heat insulation and reflective layer 23 represents one third of the total area of the cylinder body 221.
  • the upper surface of the cylinder body 221 includes a top surface of the cylinder body and a portion of side surface extending from the top surface. The total area of the top surface and the part of side surface represents one third of the total area of the cylinder body 221.
  • the heat insulation and reflective layer 23 has heat insulation and reflective function.
  • the heat insulation and reflective layer 23 is a double-layer structure.
  • the heat insulation and reflective layer 23 includes a heat insulation inner layer 231 and a reflective outer layer 232.
  • the heat insulation inner layer 231 is made of heat-preservation material, and the heat-preservation material may be selected from any one from silicate, rare earth and aerogel. But not limited to these kinds of material, the heat-preservation material may also be other material with function of heat preservation or heat insulation.
  • the reflective outer layer 232 may form a reflecting surface on the surface of the heat insulation inner layer 231 to achieve reflecting effect.
  • the reflective outer layer 232 may be made of reflective material.
  • the reflective material may be fluorocarbon coating.
  • the fluorocarbon coating may be composed of 4F type fluororesin and special heat insulation material. In case that the fluorocarbon coating forms a film, a coating film which has high reflectivity and high themal resistance is formed. When the sunshine shines on the coating film, major of energy of the sunshine will be reflected back, and is prevented from transmiting into the tank.
  • the reflective material is not limited to the fluorocarbon coating, but other reflective material.
  • the heat insulation inner layer 231 and the reflecting layer 232 may be coated on the tank 22 by many kinds of manners.
  • the heat insulation inner layer 231 is a coating layer formed on the cylinder body 121 by brush coating or spray coating of heat-preservation material.
  • the reflective outer layer 232 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 231 by pasting.
  • the total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10mm.
  • the heat insulation inner layer 231 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the cylinder body 121 by pasting.
  • the reflective outer layer 232 is a coating layer formed on the heat insulation inner layer 231 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10mm.
  • the heat insulation inner layer 231 is a coating layer formed on the cylinder body 121 by brush coating or spray coating of heat-preservation material.
  • the reflective outer layer 232 is a coating layer formed on the heat insulation inner layer 231 by brush coating or spray coating of fluorocarbon material.
  • the total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 2 mm.
  • the heat insulation inner layer 231 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the cylinder body 121 by pasting.
  • the reflective outer layer 232 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 231 by pasting.
  • the total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10 mm.
  • a heat insulation and reflective layer is coated on the tank, the heat insulation and reflective layer at least coveres the upper surface, the coverage area of the heat insulation and reflective layer at least covers one third of the total area of the cylinder body.
  • the heat insulation and reflective layer has high reflectivity to sunshine, the sunshine shining on the surface of the tank may be well reflected back.
  • the technical solution provided in this disclosure may totally replace the shading device used in the prior art.
  • the heat insulation and reflective layer has good heat insulating effect, which may obviously reduce heat transmission between the tank and outerspace, thereby reduce liquid vaporization as the rise of the temperature within the tank, keeping the pressure from rising, and avoiding potential risk caused by high pressure within the tank.
  • the heat insulation and reflective layer is not easy to be damaged, and the durability of the heat insulation and reflective layer increases at least 30%.
  • the design reference temperature of the tank may reduce from 60°C to 55°C.
  • the design reference temperature has reduced, the design pressure also has reduced, and accordingly the safety of the tank increases.
  • the heat insulation and reflective layer itself is thin, of which the thickness is between 0.1mm to 10 mm, compared to the conventional shading plate of the weight of 80kg, the net weight of the tank reduces obviously. For some higher density goods, the tank may carry more goods.
  • the height of the shading plate is beyond the tank, which is not easy to transport.
  • the heat insulation and reflective layer dicrectly covers on the tank in present disclosure, which overcomes the shortcoming of the shading plate caused by the excessive height.
  • the tank is coated by a heat insulation and reflective layer, and the coverage area of the heat insulation and reflective layer represents one third of the total area of the cylinder body.
  • the coverage area at least represents one third of the total area of the cylinder body, eg. the coverage area may represent two third.
  • the coverage area includes not only the surface of the cylinder body, but also a partion of or all of surface of the sealing heads.
  • Fig. 4a is perspective view of a tank container according to the third embodiment of the present disclosure.
  • Fig. 4b is a view showing partial enlargement of C district of Fig. 4a.
  • the tank container 30 includes a frame 31 and a tank 32 disposed in the frame 31.
  • the tank 32 includes a cylinder body 321 and two sealing heads 322 for sealing the two end openings of the cylinder body 321 respectively.
  • the outer surface of the tank 32 (including the outer surface of the cylinder body 321 and the sealing heads 322) is coated by a heat insulation and reflective layer 33 completely.
  • the heat insulation and reflective layer 33 covers the whole tank 32, that is, all the outer surface of the tank 32 is coated by the heat insulation and reflective layer 33, as to form an entire heat insulation layer to clad the whole tank 32.
  • the heat insulation effect of the entire heat insulation layer may achieve the level of “having heat insulation layer” regulated in the regulation of IMDG- “International Maritime Dangerous Goods Code” .
  • the heat insulation and reflective layer 33 has heat insulation and reflective function.
  • the heat insulation and reflective layer 33 may be a single layer structure.
  • the heat insulation and reflective layer 33 with single layer structure includes a plurality of non-metal hollow microspheres 331 with heat insulation and reflective function.
  • the matrix of the heat insulation and reflective layer 33 may be a high polymer material layer.
  • the heat insulation and reflective layer 33 may be composed of resin matrix and non-metal hollow microspheres 331 filled in the resin matrix.
  • the non-metal hollow microspheres 331 may produce sphere prism reflection effect, which may reduce sunshine energy invading into the tank, as to achieve the reflecting effect to sunshine.
  • a large number of hollow structures of non-metal hollow microspheres 331 form a heat insulating layer to stop heat conduction, thereby achieving the heat insulation effect.
  • non-metal hollow microspheres 331 may reflect sunshine
  • the non-metal hollow microspheres 331 disposed on the the tank32 may reflect visible light and infrared ray. Therefore the heat insulation and reflective layer 33 may have function of the shading plate.
  • the diameter of the non-metal hollow microsphere 331 may be between 5um to 100um.
  • the non-metal hollow microsphere 331 may be a glass hollow microsphere, a ceramic hollow microsphere or other non-metal hollow sphere.
  • the heat insulation and reflective layer 33 is a coating layer formed on the tank 32 by brush coating or spray coating.
  • the thickness of the coating layer is between 0.1mm to 2mm.
  • the heat insulation and reflective layer 33 may be a thin pasting-film or a thin blanket.
  • the thin pasting-film or the thin blanket is bonded to the tank 32 by pasting.
  • the thickness of the pasting-film or the thin blanket is between 0.1mm to 10mm.
  • titanium dioxide may be added into the resin matrix.
  • Fig. 5a is perspective view of a tank container according to the fourth embodiment of the present disclosure.
  • Fig. 5b is a view showing partial enlargement of D district of Fig. 5a.
  • the tank container 40 includes a frame 41 and a tank 42 disposed in the frame 41.
  • the tank 42 includes a cylinder body 421 and two sealing heads 422 for sealing the two end openings of the cylinder body 421 respectively.
  • the outer surface of the tank 42 (including the outer surface of the cylinder body 421 and the sealing heads 422) is coated by a heat insulation and reflective layer 43 completely.
  • the heat insulation and reflective layer 43 covers the whole tank 42, that is, all the outer surface of the tank 42 is coated by the heat insulation and reflective layer 43, as to form an entire heat insulation layer to clad the whole tank 42.
  • the heat insulation effect of the entire heat insulation layer may achieve the level of t” having heat insulation layer” regulated in the regulation of IMDG- “International Maritime Dangerous Goods Code” .
  • the heat insulation and reflective layer 43 has heat insulation and reflective function.
  • the heat insulation and reflective layer 43 is a double-layer structure.
  • the heat insulation and reflective layer 43 includes a heat insulation inner layer 431 and a reflective outer layer 432.
  • the heat insulation inner layer 431 is made of heat-preservation material, and the heat-preservation material may be selected from any one of silicate, rare earth, aerogel. But not limited to this, the heat-preservation material also may be other material with a function of heat preservation or heat insulation.
  • the reflective outer layer 432 may form a reflecting surface on the surface of the heat insulation inner layer 431 to achieve reflecting effect.
  • the reflective outer layer 432 may be made of reflective material.
  • the reflective material may be fluorocarbon coating.
  • the fluorocarbon coating may be composed of 4F type fluororesin and special heat insulation material. After the fluorocarbon coating forms a film, a coating film is formed which has high reflectivity and high themal resistance. When the sunshine shines on the coating film, major of energy of the sunshine will be reflected back, and is prevented from transmiting to the inner of the tank.
  • the reflective material is not limited to the fluorocarbon coating, but also may be other reflective material.
  • the heat insulation inner layer 431 and the reflecting layer 432 may be coated on the tank 42 by many kinds of manners.
  • the heat insulation inner layer 431 is a coating layer formed on the tank 42 by brush coating or spray coating of heat-preservation material.
  • the reflective outer layer 432 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 431 by pasting.
  • the total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10mm.
  • the heat insulation inner layer 431 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the tank 22 by pasting.
  • the reflective outer layer 432 is a coating layer formed on the heat insulation inner layer 431 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10mm.
  • the heat insulation inner layer 431 is a coating layer formed on the tank 42 by brush coating or spray coating of heat-preservation material.
  • the reflective outer layer 432 is a coating layer formed on the heat insulation inner layer 431 by brush coating or spray coating of fluorocarbon material.
  • the total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 2 mm.
  • the heat insulation inner layer 431 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the tank42 by pasting.
  • the reflective outer layer 432 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 431 by pasting.
  • the total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10 mm.
  • the outer suiface of the tank is coated by a heat insulation and reflective layer, which covers the whole tank, as to make an entire heat insulation layer formed on the outside of the tank, which has a good heat insulation effect.
  • a heat-preservation material layer is coated on the outer of the tank, and fixed to the tank by an outer packing sheet (the total weight of the heat-preservation material layer and the outer packing sheet is 200kg) ” in the traditional technique, the thickness and the weight of the heat insulation and reflective layer in the present disclosure are reduced obviously.
  • the heat insulation and reflective layer has a good heat insulation and reflecting effect, which may achieve the heat insulation level of “having heat insulation layer” regulated in the IMDG- “International Maritime Dangerous Goods Code” or other laws and regulations.
  • the design reference temperature may decrease to 50 °C. Accordingly, the maximum allowable working pressure (MAWP) of the cylinder body also decreases, and the design pressure decreases as well, thereby avoiding potential safe risk caused by high pressure within the tank.
  • MAWP maximum allowable working pressure
  • the examples in the above embodiments are all tank container. But not limited to tank container, the storage and transportation container in this disclosure may be other transportable pressure vessel, eg. a pressure vessel without frame.

Abstract

A tank container (10, 20, 30, 40), comprising: a tank (12, 22, 32, 43), which comprises a cylinder body (121, 221, 321, 421) and two sealing heads (122, 222, 322, 422) configured to seal two end openings of the cylinder body (121, 221, 321, 421) respectively; a heat insulation and reflective layer (13, 23, 33, 43) disposed on the outside of the tank, the heat insulation and reflective layer (13, 23, 33, 43) at least covers an upper surface of the cylinder body (121, 221, 321, 421) comprising a top surface of the cylinder body and a part of side surface extending from the top surface, the heat insulation and reflective layer (13, 23, 33, 43) covers an area of the cylinder body (121) at least one third of the total area.

Description

TANK CONTAINER TECHNICAL FIELD
The disclosure relates to the field of logistics transportation, more specifically to a storage and transportation container and even more specifically to a tank container.
BACKGROUND
A storage and transportation container is mainly used for storging and transporting material, eg. liquefied petroleum gas, ammonia, refrigerant and other non-refrigeration gas. The storage and transportation container can be a tank container.
The tank container is usually designed to meet the standard of ISO tank container according to the international transport regulation (eg. IMDG-International Maritime Dangerous Goods Code, ADR-European Agreement on the international carriage of dangerous goods, China standard JB/T 4781- "liquefied gas tank container" , etc. ) .
ISO tank container generally includes a frame and a tank located in the frame. The tank includes a cylinder body and two sealing heads configured to seal two ends opening of the cylinder body respectively. To meat the standard of the ISO, the tank itself and all the connecting piece and device must be arranged within the range of ISO standard specified size. For example, the size of outside frame of 20 feet tank container is 8 feet (2438 mm) in width, 20 feet in longth and 8.5 feet in height.
When the medium in the tank container is the liquefied gas, which is marked in domestic and international standards and specifications (international standards- “IMDG” , “ADR” , and China standard JB/T 4781) , eg. liquefied petroleum gas, refrigerant, ect, the cylinder body should have enough thickness to bear the maximum allowable working pressure (MAWP) . As this kind of liquefied gas in the sealed tank is generally under saturated gas-liquid mixed state, with the temperature going up, the pressure of the saturated state goes up, and the pressure within the tank will rise accordingly.
The minimum thickness of the cylinder body is usually calculated according to the standard of the pressure vessel (eg. according to ASME Section VIII, Division 2, AD 2000 Merkblatt, EN 13445, CODAP 2005 or others) .
The formula recorded in ASME Section VIII, Division 2 is as following:
Figure PCTCN2017117347-appb-000001
The “t” represents minimum thickness of the cylinder body. The “D” represents inner diameter of the cylinder body. The “P” represents design pressure. The “E” represents welding coefficient, with its value between 0.85 to 1. The “S” represents the value of allovable stress under design temperature.
The design pressure “P” of the cylinder body should not be less than the maximum allowable working pressure (MAWP) . The value of maximum allowable working pressure (MAWP) is related to absolute steam pressure of non refrigant liquiefied gas under the design reference temperature. The lower of the design reference temperature, the lower the absolute steam pressure of non refrigant liquiefied gas will be, the lower maximum allowable working pressure will be, and the lower the design pressure will be.
As stipulated in regulations of IMDG-International Maritime Dangerous Goods Code, without heating insulating layer or shading device, the design reference temperature of the cylinder body should be designed to 60℃. Having shading device, the design reference temperature of the cylinder body should be designed to 55℃. Having heating insulating layer, the design reference temperature of the cylinder body should be designed to 50℃.
Conventionally, as shown in Fig. 1, a shading plate 102 is disposed on the top of the tank 101 to shade the tank 101 from direct sunshine and avoid the temperature rising in the tank. According to international regulations, having shading device, the design reference temperature of the cylinder body should be designed to 55℃, that is, the design pressure of the cylinder body deceases compared with the cylinder body without shading device.
This design reference temperature can be reduced to 50 ℃ by employing a complete tank insulation.
However, the weight of the shading plate is more than 80kg, which increases the net weight of the tank container and a suitable insulation (including insulation and a insulation cladding) adds an additional weight of about 200 kg.
Therefore the problem exists to provide a tank container for non-refrigerated liquefied gases with a low weight and a high volume which is on the one hand designed for a design reference temperature which allows for higher strength values of the tank material but on the other hand without adding additional components to achieve such a lower design reference temperature.
SUMMARY
According to an aspect of the present disclosure, a storage and transportation container, includes a tank and a heat insulation and reflective layer. The tank includes a cylinder body and two sealing heads configured to seal two end openings of the cylinder body respectively; The heat insulation and reflective layer is disposed on the outer surface of the tank. The heat insulation and reflective layer at least covers an upper surface of the cylinder body including a top surface of the cylinder body and a part of side surface extending from the top surface. The heat insulation and reflective layer covers an area of the cylinder body at least one third of the total area.
The technical solution of the present disclosure has advantageous effects as  following:
A heat insulation and reflective layer is coated on the tank, the heat insulation and reflective layer at least coveres the upper surface, the coverage area of the heat insulation and reflective layer at least covers one third of the total area of the cylinder body. The heat insulation and reflective layer has high reflectivity to sunshine, the sunshine shining on the surface of the tank may be well reflected back. Whereby, the technical solution provided in this disclosure may totally replace the shading device used in the prior art. Meanwhile, the heat insulation and reflective layer has good heat insulating effect, which may obviously reduce heat transmission between the tank and outerspace, thereby reduce liquid vaporization as the rise of the temperature within the tank, keeping the pressure from rising, and avoiding potential risk caused by high pressure within the tank. Therefore, compared to the traditional shading plate, the heat insulation and reflective layer is thinner and lighter, accordingly the net weight of the storage and transportation container reduces obviously.
Further aspects and features result from the dependant claims, the attached drawings and the following description of embodiments of the present invention. Embodiments are described by way of example in relation to the attached drawings.
It should be undersood that the above general description and the following detail description is just exemplary, not to limit the present disclosure.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a perspective view showing a shading plate disposed on the top of a tank container in the prior art.
Fig. 2a is a perspective view of a tank container according to the first embodiment of the present disclosure.
Fig. 2b is a view showing partial enlargement of A district of Fig. 2a.
Fig. 3a is perspective view of a tank container according to the second embodiment of the present disclosure.
Fig. 3b is a view showing partial enlargement of B district of Fig. 3a.
Fig. 4a is perspective view of a tank container according to the third embodiment of the present disclosure.
Fig. 4b is a view showing partial enlargement of C district of Fig. 4a.
Fig. 5a is perspective view of a tank container according to the fourth embodiment of the present disclosure.
Fig. 5b is a view showing partial enlargement of D district of Fig. 5a.
DETAILED DESCRIPTION
Prior to a detailed description of the embodiments according to Figs. 2 to 5b general explanations are provided with regard to general embodiments.
The embodiment of the freight container according to one aspect of the present invention comprises a vessel for retaining the pressurized liquid within a shell comprising a cylindrical section and heads enclosing opposite ends of the cylindrical section, a frame connected to the vessel to transmit operational loads between the vessel and handling devices at least one opening for filling and/or discharging the vessel, a thermal system covering not less than the upper third of an outer surface of the shell, wherein the thermal system provides an insulation effect which is at least equivalent to the insulation effect of a shield separated from the outer surface of the shell by an airspace of not less than 40 mm, and the thermal system comprises a thermal coating comprising a heat-reflective, heat-absorbing and/or insulating liquid based material containing insulating, heat-absorbing and/or reflecting particles.
In such a freight container the thermal system is provided which achieves an insulation effect which is at least equivalent to the insulation effect of a shield separated from the outer surface of the shell by an airspace of not less than 40 mm. And specifically, this thermal system is achieved by a thermal coating comprising a liquid based material containing insulating, heat-absorbing and/or reflective particles. Therefore the thermal properties are achieved by a material which is added and/or included into a painting material (matrix) . The particles provide insulating, heat-absorbing and/or reflecting properties.
There are embodiments wherein the particles comprise ceramic and/or nano-particles. Such particles or nano-particles may comprise silicate or tombarthite particles which increase the insulating quality of such a coating.
There are embodiments wherein the coating comprises irregular silicate particles 5 to 100 μm in seize.
In other embodiments the coating may comprise fine non-metallic hollow microspheres which have a high reflectivity for light and/or infrared radiation and form numerous small cavities inside the coating layers (similar to a foam structure) which decrease the thermal conduction of the coating. Such hollow beads or spherical beads therefore combine reflecting and insulating features.
In other embodiments the insulating/reflecting particles may contain thermochromic dyes, particularly in the form of microcapsules, containing special dyes which changes its colour due to a change of temperature and/or radiation. Such thermochromic dyes may for example change their colour from dark (low reflective) to bright (high reflective) under the influence of sun radiation and/or an increase of the surface temperature due to such radiation.
In another embodiment the insulating/reflecting/thermo-active particles may contain particles with a latent heat storage function by exploiting the enthalpy of a reversible  thermodynamic state, in particular solid to liquid or vice versa. They take up a lot of heat energy (irradiated by the sun) and convert it into the so called “heat of fusion” without changing the temperature. This process is reversible and the storage medium releases the same amount of heat energy during solidification (e.g. during the night) . Latent heat storage material is available in the form of microencapsulated particles containing a latent heat storing substance (e.g. based on a paraffin wax) .
There are embodiments in which the thermal coating is based on a white or translucent matrix based on a component selected from epoxy resins, polyurethanes, acrylates, styrene acrylates, silicone polymers, polyester resins, and/or natural resins and other components suitable of forming a coating matrix.
There are embodiments wherein the thermal insulating coating comprises an outer surface having a high emissivity which allows for a high irradiation of heat from the container vessel itself, i.e. from the container vessel surface. Such a surface having a high emissivity can be formed by a special coating layer and/or may be formed by a sheet layer and/or a membrane layer which is applied to the coating in a wrapping and/or plating process.
Such a sheet layer may be formed by a thin, highly reflective metal foil (e.g. aluminium foil) and/or by a metalized plastic tape or foil. It may also be formed by a fiber reinforced foil or membrane having increased mechanically properties.
Such a membrane sheet and/or membrane layer may also contain an adhesive layer which is suitable to fix the layer or sheet onto the coating layer.
In another embodiment the outer surface may also be formed from a non-metallic bead coating with high reflective bead components.
In another embodiment the thermal system provides an insulation effect which is at least equivalent to the insulation effect of a complete cladding of the vessel having a thermal conductance of not more than 0,67 Wm-2K-1. Such a thermal system is able to replace a complete thermal insulation which usually comprises an insulation layer of more than 20 mm. If the thermal system according to the present invention is designed accordingly it is possible to gain an diameter increasement which results in an additional volume for a 20’ISO container.
Hereinafter, the disclosure will be further explained with reference to the accompanying drawings.
The storage and transportation container of the present disclosure may be applied to transportable pressure vessel, more specifically to the vessel for transporting non-refrigeration liquid gas. In the following embodiments, the disclosure will be explained by exampling of a tank container for transporting liquefied petroleum gas.
Embodiment One
Fig. 2a is a perspective view of a tank container according to the first embodiment  of the present disclosure. The tank container 10 includes a frame 11 and a tank 12 disposed in the frame 11. The tank 12 includes a cylinder body 121 and two sealing heads 122 for sealing the two end openings of the cylinder body 121 respectively.
The upper surface of the cylinder body 121 is covered by a heat insulation and reflective layer 13. The area of the upper surface represents one third of the total area of the cylinder body 121, that is, the coverage erea of the heat insulation and reflective layer 13 represents one third of the total area of the cylinder body 121. The upper surface of the cylinder body includes a top surface of the cylinder body and a portion of side surface extending from the top surface. The total area of the top surface and the part of side surface represents one third of the total area of the cylinder body 121.
The heat insulation and reflective layer 13 has heat insulation and reflective function. The heat insulation and reflective layer 13 is a single layer structure. The single layer structure includes a plurality of non-metal hollow microspheres 131 having heat insulation and reflective function. The matrix of the heat insulation and reflective layer 13 may be a high polymer material layer. The heat insulation and reflective layer 13 may be composed of resin matrix and non-metal hollow microspheres filled in the resin matrix. The non-metal hollow microspheres 131 may produce sphere prism reflection effect, which may reduce sunshine energy invading into the tank, thus achieving the reflecting effect to sunshine. Meamwhile, a large number of hollow structures of non-metal hollow microspheres 131 form a heat insulation layer to stop heat conduction, thereby achieving the heat insulation effect.
As non-metal hollow microspheres 131 may reflect sunshine, the non-metal hollow microspheres 131 disposed on the upper surface of the cylinder body 121 may reflect visible light and infrared ray. Therefore the heat insulation and reflective layer 13 may have function of the shading plate.
The diameter of the non-metal hollow microsphere 131 may be between 5um to 100um. The non-metal hollow microsphere 131 may be a glass hollow microsphere, a ceramic hollow microsphere or other non-metal hollow sphere. These hollow spheres 131 perform as insulating and reflecting particles. The hollow space, which is filled by a gas, increases the insulating capacity of the reflective layer 13 because the thermal conductance of gases is much lower than the thermal conductance of a solid or liquid. The hollow spheres 131 also reflect visible light and/or infrared irradiation at their outer and/or inner surfaces and therefore keep the radiation away from the cylinder body 121 and therefore operate like an internal sunshield.
The heat insulation and reflective layer is a coating layer formed on the cylinder body 121 by brush coating or spray coating. The thickness of the coating layer is between 0.1mm to 2mm.
The heat insulation and reflective layer may be a thin pasting-film or a thin blanket (e.g. a sheet layer or membrane layer formed from a metallic or metallized foil with high reflectivity/emissivity) . The thin pasting-film or the thin blanket is bonded to the cylinder  body 121 by pasting. The thickness of the pasting-film or the thin blanket is between 0.1mm to 10mm.
In addition, to further reinforce the reflecting property of the the heat insulation and reflective layer 13, titanium dioxide may be added into the resin matrix.
Embodiment Two
Refering to Fig. 3a is perspective view of a tank container according to the second embodiment of the present disclosure. Fig. 3b is a view showing partial enlargement of B district of Fig. 3a. The tank container 20 includes a frame 21 and a tank 22 disposed in the frame 21. The tank 22 includes a cylinder body 221 and two sealing heads 222 configured to seal the two end openings of the cylinder body 221 respectively.
The upper surface of the cylinder body 221 is covered by a heat insulation and reflective layer 23. The area of the upper surface represents one third of the total area of the cylinder body 221, that is, the coverage area of the heat insulation and reflective layer 23 represents one third of the total area of the cylinder body 221. The upper surface of the cylinder body 221 includes a top surface of the cylinder body and a portion of side surface extending from the top surface. The total area of the top surface and the part of side surface represents one third of the total area of the cylinder body 221.
The heat insulation and reflective layer 23 has heat insulation and reflective function. The heat insulation and reflective layer 23 is a double-layer structure. The heat insulation and reflective layer 23 includes a heat insulation inner layer 231 and a reflective outer layer 232. The heat insulation inner layer 231 is made of heat-preservation material, and the heat-preservation material may be selected from any one from silicate, rare earth and aerogel. But not limited to these kinds of material, the heat-preservation material may also be other material with function of heat preservation or heat insulation.
The reflective outer layer 232 may form a reflecting surface on the surface of the heat insulation inner layer 231 to achieve reflecting effect.
In addition, the reflective outer layer 232 may be made of reflective material. The reflective material may be fluorocarbon coating. The fluorocarbon coating may be composed of 4F type fluororesin and special heat insulation material. In case that the fluorocarbon coating forms a film, a coating film which has high reflectivity and high themal resistance is formed. When the sunshine shines on the coating film, major of energy of the sunshine will be reflected back, and is prevented from transmiting into the tank.
In addition, the reflective material is not limited to the fluorocarbon coating, but other reflective material.
The heat insulation inner layer 231 and the reflecting layer 232 may be coated on the tank 22 by many kinds of manners.
In one manner, the heat insulation inner layer 231 is a coating layer formed on the cylinder body 121 by brush coating or spray coating of heat-preservation material. The  reflective outer layer 232 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 231 by pasting. The total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10mm.
In another manner, the heat insulation inner layer 231 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the cylinder body 121 by pasting. The reflective outer layer 232 is a coating layer formed on the heat insulation inner layer 231 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10mm.
In further another manner, the heat insulation inner layer 231 is a coating layer formed on the cylinder body 121 by brush coating or spray coating of heat-preservation material. The reflective outer layer 232 is a coating layer formed on the heat insulation inner layer 231 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 2 mm.
In further another manner, the heat insulation inner layer 231 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the cylinder body 121 by pasting. The reflective outer layer 232 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 231 by pasting. The total thickness of the heat insulation inner layer 231 and the reflective outer layer 232 is between 0.1mm to 10 mm.
In the above two embodiments, A heat insulation and reflective layer is coated on the tank, the heat insulation and reflective layer at least coveres the upper surface, the coverage area of the heat insulation and reflective layer at least covers one third of the total area of the cylinder body. The heat insulation and reflective layer has high reflectivity to sunshine, the sunshine shining on the surface of the tank may be well reflected back. Whereby, the technical solution provided in this disclosure may totally replace the shading device used in the prior art. Meanwhile, the heat insulation and reflective layer has good heat insulating effect, which may obviously reduce heat transmission between the tank and outerspace, thereby reduce liquid vaporization as the rise of the temperature within the tank, keeping the pressure from rising, and avoiding potential risk caused by high pressure within the tank.
As coated on the surface of the tank in the present disclosure, the heat insulation and reflective layer is not easy to be damaged, and the durability of the heat insulation and reflective layer increases at least 30%.
According to relevant standard, in case of having shading device, the design reference temperature of the tank may reduce from 60℃ to 55℃. The design reference temperature has reduced, the design pressure also has reduced, and accordingly the safety of the tank increases.
Moreover, as the heat insulation and reflective layer itself is thin, of which the thickness is between 0.1mm to 10 mm, compared to the conventional shading plate of the weight of 80kg, the net weight of the tank reduces obviously. For some higher density goods, the tank may carry more goods.
In the conventional art, the height of the shading plate is beyond the tank, which is not easy to transport. However the heat insulation and reflective layer dicrectly covers on the tank in present disclosure, which overcomes the shortcoming of the shading plate caused by the excessive height.
In the above two embodiments, the tank is coated by a heat insulation and reflective layer, and the coverage area of the heat insulation and reflective layer represents one third of the total area of the cylinder body. But not limit to this ratio, the coverage area at least represents one third of the total area of the cylinder body, eg. the coverage area may represent two third. Moreover the coverage area includes not only the surface of the cylinder body, but also a partion of or all of surface of the sealing heads.
Embodiment Three
Refering to Fig. 4a and Fig. 4b, Fig. 4a is perspective view of a tank container according to the third embodiment of the present disclosure. Fig. 4b is a view showing partial enlargement of C district of Fig. 4a. The tank container 30 includes a frame 31 and a tank 32 disposed in the frame 31. The tank 32 includes a cylinder body 321 and two sealing heads 322 for sealing the two end openings of the cylinder body 321 respectively.
The outer surface of the tank 32 (including the outer surface of the cylinder body 321 and the sealing heads 322) is coated by a heat insulation and reflective layer 33 completely. The heat insulation and reflective layer 33 covers the whole tank 32, that is, all the outer surface of the tank 32 is coated by the heat insulation and reflective layer 33, as to form an entire heat insulation layer to clad the whole tank 32. The heat insulation effect of the entire heat insulation layer may achieve the level of “having heat insulation layer” regulated in the regulation of IMDG- “International Maritime Dangerous Goods Code” .
The heat insulation and reflective layer 33 has heat insulation and reflective function. The heat insulation and reflective layer 33 may be a single layer structure. The heat insulation and reflective layer 33 with single layer structure includes a plurality of non-metal hollow microspheres 331 with heat insulation and reflective function.
The matrix of the heat insulation and reflective layer 33 may be a high polymer material layer. The heat insulation and reflective layer 33 may be composed of resin matrix and non-metal hollow microspheres 331 filled in the resin matrix. The non-metal hollow microspheres 331 may produce sphere prism reflection effect, which may reduce sunshine energy invading into the tank, as to achieve the reflecting effect to sunshine. Meamwhile, a large number of hollow structures of non-metal hollow microspheres 331 form a heat insulating layer to stop heat conduction, thereby achieving the heat insulation effect.
As non-metal hollow microspheres 331 may reflect sunshine, the non-metal hollow microspheres 331 disposed on the the tank32 may reflect visible light and infrared ray. Therefore the heat insulation and reflective layer 33 may have function of the shading plate.
The diameter of the non-metal hollow microsphere 331 may be between 5um to 100um. The non-metal hollow microsphere 331 may be a glass hollow microsphere, a ceramic hollow microsphere or other non-metal hollow sphere.
The heat insulation and reflective layer 33 is a coating layer formed on the tank 32 by brush coating or spray coating. The thickness of the coating layer is between 0.1mm to 2mm.
The heat insulation and reflective layer 33 may be a thin pasting-film or a thin blanket. The thin pasting-film or the thin blanket is bonded to the tank 32 by pasting. The thickness of the pasting-film or the thin blanket is between 0.1mm to 10mm.
In addition, in order to further reinforce the reflecting property of the the heat insulation and reflective layer 33, titanium dioxide may be added into the resin matrix.
Embodiment Four
Refering to Fig. 5a and Fig. 5b, Fig. 5a is perspective view of a tank container according to the fourth embodiment of the present disclosure. Fig. 5b is a view showing partial enlargement of D district of Fig. 5a. The tank container 40 includes a frame 41 and a tank 42 disposed in the frame 41. The tank 42 includes a cylinder body 421 and two sealing heads 422 for sealing the two end openings of the cylinder body 421 respectively.
The outer surface of the tank 42 (including the outer surface of the cylinder body 421 and the sealing heads 422) is coated by a heat insulation and reflective layer 43 completely. The heat insulation and reflective layer 43 covers the whole tank 42, that is, all the outer surface of the tank 42 is coated by the heat insulation and reflective layer 43, as to form an entire heat insulation layer to clad the whole tank 42. The heat insulation effect of the entire heat insulation layer may achieve the level of t” having heat insulation layer” regulated in the regulation of IMDG- “International Maritime Dangerous Goods Code” .
The heat insulation and reflective layer 43 has heat insulation and reflective function. The heat insulation and reflective layer 43 is a double-layer structure. The heat insulation and reflective layer 43 includes a heat insulation inner layer 431 and a reflective outer layer 432.
The heat insulation inner layer 431 is made of heat-preservation material, and the heat-preservation material may be selected from any one of silicate, rare earth, aerogel. But not limited to this, the heat-preservation material also may be other material with a function of heat preservation or heat insulation.
The reflective outer layer 432 may form a reflecting surface on the surface of the heat insulation inner layer 431 to achieve reflecting effect.
In addition, the reflective outer layer 432 may be made of reflective material. The reflective material may be fluorocarbon coating. The fluorocarbon coating may be composed of 4F type fluororesin and special heat insulation material. After the fluorocarbon coating forms a film, a coating film is formed which has high reflectivity and high themal resistance. When the sunshine shines on the coating film, major of energy of the sunshine will be reflected back, and is prevented from transmiting to the inner of the tank.
In addition, the reflective material is not limited to the fluorocarbon coating, but also may be other reflective material.
The heat insulation inner layer 431 and the reflecting layer 432 may be coated on the tank 42 by many kinds of manners.
In one manner, the heat insulation inner layer 431 is a coating layer formed on the tank 42 by brush coating or spray coating of heat-preservation material. The reflective outer layer 432 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 431 by pasting. The total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10mm.
In another manner, the heat insulation inner layer 431 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the tank 22 by pasting. The reflective outer layer 432 is a coating layer formed on the heat insulation inner layer 431 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10mm.
In further another manner, the heat insulation inner layer 431 is a coating layer formed on the tank 42 by brush coating or spray coating of heat-preservation material. The reflective outer layer 432 is a coating layer formed on the heat insulation inner layer 431 by brush coating or spray coating of fluorocarbon material. The total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 2 mm.
In further another manner, the heat insulation inner layer 431 is a thin pasting-film or a thin blanket made of heat-preservation material, which may be bonded to the tank42 by pasting. The reflective outer layer 432 is a thin pasting-film or a thin blanket made of fluorocarbon material, which may be bonded to the heat insulation inner layer 431 by pasting. The total thickness of the heat insulation inner layer 431 and the reflective outer layer 432 is between 0.1mm to 10 mm.
In above embodiment three and embodiment four, the outer suiface of the tank is coated by a heat insulation and reflective layer, which covers the whole tank, as to make an entire heat insulation layer formed on the outside of the tank, which has a good heat insulation effect. Compared to the manner of “a heat-preservation material layer is coated on the outer of the tank, and fixed to the tank by an outer packing sheet (the total weight of the heat-preservation material layer and the outer packing sheet is 200kg) ” in the traditional  technique, the thickness and the weight of the heat insulation and reflective layer in the present disclosure are reduced obviously.
The heat insulation and reflective layer has a good heat insulation and reflecting effect, which may achieve the heat insulation level of “having heat insulation layer” regulated in the IMDG- “International Maritime Dangerous Goods Code” or other laws and regulations.
Therefore, according to regulations of the IMDG- “International Maritime Dangerous Goods Code” , the design reference temperature may decrease to 50 ℃. Accordingly, the maximum allowable working pressure (MAWP) of the cylinder body also decreases, and the design pressure decreases as well, thereby avoiding potential safe risk caused by high pressure within the tank.
It should be noted that, the examples in the above embodiments are all tank container. But not limited to tank container, the storage and transportation container in this disclosure may be other transportable pressure vessel, eg. a pressure vessel without frame.
Therefore, the embodiments described above are merely some perefable ones, and the disclosure is not limited to any specific details of these embodiments. An oridinary person skilled in the art would readily appreciate that modifications or changes based on the principles of the disclosure. Accordingly, the scope of the present invention should be limited solely by the appended claims.

Claims (12)

  1. Tank container (10, 20, 30, 40) , comprising:
    a tank (12, 22, 32, 43) comprising a cylinder body (121, 221, 321, 421) and two sealing heads (122, 222, 322, 422) configured to seal two end openings of the cylinder body (121, 221, 321, 421) respectively;
    a heat insulation and reflective layer (13, 23, 33, 43) disposed on the outside of the tank, the heat insulation and reflective layer (13, 23, 33, 43) ) at least covers an upper surface of the cylinder body (121, 221, 321, 421) comprising a top surface of the cylinder body and a part of side surface extending from the top surface, the heat insulation and reflective layer (13, 23, 33, 43) covers an area of the cylinder body (121) at least one third of the total area.
  2. Tank container (30, 40) according to claim 1, wherein the heat insulation and reflective layer (33, 43) covers the outer surfaces of the cylinder body (321, 421) and the sealing heads (322, 422) to make the whole tank body (32, 42) in the coverage.
  3. Tank container (10, 20, 30, 40) according to claim 1 or 2, wherein the heat insulation and reflective layer (13, 33) is a coating layer formed on the tank by brush coating or spray coating.
  4. Tank container (10, 20, 30, 40) according to claim 3, wherein the thickness of the coating layer is between 0.1mm to 2mm.
  5. Tank container (10, 20, 30, 40) according to claim 1 or 2, wherein the heat insulation and reflective layer (13, 33) is a thin pasting-film or a thin blanket, the thickness of the pasting-film or the thin blanket is between 0.1mm to 10mm.
  6. Tank container (10, 30) according to one of claims 1 to 5, wherein the heat insulation and reflective layer comprises (13, 33) non-metal hollow microspheres (131, 331) with heat insulation and reflective function, the diameter of the non-metal hollow microspheres (131, 331) is between 5μm to 100μm.
  7. Tank container (10, 30) according to claim 6, wherein the non-metal hollow microspheres (131, 331) comprise glass hollow microspheres and/or ceramic hollow microspheres.
  8. Tank container (20, 40) according to claim 1 or claim 2, wherein the heat insulation and reflective layer (23, 43) comprises a heat insulation inner layer (231, 431) being made of a heat preservation material and a reflective outer layer (232, 432) being made of a reflective material.
  9. Tank container (20, 40) according to claim 8, wherein the heat insulation inner layer (231, 431) is a coating layer, a pasting-film or a thin blanket, and the reflective outer layer (232, 432) is a coating layer, a pasting-film or a thin blanket.
  10. Tank container (20, 40) according to claim 8 or 9, wherein the total thickness of the heat insulation inner layer (231, 431) and the reflective outer layer (232, 432) is between 0.1mm to 10mm.
  11. Tank container (20, 40) according to one of claims 8 to 10, wherein the heat-preservation material is selected from any one of silicate, rare earth and aerogel.
  12. Tank container (20, 40) according to one of claims 8 to 10, wherein the reflective material is a fluorocarbon coating.
PCT/CN2017/117347 2017-01-13 2017-12-20 Tank container WO2018130051A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201710026484.0A CN107228277A (en) 2017-01-13 2017-01-13 Storage-transport vessel
CN201710026484.0 2017-01-13

Publications (1)

Publication Number Publication Date
WO2018130051A1 true WO2018130051A1 (en) 2018-07-19

Family

ID=58489574

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/117347 WO2018130051A1 (en) 2017-01-13 2017-12-20 Tank container

Country Status (3)

Country Link
EP (1) EP3348893B1 (en)
CN (1) CN107228277A (en)
WO (1) WO2018130051A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019127261A1 (en) * 2019-10-10 2021-04-15 Michael Heine LPG storage tank

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107228277A (en) * 2017-01-13 2017-10-03 南通中集罐式储运设备制造有限公司 Storage-transport vessel
CN110220107A (en) * 2019-05-24 2019-09-10 湖北三江航天江北机械工程有限公司 The preparation method of low temperature insulation container
FR3123706A1 (en) * 2021-06-04 2022-12-09 Airbus Operations (S.A.S.) Reservoir having reinforced insulation combining thermal insulation blankets as well as microspheres and method of manufacturing such a reservoir

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6521077B1 (en) * 1999-03-25 2003-02-18 Lydall, Inc. Method for insulating a cryogenic container
CN202046617U (en) * 2011-01-26 2011-11-23 郭宪强 Heat-insulation storage tank
CN203190021U (en) * 2013-03-11 2013-09-11 南通中集罐式储运设备制造有限公司 Tank container
CN204062463U (en) * 2014-09-02 2014-12-31 张家港中集圣达因低温装备有限公司 LNG ship transfer cask
CN205345880U (en) * 2015-12-25 2016-06-29 奥龙汽车有限公司 On -vehicle dangerization jar body
CN105754427A (en) * 2014-12-18 2016-07-13 太原市誉远涂料有限公司 Self-cleaning colorized solar heat reflecting coating
CN206398360U (en) * 2017-01-13 2017-08-11 南通中集罐式储运设备制造有限公司 Storage-transport vessel
CN107228277A (en) * 2017-01-13 2017-10-03 南通中集罐式储运设备制造有限公司 Storage-transport vessel

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1300705A (en) * 2001-02-13 2001-06-27 姚宇 Auxiliary anticorrosion process for external surface of open tank and pipeline
CN1333198C (en) * 2004-04-15 2007-08-22 中国国际海运集装箱(集团)股份有限公司 High vacuum heat insulation low temperature liquefied gas storage tank
CN102705696A (en) * 2012-05-29 2012-10-03 张家港市科华化工装备制造有限公司 Interlayer-type low-temperature storage tank
JP6130643B2 (en) * 2012-10-15 2017-05-17 三菱重工業株式会社 Storage tank for liquefied fuel
CN104356734A (en) * 2014-11-15 2015-02-18 天津恒远达科技有限公司 Novel nano ceramic reflective insulation paint
CN104403569A (en) * 2014-12-23 2015-03-11 天津恒远达科技有限公司 Reflective insulation paint for preventing crude oil storage tank from combustion

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6521077B1 (en) * 1999-03-25 2003-02-18 Lydall, Inc. Method for insulating a cryogenic container
CN202046617U (en) * 2011-01-26 2011-11-23 郭宪强 Heat-insulation storage tank
CN203190021U (en) * 2013-03-11 2013-09-11 南通中集罐式储运设备制造有限公司 Tank container
CN204062463U (en) * 2014-09-02 2014-12-31 张家港中集圣达因低温装备有限公司 LNG ship transfer cask
CN105754427A (en) * 2014-12-18 2016-07-13 太原市誉远涂料有限公司 Self-cleaning colorized solar heat reflecting coating
CN205345880U (en) * 2015-12-25 2016-06-29 奥龙汽车有限公司 On -vehicle dangerization jar body
CN206398360U (en) * 2017-01-13 2017-08-11 南通中集罐式储运设备制造有限公司 Storage-transport vessel
CN107228277A (en) * 2017-01-13 2017-10-03 南通中集罐式储运设备制造有限公司 Storage-transport vessel

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019127261A1 (en) * 2019-10-10 2021-04-15 Michael Heine LPG storage tank
DE102019127261B4 (en) 2019-10-10 2022-03-31 Michael Heine LPG storage tank

Also Published As

Publication number Publication date
CN107228277A (en) 2017-10-03
EP3348893A1 (en) 2018-07-18
EP3348893B1 (en) 2023-07-05

Similar Documents

Publication Publication Date Title
WO2018130051A1 (en) Tank container
CN110216924A (en) A kind of recombination radiation refrigeration film
JP6584681B2 (en) Laminated structure
US3325037A (en) Cryogenic structural insulating panels
US7503971B2 (en) Radiative cooling surface coatings
JP6602487B2 (en) Radiant cooling device
US20010040166A1 (en) Packaging for shipping compressed gas cylinders
CN101784845A (en) An element for emission of thermal radiation
CN101680598A (en) Device and method for storing hydrogen for an aircraft
US4190160A (en) Accident resistant transport container
US20080087665A1 (en) Freight container
US3671286A (en) Surface with low absorptivity to emissivity ratio
EP0958473A1 (en) Pressure container for fluids
CA2761831A1 (en) Portable apparatus for storing water and melting frozen water
KR20110020494A (en) Insulation structure for a lng carrier tank
JP2005163989A (en) Vacuum insulating material and using method of same
CN206398360U (en) Storage-transport vessel
EP3721452A1 (en) Storage basket for storing or transporting nuclear materials
KR20220130443A (en) Transparent radiative cooling device
RU2148864C1 (en) Container for transportation and long-time storage of spent fuel assemblies of nuclear power plants
WO1995026482A1 (en) Thermic insulated tank and a wall module element for use in construction of a thermic insulated tank
JP2009113822A (en) Low-temperature insulating and heat-insulating container
RU2175457C2 (en) Container to carry dangerous and valuable cargo
Grammer et al. Absorbing coatings for the far infrared
RU15444U1 (en) LAYERED STRUCTURE AND PROTECTIVE HOUSING FROM IT

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 17891565

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 17891565

Country of ref document: EP

Kind code of ref document: A1