US2386958A - Spherical type insulated container for liquefied gases - Google Patents
Spherical type insulated container for liquefied gases Download PDFInfo
- Publication number
- US2386958A US2386958A US42601242A US2386958A US 2386958 A US2386958 A US 2386958A US 42601242 A US42601242 A US 42601242A US 2386958 A US2386958 A US 2386958A
- Authority
- US
- United States
- Prior art keywords
- container
- shell
- pipe
- inner shell
- shells
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
Links
- 239000007789 gas Substances 0.000 title description 99
- 238000009413 insulation Methods 0.000 description 24
- 229910052751 metal Inorganic materials 0.000 description 24
- 239000002184 metal Substances 0.000 description 24
- 239000011810 insulating material Substances 0.000 description 22
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 20
- 239000000463 material Substances 0.000 description 12
- 238000003466 welding Methods 0.000 description 12
- 239000007788 liquid Substances 0.000 description 11
- 229910052759 nickel Inorganic materials 0.000 description 10
- 229910000831 Steel Inorganic materials 0.000 description 9
- 239000010959 steel Substances 0.000 description 9
- 239000007799 cork Substances 0.000 description 8
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 239000003949 liquefied natural gas Substances 0.000 description 6
- 238000001704 evaporation Methods 0.000 description 5
- 230000008020 evaporation Effects 0.000 description 5
- 238000001914 filtration Methods 0.000 description 5
- 239000012530 fluid Substances 0.000 description 5
- 230000002829 reductive effect Effects 0.000 description 5
- 229910000975 Carbon steel Inorganic materials 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 238000003860 storage Methods 0.000 description 4
- 239000010962 carbon steel Substances 0.000 description 3
- 230000000670 limiting effect Effects 0.000 description 3
- 239000003351 stiffener Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 230000008014 freezing Effects 0.000 description 2
- 238000007710 freezing Methods 0.000 description 2
- 230000008595 infiltration Effects 0.000 description 2
- 238000001764 infiltration Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012856 packing Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- UQMRAFJOBWOFNS-UHFFFAOYSA-N butyl 2-(2,4-dichlorophenoxy)acetate Chemical compound CCCCOC(=O)COC1=CC=C(Cl)C=C1Cl UQMRAFJOBWOFNS-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000000994 depressogenic effect Effects 0.000 description 1
- 238000009408 flooring Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 239000011490 mineral wool Substances 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/022—Land-based bulk storage containers
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H7/00—Construction or assembling of bulk storage containers employing civil engineering techniques in situ or off the site
- E04H7/02—Containers for fluids or gases; Supports therefor
- E04H7/18—Containers for fluids or gases; Supports therefor mainly of concrete, e.g. reinforced concrete, or other stone-like material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0128—Shape spherical or elliptical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/052—Size large (>1000 m3)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/011—Reinforcing means
- F17C2203/012—Reinforcing means on or in the wall, e.g. ribs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0329—Foam
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0337—Granular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0345—Fibres
- F17C2203/035—Glass wool
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0354—Wood
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0379—Inert
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0639—Steels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0646—Aluminium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0648—Alloys or compositions of metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0678—Concrete
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0153—Details of mounting arrangements
- F17C2205/018—Supporting feet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0332—Safety valves or pressure relief valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
- F17C2205/0335—Check-valves or non-return valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0379—Manholes or access openings for human beings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
- F17C2250/06—Controlling or regulating of parameters as output values
- F17C2250/0605—Parameters
- F17C2250/0636—Flow or movement of content
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/02—Improving properties related to fluid or fluid transfer
- F17C2260/021—Avoiding over pressurising
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/05—Regasification
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/901—Liquified gas content, cryogenic
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86292—System with plural openings, one a gas vent or access opening
- Y10T137/86324—Tank with gas vent and inlet or outlet
- Y10T137/86332—Vent and inlet or outlet in unitary mounting
Definitions
- This invention relates to insulated containers of relatively great size capable of storing extremely cold liquids such, for instance, as liquefied natural gas.
- An object of this invention is to produce an insulated container capable of safely and economically storing for long periods a relatively great quantity of liquefied gas such as liquefied natural gas.
- Liquefied natural gas at atmospheric pressure has a temperature far below F. (actually about 258 F.) and is subject to some evaporation and another object of this invention is to provide means for safely and economically taking care of the gas resulting from evaporation of liquefied natural gas stored in an insulated container of relatively great size.
- a further object of this invention is to produce means for safely and economically introducing and withdrawing liquefied natural gas from insulated containers of relatively great size.
- a further object is to produce improved mechanism by means of which low temperature liquefled gas can be charged into and removed from a relatively large insulated storage tank without damage to such tank or such mechanism.
- a further object is to produce improved mechanism for controlling the flow of liquefied gas into and from an insulated storage tank of relatively great size, without permitting conduction to such tank of an appreciable amount of heat.
- a still further object is to produce improved mechanism for controlling and limiting to a safe value, pressures generated bythe evaporation of liquefied gas within an insulated storage tank of relatively great size.
- Fig. 1 is an elevational view, partly in section, of a preferred form of insulated spherical container responding to my present invention
- Fig. 2 is an enlarged vertical fragmentary section through the axial portion of the container of Fig. 1;
- Fig. 3 is a plan view, with certain parts omitted and broken away, of the container of Figs. 1 and 2;
- Fig. 4 is a vertical elevational view of the upper portion of the container of Figs. 1 to 3, inclusive, taken at right angles to Fig. 1;
- Fig. 5 is an enlarged sectional view, partly in elevation, through the boot shown in Fig. 1 and illustrates certain additional devices not shown in Figs. 1 and 2, the insulation surrounding the gas vent pipe not being shown in this figure;
- Fig. 6 is a horizontal sectional view illustrating the manner in which the lower end of the vapor pipe is supported within the boot and is taken along the line VIVI of Fig. 5;
- Fig. 7 is an enlarged plan view of parts of Fig. 5 illustrating the means for maintaining and supporting the expansion joint in the lower end of the vapor pipe;
- Fig. 8 is a fragmentary view of the interior of the inner shell of the container of Fig. 1 and illustrates the manner of constructing the same;
- Fig. 9 is an enlarged view of two of the sphere plates of Fig. 8 and illustrating the manner in which such plates are maintained in relative position during erection until permanently secured together;
- Fig. 10 is a fragmentary perspective view illustrating two sphere plates in the upper half 01' the inner shell of the container and shows the clips for temporarily holding such plates together and the groove between the plates for reception of the weld metal
- Fig. 11 is a fragmentary sectional view taken through a typical weld seam in the lower portion of the inner shell;
- Fig. 12 illustrates in fragmentary perspective certain structural details of the container of Fig. 1;
- Fig. 13 is a medial sectional view, partly diagrammatic, of a modified form of container which is ellipsoidal in shape;
- Fig. 14 is an elevational view on a, reduced scale of the ellipsoidal container of Fig. 13;
- Fig. 15 is a view similar to Fig. 13 of a further modified form of tank having a spheroidal shape.
- Fig. 16 is a partial elevational view of the container of Fig. 15.
- Insulated containers of the character here involved are intended primarily to constitute means for supplementing the supply of natural gas or other gaseous fuels or materials to a distributing system which, for example, furnishes gas to domestic and industrial users.
- a distributing system which, for example, furnishes gas to domestic and industrial users.
- such containers must have a large capacity and the liquefied gas must be available whenever required.
- the demand for fuel gas ordinarily increases very markedly and often to a point beyond the ability of the pipe line to supply such gas; under such circumstances my present tanks or containers fill all requirements.
- Spherical containers such as those here involved are characterized by having a maximum strength and volumetric capacity for a minimum size and weight and by a minimum external surface for a given volume. I, therefore, prefer a container which has a spherical shape but I have found that some departures can be made from a true sphere while still retaining the principles of my invention and that I may, for example, employ containers which are spheroids, ellipsoids or other variants of true spheres. In each case the container is supported above the earths surface and this is advantageous not only because the atmosphere is permitted to circulate entirely around ,the container to equalize the temperature thereof but also to keep the ground below and adjacent the containers from freezing.
- the spherical container of Fig. 1 et seq. has an outer metallic shell I and an inner metallic shell I I which is smaller than and generally concentric with the outer shell so as to provide therebetween a spherical chamber II, which is completely filled with an insulating material 13 capable of constitutingan eifective barrier against the infiltration of heat from the outside atmosphere to the interior of inner shell I I.
- the major portion of the chamber between the inner and outer shells is filled with granular insulating material, in this instance cork.
- the insulating material is preferably in the form of cork blocks or other shapes since such insulation must also serve the purpose of supporting the inner shell. I have found that molded cork blocks are entirely satisfactory where comparatively large or concentrated loadsare involved since molded cork blocks are of low heat conducting value and have the ability to withstand the imposed compressive loadings at temperatures below 100 F. without progressive yielding, creep or settling.
- the heat insulating material between the shells may differ in thickness from bottom to top.
- the insulation is of the molded block type from the bottom up to a point which is not above the mid-point of the container and I have determined that for structural and functional reasons the block type insulation should extend upwardly for about 45 from the bottom, i. e., this type of insulation is used in about the bottom fourth of the container.
- the granular insulating material between the top portions of the shells is considerably thicker than the block type insulation between the bottom portions of the shells, as shown.
- the ratio is approximately 5:3.
- the granular type insulation between the shell tops is 5 feet, but other ratios may be employed depending upon the desired temperature gradient between the atmosphere and the contents of the container, the cost of the insulation and other recognized factors.
- the granular type of insulation is ordinarily much less expensive than the block type, but the former is not capable of sustaining considerable loads as is the block type.
- the upper portion of the container is that subjected to the sun's rays and the thicker insulation is thus desirable there.
- Equal thicknesses of granular and block type insulating material have approximately equal thermal efliciency.
- Shells II and II are each composed of a plurality of metal plates I4 and I5, respectively, so shaped and welded together as to form the spherical shells aforesaid.
- inner shell II is composed of a special material which does not become unduly embrittled at the low temperatures to which such shell is subjected during use.
- the outer shell is completed by metal saucers l6 and the inner shell by similar saucers l1, suitably welded in place.
- Fig. 8 which is a view of the interior of the inner shell II, it will be observed that this shell is made up of three series of plates. viz., a set of central plates l5 and two sets of polar or end plates l5" and i5'.
- the central plates are relatively long and constructed in the general manner of barrel staves. They are welded to one another along their longitudinal edges, as can be noted by the seams 15a. Plates ii are curved both longitudinally and transversely and, of course, the curvatures are imparted in such manner and extent as to provide a central sphere portion of the requisite size when the plates are assembled.
- end plates I! and I' are likewise curved both longitudinally and transversely and are so shaped as to substantially complete the polar regions of the sphere. They are welded together along the weld lines l5b. Metal saucers II are welded in place in the locations shown, I5c being the circular welds. It will be understood that all the welded seams in the inner shell are so formed as to be fluid-tight since the inner shell constitutes the receptacle for the liquefied gases or other liquids existing at low temperatures.
- austenitic steels suitable for low temperature use include 18-8, which is an alloy composed of approximately 18% chromium, approximately 8% nickel, carbon up to about .20% with the balance substantially all iron except for the usual contaminants such as sulphur, phosphorus and the like in common amounts.
- the austenitic steels are, however, relatively expensive and, therefore, are not economical for large containers.
- nickel steel with a nickel content of about 3 /2% as such is an eminently satisfactory material. It is composed of low carbon steel to which has been added approximately the amount of nickel designated, but in this connection I wish to point out that nickel may be circulates completely around the same and, therefore, equalizes the temperature thereof.
- the outer shell While the inner surface of the outer shell is in contact with the insulating material, the outer shell is at no time reduced to a temperature low enough to cause it to fail.
- I preferably fabricate the outer shell from standard carbon steel sheets or plates which are, as understood, suitably configured so as to produce, when assembled, a shell of the desired size and diameter.
- the outer shell III i provided with a circular stiffening ring 18 which is horizontally disposed and welded thereto somewhat above its equatorial section. Between the stiffening ring l8 and the top portion of the shell I provide the stiffeners I9 which, it will be noted, are 8.1-
- the inner shell ll of my new container may be composed of any metal or alloy which has an impact valueof at least 10 ft. lbs. at the particular temperatures involved in any given installation.
- the outer shell III is constructed similarly to the inner shell H and is composed of a series of central carbon steel plates 14' and polar or end plates l4" and I4', the plates being shaped, assembled and welded in a manner which will be understood from the figures in question and from Fig. 8.
- the outer shell is not subjected to the influence of a low temperature and, therefore, need not be made of a special material like that of the inner shell although it must be fluid tight. It will be appreciated that the outer shell is in constant contact with the atmosphere which ranged in the manner of meridians of longitude on the earth's surface and thus converge toward the top of the shell.
- stifieners 19 may be varied in accordance with the particular installation and especially in accordance with the size of the container.
- the circular horizontal stiffening ring I8 is T-shaped in section, that the horizontal web l8 thereof has its inner edge attached (welded) to the outer shell I0 and that the flange I8" is disposed vertically.
- Fig. 12 also discloses that each of the stiffeners I9 is T-shaped in section and that the lower end of the web 19' thereof is secured to the web l8 of stiffening ring I8 by means of angle plates 20 which are bolted or riveted together and to the stiffener ring web as at 2
- the flange l9" of each such rib l9 has its lowermost edge resting upon the upper edge of the flange l8" of the stiffening ring IS.
- the outer shell I0 is, as shown, supported an appreciable distance above th surface of the earth, which in Fig. 1 is designated by the ground line 24.
- Columns 25 are provided and are spaced around the container in a circular row, being welded or otherwise suitably secured to the outer shell at the areas of contact. The particular size, shape and spacing of such columns depends to some extent upon the size of the container and the weight of the liquid contents thereof.
- the lower ends of these columns 25 are provided with base plates 26 which rest upon or are embedded in the concrete foundations 21 which are of substantial size and strength and the lower portions of which are'properly enlarged and embedded in the earth. It will be understood that the weight of the container and its contents is transferred to the foundations through columns 25.
- the columns 25 be guyed for purposes of added stability and in Fig. 1 I have illustrated the use of guy rods 28, the ends of which are securely connected to plates 25, and tumbuckles 30 are provided for the usual purpose of varying or adjusting the tension on said rods.
- is provided, access to which may be had by any suitable means (not shown) such as a ladder or circular stairway.
- This balcony is composed of a lower circular girder 32 and an upper circular girder l3, and between the two are disposed the angular connecting members or bars 34.
- a suitable flooring generally composed of metal gratings extends inwardly from the girder 32 and may be suitably attached to shell i and that the girder 33 constitutes a guard and hand rail.
- Circular girders I l and 32 function as the upper and. lower flanges of a horizontal circular girder disposed at the level oi. the points of connection between outer shell I. and columns 25.
- the girder 32 is subjected to load and concentrates that load in the columns.
- My new container is provided with operating mechanism the general arrangement of which is shown in Fig. l but the details of which will be more clearly apparent from Figs. 2 and 5.
- Roof member 31 is provided with one or more rupture discs 42, the function and operation of which will be explained hereinafter.
- Thes ruptured discs are of frangible material and are normally maintained in unbroken condition between suitable clamping rings or the like 43, bolted together at H, and mounted on the short vertical tubes 45.
- a cylindrical housing 45 Near its lower endQpipe 35 passes downwardly through an opening in the top of a cylindrical housing 45.
- This housing has perforations 41 in its side wall and is suitably secured to an annular bottom member ll, as by welding. Bottom member ll is secured to the inner shell ll above an opening which is provided for that p rpose.
- the top 01' housing 48 has a central opening for accommodating pipe 35 to which it is welded.
- the housing top is also provided with an opening 49 which is a ed with an opening 50 in a horizontal plate-like member 5
- Pipe 35 passes through both the inner and the outer shells of the container, through the space therebetween and into a cylindrical member 52 which forms one end of a bootlike metal casing or housing 53, to be described.
- the upper and lower portions of pipe 35 are integrally connected together by an expansion joint or section 54.
- This expansion section is a short corrugated piece of pipe having a bellows-like structure and action and the ends thereof are flanged for connectionto the upper and lower portions of pipe 35 by means of bolts 55.
- pipe 35 makes a 90 turn to horizontal and extends through the horizontal portion 55 of boot-like metal casing or housing 53.
- Adjacent pipe 35 I provide a pipe 51 which serves both as an inlet and outlet pipe for the liquid contents of the container.
- This pipe is suitably maintained in appropriate position by a bracket member 58 extending from and secured to pipe 35 and a cylindrical collar 59, the wall of which is beveled at its upper end to provide a tapering opening and seat for the reception of a plug valve 65 which is correspondingly tapered.
- the plug valve is secured on the lower end of a guide rod 5
- Guide rod 5! passes through guide discs 53 which are secured in the position shown in Fig. 2 by means of welding, brazing or the like, and they ensure that the plug valve in it downward travel will always seat accurately in the upper end of the outlet and inlet pipe 51.
- the position illustrated in Fig. 2 shows the plug valve in its upper or open position.
- Pipe 51 is also provided with an expansion joint or section 54'- similar to that in the pipe 85. Below the expansion section, pipe 51 turns through 90 and passes through the end wall of pipe 35, thereafter traveling concentrically within the horizontal portion of pipe 35, as shown. Pipes 35 and 51 are provided with similar expansion Joints or sections 5
- Pipe 51 when the tank is being filled, contains liquefied gas at a temperature of about --"244 F. and at a pressure of about 15 pounds per square inch gauge. when this liquefied gas enters the tank, its pressure is reduced at the 'surface to about five pounds per square inch gauge and its temperature is reduced to about 254 F. A portion of the liquefied gas within the tank evaporates, lowering the temperature of the remainder and the flash or evaporated gas has the same temperature, namely -254 F. This flash gas is conducted out of the tank through vent pipe 35.
- vent pipe 35 surrounds the horizontal portion of pipe 51 which conducts the liquefied gas into and from the tank.
- the temperature of this flash or vent gas at this point is somewhat warmer than 254 F. and ranges around 225' F. because of absorption of heat from the insulation within the casing or housing 53.
- Heat entering boot-like casing or housing 53 travels slowly through the insulation surrounding vent pipe 35 and is absorbed by the vent gas in pipe 35, thus raising the temperature of such gas. Only a very small amount of such heat is conducted to pipe 51 because of the small tem- 40 perature difierence'between pipes 51 and 35 with the result that most of the heat which is conducted into the boot-like casing 53 from the outside is absorbed by the vent gas leaving the tank and is thus prevented from being absorbed by the liquefied gas entering the tank.
- vent gas conduit 35 which extends outwardly beyond the tank or container is arranged in heat shielding relation to the outwardly extending portion of liquefied gas pipe 51 improves the thermal efilciency of the tank and makes it unnecessary to reliquefy such portion of the liquefied gas that would have been evaporated if it were not for such arrangement.
- the vertical wall portion of boot 53 is provided with an access opening normally closed by a cover 54.
- the boot is also provided with a metal chamber 55 welded or otherwise secured thereto and communicating with the interior of the boot.
- Chamber is filled with a filtering material it such as steel wool, mineral wool or the like, and is preferably packed in suchmanner that the density of the filtering mediumincreases in a radially outward direction. This may be accomplished by packing the filtering material tightly in the chamber adjacent the outer end thereof and then successively more loosely packing in the filtering material in the direction of the boot.
- the boot and the insulation can be relieved 01. air and moisture and reduced to a low internal pressure which enhances the insulating efiect. This then becomes the resultant insulating eflfect produced both by evacuation and the use of insulating materiaL- Since during evacuation there is some tendency for insulating granules to move toward the needle valve, the use of filtering material as described prevents obstruction of the valve and loss of insulating material and, if I desire, I may reduce the tendency of the granular insulating material to move toward the needle valve by employing cork blocks, strips or sheets (not shown) over the opening in the boot where the chamber 65 is attached, and such cork pieces may be similar to those between the lower portions of the container shells.
- pipe 35 begins to taper somewhat beyond the outer end 69 of the horizontal portion of boot 53, and pipe 51 serving as the inlet and outlet for liquefied gas passes through end 69 and extends therebeyond.
- Outlet pipe 51 is, however, provided just beyond the boot with a branch offtake pipe 10, suitably valved, and which may lead to or be connected to any suitable mechanism, such as a regassifier, since the primary function of the withdrawn liquefied gas is to supplement a gas distributing system.
- Vent gas conduit 35 beyond the outer end of boot-like casing 53 is provided with a branch conduit II which is of substantially the same cross sectional area as the vent gas conduit and which extends upwardly to a position above the top of the container as disclosed in Fig.
- this branch conduit is provided with one or more valve devices designed to open at a predetermined or excessive pressure.
- This branch conduit serves as an emergency device for venting gas from conduit 35 in the event of such rapid generation of gas in the container that a material increase in in- ..ternal pressure ensues.
- Outer shell I of the container is provided with a cylindrical polar cap piece 13 having a depending flange which is secured to the edge wall of an opening in the top of the shell.
- This cappiece is provided with a cylindrical collar portion 14 terminating in a horizontal annular flange which is bolted at 15 or otherwise suitably secured to the lower horizontal flange of a short vertical section of pipe 16, the upper portion of which has secured thereto an annular tray-like member 11.
- This sub-assembly is completed by a closure disc 18 resting on the top of the pipe section I6 and having a depending flange 19 projecting into the tray-like member 11.
- Oil or some other suitable sealing medium is contained in the tray-like member 11 so as to cut oil communication under normal conditions with the atmosphere above the container.
- the parts just described are above the rupture discs 42 and are placed into communication with the interior of inner shell II when the rupture discs become broken due to the existence of excess pressure within the said inner shell.
- Cable member 62 passes up through one or more guides 80, projecting radially from and welded to pipe 35.
- the cable member 62 passes through the inner shell within a hollow box-like member 8
- has an upper closure member 82 which has an opening through which a rod 83, attached to the upper end of cable 62, extends.
- the upper end of rod 83 is provided with a manually operable device 84 maintained in position by a tripod-like support 85.
- Rod 83 has a threaded portion which engages a nut-like member 86.
- rod 83 is drilled to receive a transversely extending cotter pin or the like 81 which prevents downward movement of rod 83 beyond a predetermined point and also prevents accidental disassembly.
- device 84 which is provided with spokes or handles, valve 60 through the movement of rod 83, cable 62, rod 6
- rod 83 can be raised or lowered vertically through the nut-like member by appropriate manipulation of device 84.
- is also provided with an access opening 88 anda cover 89.
- a cylindrical collar 90 is positioned therearound in spaced relationship.
- the upper end of cylindrical collar 90 is provided with a sealing tray 9
- a flanged covering member 92 rests in the sealing tray and has an outwardly and downwardly extending annular flange 93 which, with the sealing liquid in tray 9
- the top of collar 90 is provided with a removable disc-like closure member 94 which is normally bolted in place as at 95, as shown, to the flanged upper end of a short tubular piece 96 rising from and communicating with cover member 92.
- the boot 53 Since the boot 53 is of considerable weight and length, it is desirable to so support pipe 35 that it can not be harmfully affected by movement of the boot. I therefore provide means for supporting pipe 35 adjacent expansion section 54 and therefore adjacent the supported end of the boot.
- this includes means for limiting the downward expanding movement of expansion joint 54.
- This means comprises a pair of vertically spaced two-part clamping rings 91 bolted together at 98 and a plurality of vertically arranged angularly spaced bars 99 which are bolted at I00 or otherwise suitably secured to lugs 0
- I also provide, as shown in Figs. 5 and 6, means for limiting lateral movements of pipe 35 with relation to expansion joint or section 54.
- This means includes a plurality of chains or other flexible connecting members I02, the outer ends of which are connected to plates I03, by means of yokes I04. which are secured to the outer portion of the boot wall and the inner ends of which are connected by means of yokes M4 to an annular supporting ring
- 05 which surrounds the lowermost end of the vertical portion of pipe 35.
- the purpose of these supports is to restrain collar I05 from movement in a horizontal direction, thus relieving expansion joint 54.
- These supports also prevent damage to expansion joint 54" by horizontal movement laterally of the boot.
- These supports permit slight vertical movement of collar I05 which occurs when the container is cooled down or warmed up due to expansion of the metal between such collar and the inner shell I by which pipe 35, through housing 46, is supported.
- the outer shell I0 is provided with a plurality of manholes I06 to give access to the interior thereof and to provide means for introducing insulating material into the space between the shells.
- the precise number, size and spacing of suchv manholes depend upon the size and nature of the particular container.
- the outer shell is provided with apertures in which short pipes III! are inserted and suitably secured as by welding.
- Such pipes are usually flanged at their outer ends and are normally closed by a manhole cover or closure I08.
- the inner shell II is provided with only two such manholes I09 and, as particularly shown in Figs.
- breather valves III are provided for the usual purpose in a polar fitting III secured to the top of the outer shell.
- a spherical container As explained above, my present invention is not limited to the use of a spherical container and in Figs. 13 and 14 I have illustrated an ellipsoidal container.
- This comprises an inner ellipsoidal shell I I2 and an outer ellipsoidal shell II3 substantially uniformly spaced from the inner shell.
- insulating material I I4 is provided which constitutes an effective barrier against the infiltration of heat.
- This insulation is partly in granulated form and partly in the form of blocks, strips or sheets of cork or other suitable insulating medium. The latter are employed throughout the areas subjected to the most concentrated loading. As shown in Fig. 13, these areas are between the bottom portions of the two shells.
- FIG. 13 and 14 is shown somewhat diagrammati- Insofar as the provision of the boot II! is concerned. This is to be understood as being identical with or essentially the same as the boot 53 above described.
- a central vertical axial pipe II is provided which extends through the inner container and into the boot, and a liquid outlet pipe I" is provided in a manner which will be understood from what has preceded.
- the outer shell is supported by a plurality of spaced vertical columns III terminating at their lower ends in base plates II! which are associated, as before, with the foundations I2Il embedded in the earth up to a point such as that indicated by the ground line I2I. Braces or stress equalizers in the form of any rods I22 or the like are provided inamannersimilartothoseshowninFig. l.
- the outer shell may likewise also be provided with a circular girder I23 above its equatorial portion, and a balcony I24 completes the unit. These parts are described above in connection with Fig. 1.
- the container may be in the form of a spheroid or a modified sphere in which the lowermost portion is straightened or flattened so that the container has the form which a drop of liquid mercury normally assumes on a flat clean surface.
- a system of grillage beams between the tops of the columns Illa and the container bottom.
- These may be in the form of sets of metal beams I25 and I26 arranged at right angles to one another. The grillage equalizes the stresses on the container bottom and transmits the load to the columns and thence to the foundations and into the ground.
- FIG. 9 typical welding'operations in connection with the fabrication of the inner shell II are carried out by associating a pair of plates such as those designated at I5 and I5 in the relationship shown in Fig. 9 and temporarily securing the same together mechanically by means of clips, one of which, for the upper part of such shell is illustrated in Fig. 10.
- Each such clip is composed of two metal angle members I21, the flanges of -which are secured to the shell plates and the webs of which are secured together as by bolts I 28.
- the contiguous edges of the shell plates are beveled so as to provide 40 a V-shaped groove I29, the wider end of which is adjacent the clips.
- Weld metal is deposited in such groove and forms a particularly effective union between the plates. .After properly preparing the plates for welding as by cleaning the same they are preheated prior to welding. I have found that by preheating the plates to a temperature of from about 170-350 F., i. e., a temperature materially above the prevailing ambient temperature, an efiective weld is consistently secured. The weld metal becomes alloyed with the plates forming a permanent integral structure. As shown in Fig. 11, the lower plates of the inner shell may be welded in place, even though the cork blocks are combustible. In carrying out welding under such conditions, I first place a non-combustible member such as a refractory.
- a non-combustible member such as a refractory.
- An insulated container for storing liquefied gas comprising 'inner and outer spaced apart metallic shells insulated one from the other, means communicating with the innershell adjacent its bottom for conveying liquefied gas into and from said shell, a casing having fluid tight connection to the outer shell, extendingan appreciable distance from such connection and surrounding and spaced from said liquefied gas conveying means, a vent gas conduit communicating with the interior of the inner shell adjacent its top and having a portion thereof extending through said casing in heat shielding relation to said liquefied gas conveying means, said conduit being of suflicient cross sectional area to provide a free vent for vapors forming within the inner shell above the liquefied gas contained therein, and means for insulating said casing from said conduit and said liquefied gas conveying means.
- An insulated contained for storing liquefied gas comprising inner and outer spaced apart metallic shells insulated one from the other, means communicating with the inner shell adjacent its bottom for conveying liquefied gas into and from said shell, a casing having fluid tight connection to the outer shell, extending an appreciable distance from such connection and surrounding and spaced from said liquefied gas conveying means, a vent gas conduit communicating with the interior of the inner shell adjacent its top and having a portion thereof extending through said casing in heat shielding relation to said liquefied gas conveying means, said conduit being of suificient cross sectional area to provide a free vent for vapors forming within the inner shell above the liquefied gas contained therein, valve means within the inner shell for controlling said liquefied gas conveying means. and means operable from the exterior of the container for opening and closing said valve means.
- An insulated container for storing liquefied gas comprising inner and outer spaced apart metallic shells with insulating material therebetween, a metallic boot-like casing having fluid tight connection to the lower part of the outer shell and extending an appreciable distance from such connection, a pipe serving as a liquefied gas inlet and outlet, having an orifice within the inner shell adjacent its bottom and extending from such orifice into andthrough said casing, a vent gas conduit extending from near the top of the inner shell through an opening in the outer shell and through said casing in heat shielding relation to said pipe, insulation between said casing and said conduit, means operable from the exterior of the container for opening and closing said orifice, and means within said casing for flexibly supporting said conduit.
- An insulated container for storing liquefied gas comprising inner and outer spaced apart metallic shells with heat insulating material therebetween, a pipe serving as a liquefied gas inlet and outlet pipe, a vent gas conduit within the inner shell extending above the liquefied gas level, secured within an opening in the bot.- tom of such shell and substantially paralleling said pipe where the latter passes through said insulating material, means in said conduit and pipe for compensating for movement thereof due to temperature changes, and means providing a support for the upper portion of said conduit and which includes a, sliding joint.
- An insulated container for storing liquefied gas comprising inner and outer spaced apart me- P tallic shells, insulation between such shells.
- liquefied gas pipe having an orifice within and near the bottom of the inner shell and extending outwardly beyond the container, a vent gas discharge conduit having its inlet adjacent the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells with a portion thereof arranged in heat shielding relation to said liquefied gas pipe.
- a container for storing liquefied gas comprising inner and outer spaced apart metallic shells, heat insulating material between said shells, a liquefied gas pipe having an orifice within and near the bottom of the inner shell, a vent gas discharge conduit having its inlet adjacent the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells and then laterally beneath the container with part thereof arranged in heat shielding relation to said liquefied gas pipe and a casing having fluid tight connection with the lower portion of said outer shell and extending an appreciable distance from such connection and surrounding said vent gas conduit and said D D 7.
- a container for storing liquefied gas comprising inner and outer spaced apart metallic shells, heat insulating material within the space between said shells, a liquefied gas pipe having an orifice within and near the bottom of the inner shell, a vent gas discharge conduit having an inlet near the top of the inner shell, extending downwardly through the bottoms of the inner and outer shells and having'part thereof arranged in heat shielding relation to said pipe, a valve controlling the flow of liquefied gas through said orifice, and means operable from the exterior of the container for controlling said valve.
- An insulated container for storing liquefied gas comprising inner and outer spaced apart metallic shells insulated one from the other, a liquefied gas conduit having a valve controlled orifice within and near the bottom orthe inner shell and extending outwardly beyond the container, a vent gas discharge conduit having its inlet near the top oi the inner shell and extending downwardly and outwardly through the inner and outer shells and beyond the container and having a portion thereof arranged in heat shielding relation to said liquefied: gas conduit, and a liquefied gas outlet pipe connected to said liquefied gas conduit.
- a container for storing liquefied gas comprising inner and outer spaced apart metallic shells, heat insulating material within the space between said shells, a vent gas discharge conduit having its inlet near the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells. and a cylindrical member attachedto the upper portion of the inner shell and surrounding the upper end of said conduit, the upper end oi said conduit having a sliding fit with said cylindrical member.
- A'reservoir for storing liquefied natural gas comprising inner and outer metallic shells, heat insulating material within the space between such shells, a. vent gas discharge conduit having its inlet near the top of the inner shell to about chromium and from about 10% to about 26% nickel; the inner shell having attached to .one 01 its surfaces and straddling the Joints between its adjacent plate sections, metallic strap-like members formed to provide pockets for said weld metal, and protective members of non-combustible material located between the insulating material and the strap-like members attached to the lower portion of such shell; such protective members being held in place by such insulating material,
- vent gas discharge conduit extends vertically within the inner shell and terminates near the top thereof.
- vent gas conduit extends vertically within and extending downwardly and outwardly 39 the inner shell and includes a sliding joint to through and beyond such shells, and a branch conduit connecting with said gas conduit outside of the reservoir and extending above the same; said branch conduit being provided with provide for expansion and contraction of such inner shell.
- inner and outer shells are substantially a check valve constructed to permit escape 01 gas spherical and the vent gas conduit extends verwhen excessive evaporation occurs within the inner shell.
- An insulated container for storing liquefied gas comprising inner and outer spaced apart metallic shells, insulating material arranged in the space between said shells; the innor shell being fabricated from sections or steel alloy plate containing from-about 2% to about 10% nickel; said plate sections being joined togetherby weld metal containing from about 15% mchanges.
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Description
Oct. 16, 1945. j O JACKSON 2,386,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 7 Sheets-Sheet l Oct. 16, 1945. J. o. JACKSON 2,386,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 7 Sheets-Sheet 2 15 67 35 INYENTOR =9 2. (v m awwyfl am M Oct. 16, 1945. O JACKSON 2,386,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 7 Sheets-Sheet 5 Oct. 16,- 1945. J. o. JACKSON 2,386,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 '7 Sheets-Sheet.4
Get. 16, 1941-5. O JACKSON 2,336,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 7 Sheets-Sheet 5 I I gNVENTgliJ 3Y4 hl e t 47%!) A TTORNE Y5 00E lfi, 1945. J O JACKSON 2,386,958
SPHERICAL TYPE INSULATED CONTAINERS FOR LIQUEFIED GASES Filed Jan. 8, 1942 '7 Sheets-Sheet 6 Get. 16, 1945. J. o JACKSON SPHERICAL TYPE INSULATED CONTAINERS FO R LIQUEFIED GASES Filed Jan. 8, 1942 '7 Sheets-Sheet 7 Patented Oct. 16, 1945 SPHERICAL TYPE INSULATED CONTAINER FOR LIQUEFIED GASES James 0. Jackson, Grafton, Pa., assignor to Pittsburgh-Des Moines Company, a corporation of Pennsylvania Application January 8, 1942, Serial No. 426,012
21 Claims.
This invention relates to insulated containers of relatively great size capable of storing extremely cold liquids such, for instance, as liquefied natural gas.
An object of this invention is to produce an insulated container capable of safely and economically storing for long periods a relatively great quantity of liquefied gas such as liquefied natural gas.
Liquefied natural gas at atmospheric pressure has a temperature far below F. (actually about 258 F.) and is subject to some evaporation and another object of this invention is to provide means for safely and economically taking care of the gas resulting from evaporation of liquefied natural gas stored in an insulated container of relatively great size.
A further object of this invention is to produce means for safely and economically introducing and withdrawing liquefied natural gas from insulated containers of relatively great size.
A further object is to produce improved mechanism by means of which low temperature liquefled gas can be charged into and removed from a relatively large insulated storage tank without damage to such tank or such mechanism.
A further object is to produce improved mechanism for controlling the flow of liquefied gas into and from an insulated storage tank of relatively great size, without permitting conduction to such tank of an appreciable amount of heat.
A still further object is to produce improved mechanism for controlling and limiting to a safe value, pressures generated bythe evaporation of liquefied gas within an insulated storage tank of relatively great size.
In the accompanying drawings wherein I have illustrated successful embodiments oithe present invention:
Fig. 1 is an elevational view, partly in section, of a preferred form of insulated spherical container responding to my present invention;
Fig. 2 is an enlarged vertical fragmentary section through the axial portion of the container of Fig. 1;
Fig. 3 is a plan view, with certain parts omitted and broken away, of the container of Figs. 1 and 2;
Fig. 4 is a vertical elevational view of the upper portion of the container of Figs. 1 to 3, inclusive, taken at right angles to Fig. 1;
Fig. 5 is an enlarged sectional view, partly in elevation, through the boot shown in Fig. 1 and illustrates certain additional devices not shown in Figs. 1 and 2, the insulation surrounding the gas vent pipe not being shown in this figure;
Fig. 6 is a horizontal sectional view illustrating the manner in which the lower end of the vapor pipe is supported within the boot and is taken along the line VIVI of Fig. 5;
Fig. 7 is an enlarged plan view of parts of Fig. 5 illustrating the means for maintaining and supporting the expansion joint in the lower end of the vapor pipe;
Fig. 8 is a fragmentary view of the interior of the inner shell of the container of Fig. 1 and illustrates the manner of constructing the same;
Fig. 9 is an enlarged view of two of the sphere plates of Fig. 8 and illustrating the manner in which such plates are maintained in relative position during erection until permanently secured together;
Fig. 10 is a fragmentary perspective view illustrating two sphere plates in the upper half 01' the inner shell of the container and shows the clips for temporarily holding such plates together and the groove between the plates for reception of the weld metal Fig. 11 is a fragmentary sectional view taken through a typical weld seam in the lower portion of the inner shell;
Fig. 12 illustrates in fragmentary perspective certain structural details of the container of Fig. 1;
Fig. 13 is a medial sectional view, partly diagrammatic, of a modified form of container which is ellipsoidal in shape;
Fig. 14 is an elevational view on a, reduced scale of the ellipsoidal container of Fig. 13;
Fig. 15 is a view similar to Fig. 13 of a further modified form of tank having a spheroidal shape; and
Fig. 16 is a partial elevational view of the container of Fig. 15.
Like numerals designate corresponding parts throughout the various views of the drawings.
Insulated containers of the character here involved are intended primarily to constitute means for supplementing the supply of natural gas or other gaseous fuels or materials to a distributing system which, for example, furnishes gas to domestic and industrial users. To be of value. such containers must have a large capacity and the liquefied gas must be available whenever required. For example, in the wintertime or during cold weather the demand for fuel gas ordinarily increases very markedly and often to a point beyond the ability of the pipe line to supply such gas; under such circumstances my present tanks or containers fill all requirements. While there is always some vaporization or regasincation of the liquefied gas stored within the tank or container, my new containers are so constructed as to keep losses to a minimum and have such a capacity that, if unused, a tank full of liquefied gas would not be exhausted by evaporation or vaporization for approximately two years. The gaseous equivalent of the liquefied gas is approximately 600 times the volume of liquid. It is to be understood that one or a plurality of the present containers may be employed depending upon conditions, and that where more than one are employed they may be suitably interconnected by communicating piping.
Spherical containers such as those here involved are characterized by having a maximum strength and volumetric capacity for a minimum size and weight and by a minimum external surface for a given volume. I, therefore, prefer a container which has a spherical shape but I have found that some departures can be made from a true sphere while still retaining the principles of my invention and that I may, for example, employ containers which are spheroids, ellipsoids or other variants of true spheres. In each case the container is supported above the earths surface and this is advantageous not only because the atmosphere is permitted to circulate entirely around ,the container to equalize the temperature thereof but also to keep the ground below and adjacent the containers from freezing. were it attempted to rest the containers on the ground in the manner employed in connection with present day oil tanks, the low temperatures due to the liquefied gases contained therein would'cause freezing of the earth and a consequent heaving thereof. This would result in distorting or buckling the adjacent portions of the container and the introduction of undesired stresses. Such conditions are highly undesirable and would in some cases entirely destroy the utility of the container. It will, furthermore, be understood that the construction of large elevated insulated containers gave rise to numerous problems which had to be overcome. That such are successfully solved by the present invention is evidenced by the fact that containers embodying this invention are being successfully employed commer cially.
The spherical container of Fig. 1 et seq. has an outer metallic shell I and an inner metallic shell I I which is smaller than and generally concentric with the outer shell so as to provide therebetween a spherical chamber II, which is completely filled with an insulating material 13 capable of constitutingan eifective barrier against the infiltration of heat from the outside atmosphere to the interior of inner shell I I. As shown in Figs. 1 and 2 in particular, the major portion of the chamber between the inner and outer shells is filled with granular insulating material, in this instance cork. In the lower portion of this chamber between the bottom portions of the shells the insulating material is preferably in the form of cork blocks or other shapes since such insulation must also serve the purpose of supporting the inner shell. I have found that molded cork blocks are entirely satisfactory where comparatively large or concentrated loadsare involved since molded cork blocks are of low heat conducting value and have the ability to withstand the imposed compressive loadings at temperatures below 100 F. without progressive yielding, creep or settling.
It will further be observed from Fig. 1 in particular that the heat insulating material between the shells may differ in thickness from bottom to top. The insulation is of the molded block type from the bottom up to a point which is not above the mid-point of the container and I have determined that for structural and functional reasons the block type insulation should extend upwardly for about 45 from the bottom, i. e., this type of insulation is used in about the bottom fourth of the container. Above the block type insulation the insulation is of the granular type. While all the insulation is relatively compressible, the block type of insulation which is less compressible than the granular type is necessary for load-supporting purposes and it will be noted that the inner shell rests directly upon such block type insulation. The granular insulating material between the top portions of the shells is considerably thicker than the block type insulation between the bottom portions of the shells, as shown. In Fig. 1, the ratio is approximately 5:3. Thus, for block type insulation 3 feet in thickness between the shell bottoms, the granular type insulation between the shell tops is 5 feet, but other ratios may be employed depending upon the desired temperature gradient between the atmosphere and the contents of the container, the cost of the insulation and other recognized factors. In this connection, the granular type of insulation is ordinarily much less expensive than the block type, but the former is not capable of sustaining considerable loads as is the block type. Again, the upper portion of the container is that subjected to the sun's rays and the thicker insulation is thus desirable there.
Equal thicknesses of granular and block type insulating material have approximately equal thermal efliciency.
It will further be appreciated that when the 40 block type insulation compresses due to the weight of the inner shell and its contents, the axial pipe (35) moves downwardly, sometimes as much as 6 inches. Thus, the expansion joints hereinafter described as well as the sliding fit at the upper end of such pipe become necessary and important adjuncts of the container not only on account of movements due to compression of the insulation but also to take care of expected contraction and expansion due to temperature changes.
Shells II and II are each composed of a plurality of metal plates I4 and I5, respectively, so shaped and welded together as to form the spherical shells aforesaid. As will hereinafter more ordinary carbon steel but inner shell II is composed of a special material which does not become unduly embrittled at the low temperatures to which such shell is subjected during use. The outer shell is completed by metal saucers l6 and the inner shell by similar saucers l1, suitably welded in place.
Referring to Fig. 8, for example, which is a view of the interior of the inner shell II, it will be observed that this shell is made up of three series of plates. viz., a set of central plates l5 and two sets of polar or end plates l5" and i5'. The central plates are relatively long and constructed in the general manner of barrel staves. They are welded to one another along their longitudinal edges, as can be noted by the seams 15a. Plates ii are curved both longitudinally and transversely and, of course, the curvatures are imparted in such manner and extent as to provide a central sphere portion of the requisite size when the plates are assembled. The end plates I!" and I' are likewise curved both longitudinally and transversely and are so shaped as to substantially complete the polar regions of the sphere. They are welded together along the weld lines l5b. Metal saucers II are welded in place in the locations shown, I5c being the circular welds. It will be understood that all the welded seams in the inner shell are so formed as to be fluid-tight since the inner shell constitutes the receptacle for the liquefied gases or other liquids existing at low temperatures.
Since many metals and alloys become embrittled at low temperatures, and thus lose ductility and their ability to withstand strains, it is necessary to employ special metals and alloys which do not become unduly embrlttled even at temperatures as low as about -260 F. It has been found that a metal or alloy which has, at the low temperature involved, an impact value (Charpy) of less than ft. lbs. is unsatisfactory for use under the conditions encountered. Or-
dinary mild steels or low carbon steels as well as many other common or well-known metals and alloys, when tested at low temperatures, have an impact value as low as 2-3 ft. lbs., which represents practically complete loss of ductility and renders them valueiess for low temperature service. I have found that the austenitic steels are highly resistant to embrittlement at low temperature, and even at temperatures in the neighborhood of -260 F. have an impact value well over 10 ft. lbs. and thus are capable of use for the inner shell in my new container. Among the austenitic steels suitable for low temperature use I include 18-8, which is an alloy composed of approximately 18% chromium, approximately 8% nickel, carbon up to about .20% with the balance substantially all iron except for the usual contaminants such as sulphur, phosphorus and the like in common amounts. The austenitic steels are, however, relatively expensive and, therefore, are not economical for large containers. I prefer to employ nickel steel with a nickel content of about 3 /2% as such is an eminently satisfactory material. It is composed of low carbon steel to which has been added approximately the amount of nickel designated, but in this connection I wish to point out that nickel may be circulates completely around the same and, therefore, equalizes the temperature thereof. While the inner surface of the outer shell is in contact with the insulating material, the outer shell is at no time reduced to a temperature low enough to cause it to fail. Thus, I preferably fabricate the outer shell from standard carbon steel sheets or plates which are, as understood, suitably configured so as to produce, when assembled, a shell of the desired size and diameter.
Referring further to Fig. 1, it will be observed that the outer shell III i provided with a circular stiffening ring 18 which is horizontally disposed and welded thereto somewhat above its equatorial section. Between the stiffening ring l8 and the top portion of the shell I provide the stiffeners I9 which, it will be noted, are 8.1-
employed up to approximately 10% and that even rather small percentages of nickel in fractional amounts below 1% constitute a substantial improvement over straight low carbon steel. Such variations are deemed to be a part hereof and it is also within the scope of my invention to employ metals which do not become embrittled at the low temperatures involved, such as copper and aluminum. In general, I wish to point out that the inner shell ll of my new container may be composed of any metal or alloy which has an impact valueof at least 10 ft. lbs. at the particular temperatures involved in any given installation.
The outer shell III, as will be best observed from Figs. 3 and 4, is constructed similarly to the inner shell H and is composed of a series of central carbon steel plates 14' and polar or end plates l4" and I4', the plates being shaped, assembled and welded in a manner which will be understood from the figures in question and from Fig. 8. The outer shell is not subjected to the influence of a low temperature and, therefore, need not be made of a special material like that of the inner shell although it must be fluid tight. It will be appreciated that the outer shell is in constant contact with the atmosphere which ranged in the manner of meridians of longitude on the earth's surface and thus converge toward the top of the shell. The number, size and spacing of stifieners 19 may be varied in accordance with the particular installation and especially in accordance with the size of the container. By referring to Fig. 12 it will further be appreciated that the circular horizontal stiffening ring I8 is T-shaped in section, that the horizontal web l8 thereof has its inner edge attached (welded) to the outer shell I0 and that the flange I8" is disposed vertically.
Fig. 12 also discloses that each of the stiffeners I9 is T-shaped in section and that the lower end of the web 19' thereof is secured to the web l8 of stiffening ring I8 by means of angle plates 20 which are bolted or riveted together and to the stiffener ring web as at 2|, or these parts may be secured in any other suitable manner as by welding, if preferred. The flange l9" of each such rib l9 has its lowermost edge resting upon the upper edge of the flange l8" of the stiffening ring IS. The relation of such parts to the plates I4 and I47 of the outer container I0 is likewise delineated and a connection is made between the underside of the web l8 to the adjacent plate It by means of angle plates 22 suitably bolted, riveted, welded or otherwise suitably secured thereto as at 23.
The outer shell I0 is, as shown, supported an appreciable distance above th surface of the earth, which in Fig. 1 is designated by the ground line 24. Columns 25 are provided and are spaced around the container in a circular row, being welded or otherwise suitably secured to the outer shell at the areas of contact. The particular size, shape and spacing of such columns depends to some extent upon the size of the container and the weight of the liquid contents thereof. The lower ends of these columns 25 are provided with base plates 26 which rest upon or are embedded in the concrete foundations 21 which are of substantial size and strength and the lower portions of which are'properly enlarged and embedded in the earth. It will be understood that the weight of the container and its contents is transferred to the foundations through columns 25. It is preferable but not essential that the columns 25 be guyed for purposes of added stability and in Fig. 1 I have illustrated the use of guy rods 28, the ends of which are securely connected to plates 25, and tumbuckles 30 are provided for the usual purpose of varying or adjusting the tension on said rods.
As will also appear from Fig. 1, a circular horizontal balcony 3| is provided, access to which may be had by any suitable means (not shown) such as a ladder or circular stairway. This balcony is composed of a lower circular girder 32 and an upper circular girder l3, and between the two are disposed the angular connecting members or bars 34. It is to be understood that a suitable flooring generally composed of metal gratings extends inwardly from the girder 32 and may be suitably attached to shell i and that the girder 33 constitutes a guard and hand rail. The particular details of the balcony are not per se a part of the present invention. Circular girders I l and 32 function as the upper and. lower flanges of a horizontal circular girder disposed at the level oi. the points of connection between outer shell I. and columns 25. Thus, the girder 32 is subjected to load and concentrates that load in the columns.
My new container is provided with operating mechanism the general arrangement of which is shown in Fig. l but the details of which will be more clearly apparent from Figs. 2 and 5. Roof member 31 is provided with one or more rupture discs 42, the function and operation of which will be explained hereinafter. Thes ruptured discs are of frangible material and are normally maintained in unbroken condition between suitable clamping rings or the like 43, bolted together at H, and mounted on the short vertical tubes 45.
Near its lower endQpipe 35 passes downwardly through an opening in the top of a cylindrical housing 45. This housing has perforations 41 in its side wall and is suitably secured to an annular bottom member ll, as by welding. Bottom member ll is secured to the inner shell ll above an opening which is provided for that p rpose. The top 01' housing 48 has a central opening for accommodating pipe 35 to which it is welded. The housing top is also provided with an opening 49 which is a ed with an opening 50 in a horizontal plate-like member 5| welded to housing 45 and to pipe 35. Pipe 35 passes through both the inner and the outer shells of the container, through the space therebetween and into a cylindrical member 52 which forms one end of a bootlike metal casing or housing 53, to be described. The upper and lower portions of pipe 35 are integrally connected together by an expansion joint or section 54. This expansion section is a short corrugated piece of pipe having a bellows-like structure and action and the ends thereof are flanged for connectionto the upper and lower portions of pipe 35 by means of bolts 55. At its lower end, pipe 35 makes a 90 turn to horizontal and extends through the horizontal portion 55 of boot-like metal casing or housing 53.
Adjacent pipe 35 I provide a pipe 51 which serves both as an inlet and outlet pipe for the liquid contents of the container. This pipe is suitably maintained in appropriate position by a bracket member 58 extending from and secured to pipe 35 and a cylindrical collar 59, the wall of which is beveled at its upper end to provide a tapering opening and seat for the reception of a plug valve 65 which is correspondingly tapered. The plug valve is secured on the lower end of a guide rod 5|, to the upper end of which is secured the lower end of a cable or the like 82. Guide rod 5! passes through guide discs 53 which are secured in the position shown in Fig. 2 by means of welding, brazing or the like, and they ensure that the plug valve in it downward travel will always seat accurately in the upper end of the outlet and inlet pipe 51. i The position illustrated in Fig. 2 shows the plug valve in its upper or open position.
The portions of the boot-like casing or housing surrounding these pipes and expansion sections are considerably larger than the pipes themselves, thus providing spaces which are filled with insulating material 13. Pipe 51, when the tank is being filled, contains liquefied gas at a temperature of about --"244 F. and at a pressure of about 15 pounds per square inch gauge. when this liquefied gas enters the tank, its pressure is reduced at the 'surface to about five pounds per square inch gauge and its temperature is reduced to about 254 F. A portion of the liquefied gas within the tank evaporates, lowering the temperature of the remainder and the flash or evaporated gas has the same temperature, namely -254 F. This flash gas is conducted out of the tank through vent pipe 35. The flash or vent gas passing from the tank through vent pipe 35 surrounds the horizontal portion of pipe 51 which conducts the liquefied gas into and from the tank. The temperature of this flash or vent gas at this point is somewhat warmer than 254 F. and ranges around 225' F. because of absorption of heat from the insulation within the casing or housing 53.
Heat entering boot-like casing or housing 53 travels slowly through the insulation surrounding vent pipe 35 and is absorbed by the vent gas in pipe 35, thus raising the temperature of such gas. Only a very small amount of such heat is conducted to pipe 51 because of the small tem- 40 perature difierence'between pipes 51 and 35 with the result that most of the heat which is conducted into the boot-like casing 53 from the outside is absorbed by the vent gas leaving the tank and is thus prevented from being absorbed by the liquefied gas entering the tank. The fact that that portion of vent gas conduit 35 which extends outwardly beyond the tank or container is arranged in heat shielding relation to the outwardly extending portion of liquefied gas pipe 51 improves the thermal efilciency of the tank and makes it unnecessary to reliquefy such portion of the liquefied gas that would have been evaporated if it were not for such arrangement.
The vertical wall portion of boot 53 is provided with an access opening normally closed by a cover 54. The boot is also provided with a metal chamber 55 welded or otherwise secured thereto and communicating with the interior of the boot. Chamber is filled with a filtering material it such as steel wool, mineral wool or the like, and is preferably packed in suchmanner that the density of the filtering mediumincreases in a radially outward direction. This may be accomplished by packing the filtering material tightly in the chamber adjacent the outer end thereof and then successively more loosely packing in the filtering material in the direction of the boot.
the boot and the insulation can be relieved 01. air and moisture and reduced to a low internal pressure which enhances the insulating efiect. This then becomes the resultant insulating eflfect produced both by evacuation and the use of insulating materiaL- Since during evacuation there is some tendency for insulating granules to move toward the needle valve, the use of filtering material as described prevents obstruction of the valve and loss of insulating material and, if I desire, I may reduce the tendency of the granular insulating material to move toward the needle valve by employing cork blocks, strips or sheets (not shown) over the opening in the boot where the chamber 65 is attached, and such cork pieces may be similar to those between the lower portions of the container shells.
As will be best noted from Fig. 5, pipe 35 begins to taper somewhat beyond the outer end 69 of the horizontal portion of boot 53, and pipe 51 serving as the inlet and outlet for liquefied gas passes through end 69 and extends therebeyond. Outlet pipe 51 is, however, provided just beyond the boot with a branch offtake pipe 10, suitably valved, and which may lead to or be connected to any suitable mechanism, such as a regassifier, since the primary function of the withdrawn liquefied gas is to supplement a gas distributing system. Vent gas conduit 35 beyond the outer end of boot-like casing 53 is provided with a branch conduit II which is of substantially the same cross sectional area as the vent gas conduit and which extends upwardly to a position above the top of the container as disclosed in Fig. 1. At its top, this branch conduit is provided with one or more valve devices designed to open at a predetermined or excessive pressure. This branch conduit serves as an emergency device for venting gas from conduit 35 in the event of such rapid generation of gas in the container that a material increase in in- ..ternal pressure ensues.
Outer shell I of the container is provided with a cylindrical polar cap piece 13 having a depending flange which is secured to the edge wall of an opening in the top of the shell. This cappiece is provided with a cylindrical collar portion 14 terminating in a horizontal annular flange which is bolted at 15 or otherwise suitably secured to the lower horizontal flange of a short vertical section of pipe 16, the upper portion of which has secured thereto an annular tray-like member 11. This sub-assembly is completed by a closure disc 18 resting on the top of the pipe section I6 and having a depending flange 19 projecting into the tray-like member 11. Oil or some other suitable sealing medium is contained in the tray-like member 11 so as to cut oil communication under normal conditions with the atmosphere above the container. The parts just described are above the rupture discs 42 and are placed into communication with the interior of inner shell II when the rupture discs become broken due to the existence of excess pressure within the said inner shell.
The top closure 82 of member 8| is also provided with an access opening 88 anda cover 89. In order to seal oil yet give access to the parts just described, a cylindrical collar 90 is positioned therearound in spaced relationship. The upper end of cylindrical collar 90 is provided with a sealing tray 9|. A flanged covering member 92 rests in the sealing tray and has an outwardly and downwardly extending annular flange 93 which, with the sealing liquid in tray 9| completes the seal. The top of collar 90 is provided with a removable disc-like closure member 94 which is normally bolted in place as at 95, as shown, to the flanged upper end of a short tubular piece 96 rising from and communicating with cover member 92.
Since the boot 53 is of considerable weight and length, it is desirable to so support pipe 35 that it can not be harmfully affected by movement of the boot. I therefore provide means for supporting pipe 35 adjacent expansion section 54 and therefore adjacent the supported end of the boot.
As will be understood from Figs. 5 and 7, this includes means for limiting the downward expanding movement of expansion joint 54. This means comprises a pair of vertically spaced two-part clamping rings 91 bolted together at 98 and a plurality of vertically arranged angularly spaced bars 99 which are bolted at I00 or otherwise suitably secured to lugs 0| extending outwardly from said clamping rings 91.
I also provide, as shown in Figs. 5 and 6, means for limiting lateral movements of pipe 35 with relation to expansion joint or section 54. This means includes a plurality of chains or other flexible connecting members I02, the outer ends of which are connected to plates I03, by means of yokes I04. which are secured to the outer portion of the boot wall and the inner ends of which are connected by means of yokes M4 to an annular supporting ring |05 which surrounds the lowermost end of the vertical portion of pipe 35. I prefer to use chains for these supports because of the low heat conductivity inherent in a chain. The purpose of these supports is to restrain collar I05 from movement in a horizontal direction, thus relieving expansion joint 54. These supports also prevent damage to expansion joint 54" by horizontal movement laterally of the boot. These supports permit slight vertical movement of collar I05 which occurs when the container is cooled down or warmed up due to expansion of the metal between such collar and the inner shell I by which pipe 35, through housing 46, is supported.
The outer shell I0 is provided with a plurality of manholes I06 to give access to the interior thereof and to provide means for introducing insulating material into the space between the shells. The precise number, size and spacing of suchv manholes depend upon the size and nature of the particular container. At such points the outer shell is provided with apertures in which short pipes III! are inserted and suitably secured as by welding. Such pipes are usually flanged at their outer ends and are normally closed by a manhole cover or closure I08. The inner shell II is provided with only two such manholes I09 and, as particularly shown in Figs. 3 and 4, these are preferably located at diametrically opposite points and in such relationship to a corresponding pair of manholes in'the outer shell as to enable access to be gained to the interior of the ,inner shell through such manholes in the outer shell. As will also be apparent from Figs. 3 and 4, breather valves III are provided for the usual purpose in a polar fitting III secured to the top of the outer shell.
As explained above, my present invention is not limited to the use of a spherical container and in Figs. 13 and 14 I have illustrated an ellipsoidal container. This comprises an inner ellipsoidal shell I I2 and an outer ellipsoidal shell II3 substantially uniformly spaced from the inner shell. Between the shells insulating material I I4 is provided which constitutes an effective barrier against the infiltration of heat. This insulation is partly in granulated form and partly in the form of blocks, strips or sheets of cork or other suitable insulating medium. The latter are employed throughout the areas subjected to the most concentrated loading. As shown in Fig. 13, these areas are between the bottom portions of the two shells. For simplicity and to prevent undue repetition, the ellipsoidal container of Figs. 13 and 14 is shown somewhat diagrammati- Insofar as the provision of the boot II! is concerned. this is to be understood as being identical with or essentially the same as the boot 53 above described. A central vertical axial pipe II is provided which extends through the inner container and into the boot, and a liquid outlet pipe I" is provided in a manner which will be understood from what has preceded. The outer shell is supported by a plurality of spaced vertical columns III terminating at their lower ends in base plates II! which are associated, as before, with the foundations I2Il embedded in the earth up to a point such as that indicated by the ground line I2I. Braces or stress equalizers in the form of any rods I22 or the like are provided inamannersimilartothoseshowninFig. l. The outer shell may likewise also be provided with a circular girder I23 above its equatorial portion, and a balcony I24 completes the unit. These parts are described above in connection with Fig. 1.
As further shown in Figs. and 16, the container may be in the form of a spheroid or a modified sphere in which the lowermost portion is straightened or flattened so that the container has the form which a drop of liquid mercury normally assumes on a flat clean surface. The correspondence of parts as compared with Figs. 13 and 14 will be clear from the numerals employed. In this form I have found it desirable to support the bottom of the outer shell by a system of grillage beams between the tops of the columns Illa and the container bottom. These may be in the form of sets of metal beams I25 and I26 arranged at right angles to one another. The grillage equalizes the stresses on the container bottom and transmits the load to the columns and thence to the foundations and into the ground.
assaoss The welding procedure utilized in connection with the fabrication of the inner shells of these containers will be more fully understood by referring to my copending applications Serial No. 425,756, filed January 6, 1942, now Patent-2,337,- 049 and Serial No. 427,069 filed January 16, 1942. From these it will be appreciated that difficulties are encountered in so producing these welded structures that they will have the necessary strength and ductility at low temperatures. Or-
dinary steels and conventional welds become em-- brittled at low temperatures, thereby suffering serious loss in ductility. It is required by the A. S. M. E. Code for Unfired Pressure Vessels that steel for low temperature vessels shall'have a Charpy impact value of at least ten ft. lbs. at the temperature at which it is to be used. By making the inner shell of each of my new containers out of a nickel steel containing about 3%% (3-4%) of nickel and by employing the procedure and weld metal, set forth in my aforesaid copending applications, I have made it possible to produce welded structures which even at temperatures as low as -260 F. have a Charpy impact value of from 18-20 ft. lbs at --260 F.
As illustrated in Figs. 9, 10 and 11, typical welding'operations in connection with the fabrication of the inner shell II are carried out by associating a pair of plates such as those designated at I5 and I5 in the relationship shown in Fig. 9 and temporarily securing the same together mechanically by means of clips, one of which, for the upper part of such shell is illustrated in Fig. 10. Each such clip is composed of two metal angle members I21, the flanges of -which are secured to the shell plates and the webs of which are secured together as by bolts I 28. It will be noted that the contiguous edges of the shell plates are beveled so as to provide 40 a V-shaped groove I29, the wider end of which is adjacent the clips. Weld metal is deposited in such groove and forms a particularly effective union between the plates. .After properly preparing the plates for welding as by cleaning the same they are preheated prior to welding. I have found that by preheating the plates to a temperature of from about 170-350 F., i. e., a temperature materially above the prevailing ambient temperature, an efiective weld is consistently secured. The weld metal becomes alloyed with the plates forming a permanent integral structure. As shown in Fig. 11, the lower plates of the inner shell may be welded in place, even though the cork blocks are combustible. In carrying out welding under such conditions, I first place a non-combustible member such as a refractory.
- with the surface thereof. I. then secure to the marginal portions of contiguous shell plates, as by spot welding, a metal backing-up strip I3I, the center of which is depressed as at I22 to form a shallow channel I33 between it and the adjacent surfaces of such shell plates. The V-shaped groove between the plates is then filled with weld metal I34, part of which enters the said shal- Below the mid horizontal section or the inner shell the welding is preferably carried on from the inside of the shell and above such section, the welding is preferably carried on from the outside. The weld grooves therefore for the lower half of the inner shell will be on the inside of such shell, while for the upper half the grooves will be on the outside.
It is to be understood that the particular shapes illustrated and described are submitted by way of example and are not to be deemed as limitative or restrictive. Within the purview of the present invention I may employ a container which is either spherical or a modified sphere such as the ellipsoidal or spheroidal forms described above. The expression spherical type container" is intended to cover all forms of container forming a part of the present invention, and where employed herein is generic in its significance. It is to be understood further that my new containers may be made of any required size and of any suitable materials and that while the containers are especially designed for storing relatively large quantities of liquefied gases or other liquids at relatively low temperatures, theoretically my new containers could also be employed in connection with the storage of hot liquids or liquids at elevated temperatures. The scope of the invention is rather that defined by the appended claims.
Having thus described my invention, what I claim as new and desire to secure by Letters Patent is:
1. An insulated container for storing liquefied gas, comprising 'inner and outer spaced apart metallic shells insulated one from the other, means communicating with the innershell adjacent its bottom for conveying liquefied gas into and from said shell, a casing having fluid tight connection to the outer shell, extendingan appreciable distance from such connection and surrounding and spaced from said liquefied gas conveying means, a vent gas conduit communicating with the interior of the inner shell adjacent its top and having a portion thereof extending through said casing in heat shielding relation to said liquefied gas conveying means, said conduit being of suflicient cross sectional area to provide a free vent for vapors forming within the inner shell above the liquefied gas contained therein, and means for insulating said casing from said conduit and said liquefied gas conveying means.
2. An insulated contained for storing liquefied gas, comprising inner and outer spaced apart metallic shells insulated one from the other, means communicating with the inner shell adjacent its bottom for conveying liquefied gas into and from said shell, a casing having fluid tight connection to the outer shell, extending an appreciable distance from such connection and surrounding and spaced from said liquefied gas conveying means, a vent gas conduit communicating with the interior of the inner shell adjacent its top and having a portion thereof extending through said casing in heat shielding relation to said liquefied gas conveying means, said conduit being of suificient cross sectional area to provide a free vent for vapors forming within the inner shell above the liquefied gas contained therein, valve means within the inner shell for controlling said liquefied gas conveying means. and means operable from the exterior of the container for opening and closing said valve means.
3. An insulated container for storing liquefied gas, comprising inner and outer spaced apart metallic shells with insulating material therebetween, a metallic boot-like casing having fluid tight connection to the lower part of the outer shell and extending an appreciable distance from such connection, a pipe serving as a liquefied gas inlet and outlet, having an orifice within the inner shell adjacent its bottom and extending from such orifice into andthrough said casing, a vent gas conduit extending from near the top of the inner shell through an opening in the outer shell and through said casing in heat shielding relation to said pipe, insulation between said casing and said conduit, means operable from the exterior of the container for opening and closing said orifice, and means within said casing for flexibly supporting said conduit.
4. An insulated container for storing liquefied gas, comprising inner and outer spaced apart metallic shells with heat insulating material therebetween, a pipe serving as a liquefied gas inlet and outlet pipe, a vent gas conduit within the inner shell extending above the liquefied gas level, secured within an opening in the bot.- tom of such shell and substantially paralleling said pipe where the latter passes through said insulating material, means in said conduit and pipe for compensating for movement thereof due to temperature changes, and means providing a support for the upper portion of said conduit and which includes a, sliding joint.
5. An insulated container for storing liquefied gas, comprising inner and outer spaced apart me- P tallic shells, insulation between such shells. a
liquefied gas pipe having an orifice within and near the bottom of the inner shell and extending outwardly beyond the container, a vent gas discharge conduit having its inlet adjacent the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells with a portion thereof arranged in heat shielding relation to said liquefied gas pipe.
6. A container for storing liquefied gas, comprising inner and outer spaced apart metallic shells, heat insulating material between said shells, a liquefied gas pipe having an orifice within and near the bottom of the inner shell, a vent gas discharge conduit having its inlet adjacent the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells and then laterally beneath the container with part thereof arranged in heat shielding relation to said liquefied gas pipe and a casing having fluid tight connection with the lower portion of said outer shell and extending an appreciable distance from such connection and surrounding said vent gas conduit and said D D 7. A container for storing liquefied gas, comprising inner and outer spaced apart metallic shells, heat insulating material within the space between said shells, a liquefied gas pipe having an orifice within and near the bottom of the inner shell, a vent gas discharge conduit having an inlet near the top of the inner shell, extending downwardly through the bottoms of the inner and outer shells and having'part thereof arranged in heat shielding relation to said pipe, a valve controlling the flow of liquefied gas through said orifice, and means operable from the exterior of the container for controlling said valve.
8. An insulated container for storing liquefied gas, comprising inner and outer spaced apart metallic shells insulated one from the other, a liquefied gas conduit having a valve controlled orifice within and near the bottom orthe inner shell and extending outwardly beyond the container, a vent gas discharge conduit having its inlet near the top oi the inner shell and extending downwardly and outwardly through the inner and outer shells and beyond the container and having a portion thereof arranged in heat shielding relation to said liquefied: gas conduit, and a liquefied gas outlet pipe connected to said liquefied gas conduit.
9. A container for storing liquefied gas, comprising inner and outer spaced apart metallic shells, heat insulating material within the space between said shells, a vent gas discharge conduit having its inlet near the top of the inner shell and extending downwardly through the bottoms of the inner and outer shells. and a cylindrical member attachedto the upper portion of the inner shell and surrounding the upper end of said conduit, the upper end oi said conduit having a sliding fit with said cylindrical member.
10. A'reservoir for storing liquefied natural gas, comprising inner and outer metallic shells, heat insulating material within the space between such shells, a. vent gas discharge conduit having its inlet near the top of the inner shell to about chromium and from about 10% to about 26% nickel; the inner shell having attached to .one 01 its surfaces and straddling the Joints between its adjacent plate sections, metallic strap-like members formed to provide pockets for said weld metal, and protective members of non-combustible material located between the insulating material and the strap-like members attached to the lower portion of such shell; such protective members being held in place by such insulating material,
13. A structure according to claim 2 in which the means for opening and closing said valve means is insulated from the inner shell.
14. A structure according to claim 1, in which the inner and outer shells are substantially spherical.
15. A structure according to claim 1, in which the inner and outer shells are in the form 01' ellipsoids.
16. A structure according to claim 1, in which the inner and outer shells are in the form of ellipsoids with flattened bottoms.
17. A structure according to claim 1, in which 5 the vent gas discharge conduit extends vertically within the inner shell and terminates near the top thereof.
18. A structure according to claim 1, in which the vent gas conduit extends vertically within and extending downwardly and outwardly 39 the inner shell and includes a sliding joint to through and beyond such shells, and a branch conduit connecting with said gas conduit outside of the reservoir and extending above the same; said branch conduit being provided with provide for expansion and contraction of such inner shell.
19. A structure according to claim 1, in which the inner and outer shells are substantially a check valve constructed to permit escape 01 gas spherical and the vent gas conduit extends verwhen excessive evaporation occurs within the inner shell.
11. A structure according to claim 1 in which the inner and outer shells are substantially spherical, the casing is at its lower polar region and the vent gas conduit extends vertically above said polar region.
12. An insulated container for storing liquefied gas, comprising inner and outer spaced apart metallic shells, insulating material arranged in the space between said shells; the innor shell being fabricated from sections or steel alloy plate containing from-about 2% to about 10% nickel; said plate sections being joined togetherby weld metal containing from about 15% mchanges.
inner shell above the lower shell and terminates near tically within the polar region of such the top or such shell.
20. A structure according to claim 1 in which secured to the outer shell 40 the casing surrounding the outwardly extending portions of the conduit and pipe has its outer end, closed and hermetically sealed to the vent gas conduit.
21. A structure according to claim 1, in which the outwardly extending portions of the vent gas conduit and the liquefied gas conveying means are provided with means for compensating for changes in their lengths due to temperature JAIMES O. JACKSON.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US42601242 US2386958A (en) | 1942-01-08 | 1942-01-08 | Spherical type insulated container for liquefied gases |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US42601242 US2386958A (en) | 1942-01-08 | 1942-01-08 | Spherical type insulated container for liquefied gases |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2386958A true US2386958A (en) | 1945-10-16 |
Family
ID=23688919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US42601242 Expired - Lifetime US2386958A (en) | 1942-01-08 | 1942-01-08 | Spherical type insulated container for liquefied gases |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2386958A (en) |
Cited By (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2451486A (en) * | 1944-09-01 | 1948-10-19 | Chicago Bridge & Iron Co | Vacuum tank for storing liquids at high or low temperatures |
| US2481664A (en) * | 1945-03-19 | 1949-09-13 | Joseph L Hemp | Insulated container |
| US2562601A (en) * | 1942-07-03 | 1951-07-31 | Dubois | Tanks adapted to contain liquids or gases |
| US2581571A (en) * | 1945-10-24 | 1952-01-08 | Westinghouse Electric Corp | Circuit interrupter |
| US2668634A (en) * | 1950-02-23 | 1954-02-09 | Chicago Bridge & Iron Co | Spherical segment tank and method of making same |
| US2751755A (en) * | 1954-05-14 | 1956-06-26 | Superior Tank & Construction C | Pressure tank |
| US2777295A (en) * | 1952-09-12 | 1957-01-15 | Union Carbide & Carbon Corp | Concrete reservoir for liquefied gases |
| DE1041512B (en) * | 1956-01-13 | 1958-10-23 | Knapsack Ag | Storage of a lying container for cryogenic liquids |
| US2961118A (en) * | 1958-10-02 | 1960-11-22 | Chicago Bridge & Iron Co | Elevated storage tank |
| US2963874A (en) * | 1957-08-05 | 1960-12-13 | Columbia Southern Chem Corp | Method of and means for storing chlorine |
| US3074586A (en) * | 1958-10-30 | 1963-01-22 | Liquefreeze Company Inc | Shipper container |
| US3122000A (en) * | 1962-03-30 | 1964-02-25 | Paul J Sirocky | Apparatus for transferring cryogenic liquids |
| US3302814A (en) * | 1963-09-16 | 1967-02-07 | Martin Marietta Corp | Fluid core joint |
| DE1261008B (en) * | 1961-03-21 | 1968-02-08 | Conch Int Methane Ltd | Tanker for the transport of cryogenic liquids at atmospheric pressure |
| DE1281291B (en) * | 1964-08-10 | 1968-10-24 | Conch Int Methane Ltd | Pipeline connection to a membrane liquid gas container of a tanker |
| US3435983A (en) * | 1965-07-13 | 1969-04-01 | Conch Int Methane Ltd | Tank keyway and weld tester |
| US3595424A (en) * | 1969-02-24 | 1971-07-27 | Conch Int Methane Ltd | Containers for liquefied gases |
| JPS4874611A (en) * | 1972-01-03 | 1973-10-08 | ||
| US3927497A (en) * | 1972-11-15 | 1975-12-23 | Hitachi Ltd | Supporting structure of pressure vessel |
| US4106423A (en) * | 1976-10-28 | 1978-08-15 | General Dynamics Corporation | Weather covers for tankers |
| US4145892A (en) * | 1977-07-29 | 1979-03-27 | Gosudarstvenny Proektno-Konstruktorsky Institut Po Proektirovaniju Tekhnologii Montazha Legkoi I Pischevoi Promyshlennosti | Liquid storage reservoir |
| WO2000045085A1 (en) * | 1999-01-29 | 2000-08-03 | Phillips Petroleum Company | Bottom entry pumping system with tertiary containment |
| US20050061222A1 (en) * | 2003-09-24 | 2005-03-24 | Miyazaki Satoshi | Tank covers and ships |
| US20080078771A1 (en) * | 2006-09-28 | 2008-04-03 | Nichias Corporation | Insulated container and method of manufacturing the same |
| US20080283123A1 (en) * | 2005-09-15 | 2008-11-20 | Manbas Alpha Ab | Pressure Controlled Gas Storage |
| RU180823U1 (en) * | 2017-10-24 | 2018-06-25 | Общество с ограниченной ответственностью "Научно-технический комплекс "Криогенная техника" | RESERVOIR WITH COMPENSATION OF SEATING OF VACUUM PERLITE HEAT INSULATION |
| US11022253B2 (en) * | 2016-05-16 | 2021-06-01 | Mitsubishi Shipbuilding Co., Ltd. | Liquefied gas-based rapid cooling possibility determination device, liquefied gas storage tank, liquefied gas carrying vessel, and liquefied gas-based rapid cooling possibility determination method |
| WO2022235946A1 (en) * | 2021-05-05 | 2022-11-10 | Cb&I Sts Delaware Llc | Large-scale vacuum insulated cryogenic storage |
| EP4174360A4 (en) * | 2020-06-26 | 2024-03-20 | Kawasaki Jukogyo Kabushiki Kaisha | DOUBLE HULL TANK |
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1942
- 1942-01-08 US US42601242 patent/US2386958A/en not_active Expired - Lifetime
Cited By (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2562601A (en) * | 1942-07-03 | 1951-07-31 | Dubois | Tanks adapted to contain liquids or gases |
| US2451486A (en) * | 1944-09-01 | 1948-10-19 | Chicago Bridge & Iron Co | Vacuum tank for storing liquids at high or low temperatures |
| US2481664A (en) * | 1945-03-19 | 1949-09-13 | Joseph L Hemp | Insulated container |
| US2581571A (en) * | 1945-10-24 | 1952-01-08 | Westinghouse Electric Corp | Circuit interrupter |
| US2668634A (en) * | 1950-02-23 | 1954-02-09 | Chicago Bridge & Iron Co | Spherical segment tank and method of making same |
| US2777295A (en) * | 1952-09-12 | 1957-01-15 | Union Carbide & Carbon Corp | Concrete reservoir for liquefied gases |
| US2751755A (en) * | 1954-05-14 | 1956-06-26 | Superior Tank & Construction C | Pressure tank |
| DE1041512B (en) * | 1956-01-13 | 1958-10-23 | Knapsack Ag | Storage of a lying container for cryogenic liquids |
| US2963874A (en) * | 1957-08-05 | 1960-12-13 | Columbia Southern Chem Corp | Method of and means for storing chlorine |
| US2961118A (en) * | 1958-10-02 | 1960-11-22 | Chicago Bridge & Iron Co | Elevated storage tank |
| US3074586A (en) * | 1958-10-30 | 1963-01-22 | Liquefreeze Company Inc | Shipper container |
| DE1261008B (en) * | 1961-03-21 | 1968-02-08 | Conch Int Methane Ltd | Tanker for the transport of cryogenic liquids at atmospheric pressure |
| US3122000A (en) * | 1962-03-30 | 1964-02-25 | Paul J Sirocky | Apparatus for transferring cryogenic liquids |
| US3302814A (en) * | 1963-09-16 | 1967-02-07 | Martin Marietta Corp | Fluid core joint |
| DE1281291B (en) * | 1964-08-10 | 1968-10-24 | Conch Int Methane Ltd | Pipeline connection to a membrane liquid gas container of a tanker |
| US3435983A (en) * | 1965-07-13 | 1969-04-01 | Conch Int Methane Ltd | Tank keyway and weld tester |
| US3595424A (en) * | 1969-02-24 | 1971-07-27 | Conch Int Methane Ltd | Containers for liquefied gases |
| JPS4874611A (en) * | 1972-01-03 | 1973-10-08 | ||
| US3927497A (en) * | 1972-11-15 | 1975-12-23 | Hitachi Ltd | Supporting structure of pressure vessel |
| US4106423A (en) * | 1976-10-28 | 1978-08-15 | General Dynamics Corporation | Weather covers for tankers |
| US4145892A (en) * | 1977-07-29 | 1979-03-27 | Gosudarstvenny Proektno-Konstruktorsky Institut Po Proektirovaniju Tekhnologii Montazha Legkoi I Pischevoi Promyshlennosti | Liquid storage reservoir |
| WO2000045085A1 (en) * | 1999-01-29 | 2000-08-03 | Phillips Petroleum Company | Bottom entry pumping system with tertiary containment |
| US6286320B1 (en) | 1999-01-29 | 2001-09-11 | Phillips Petroleum Company | Bottom entry pumping system with tertiary containment |
| AU768752B2 (en) * | 1999-01-29 | 2004-01-08 | Conocophillips Company | Bottom entry pumping system with tertiary containment |
| US7520232B2 (en) * | 2003-09-24 | 2009-04-21 | Mitsubishi Heavy Industries, Ltd. | Tank covers and ships |
| US20050061222A1 (en) * | 2003-09-24 | 2005-03-24 | Miyazaki Satoshi | Tank covers and ships |
| US20080283123A1 (en) * | 2005-09-15 | 2008-11-20 | Manbas Alpha Ab | Pressure Controlled Gas Storage |
| US8327865B2 (en) * | 2005-09-15 | 2012-12-11 | Manbas Alpha Ab | Pressure controlled gas storage |
| US20080078771A1 (en) * | 2006-09-28 | 2008-04-03 | Nichias Corporation | Insulated container and method of manufacturing the same |
| US11022253B2 (en) * | 2016-05-16 | 2021-06-01 | Mitsubishi Shipbuilding Co., Ltd. | Liquefied gas-based rapid cooling possibility determination device, liquefied gas storage tank, liquefied gas carrying vessel, and liquefied gas-based rapid cooling possibility determination method |
| RU180823U1 (en) * | 2017-10-24 | 2018-06-25 | Общество с ограниченной ответственностью "Научно-технический комплекс "Криогенная техника" | RESERVOIR WITH COMPENSATION OF SEATING OF VACUUM PERLITE HEAT INSULATION |
| EP4174360A4 (en) * | 2020-06-26 | 2024-03-20 | Kawasaki Jukogyo Kabushiki Kaisha | DOUBLE HULL TANK |
| WO2022235946A1 (en) * | 2021-05-05 | 2022-11-10 | Cb&I Sts Delaware Llc | Large-scale vacuum insulated cryogenic storage |
| US11898703B2 (en) | 2021-05-05 | 2024-02-13 | CB&I STS Delaware LLC. | Large-scale vacuum insulated cryogenic storage |
| CN117642572A (en) * | 2021-05-05 | 2024-03-01 | 西比埃Sts特拉华有限责任公司 | Large-scale vacuum insulated cryogenic storage parts |
| JP2024519740A (en) * | 2021-05-05 | 2024-05-21 | シービーアンドアイ エスティーエス デラウェア エルエルシー | Large-scale vacuum insulated cryogenic storage |
| AU2022269650B2 (en) * | 2021-05-05 | 2025-10-16 | Cb&I Sts Delaware Llc | Large-scale vacuum insulated cryogenic storage |
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