US1651521A - Method and apparatus for the storage and the transportation of gas - Google Patents

Method and apparatus for the storage and the transportation of gas Download PDF

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Publication number
US1651521A
US1651521A US86529A US8652926A US1651521A US 1651521 A US1651521 A US 1651521A US 86529 A US86529 A US 86529A US 8652926 A US8652926 A US 8652926A US 1651521 A US1651521 A US 1651521A
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United States
Prior art keywords
wire
gas
metal
envelope
stress
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US86529A
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English (en)
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Lucas-Girardville Paul Nicolas
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/04—Protecting sheathings
    • F17C1/06—Protecting sheathings built-up from wound-on bands or filamentary material, e.g. wires
    • 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
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
    • 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
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0123—Shape cylindrical with variable thickness or diameter
    • 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
    • F17C2201/056—Small (<1 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
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0604—Liners
    • 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
    • F17C2203/0614—Single wall
    • F17C2203/0619—Single wall with two layers
    • 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
    • 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
    • F17C2203/0656—Metals in form of filaments
    • 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
    • F17C2205/0388—Arrangement of valves, regulators, filters
    • F17C2205/0394—Arrangement of valves, regulators, filters in direct contact with the pressure vessel
    • 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
    • F17C2223/0107—Single phase
    • F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
    • 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
    • F17C2223/036—Very high pressure (>80 bar)
    • 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
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/043—Pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/011—Improving strength
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/07—Applications for household use
    • F17C2270/0745—Gas bottles

Definitions

  • I substitute for the usual thick and heavycontainers, a vessel with relatively thin and light walls, with the addition of means whereby the device is strengthened and protected against bursting.
  • M first means of rotection consist'in the; apphcation about sai walls ofsuitable hoopj ing which has-a great, tensile strength and consists of strong steel wire, -'known per se.
  • This method of reinforcement has already been employed ,in. artillery practice, but when the question relates to light weight containers 1t becomes necessary to employ special arrangements and to take suitable precautions.
  • wirehooping is wound upon the metal cylinder under a-certain. pressure and tenslon.
  • 1 is a diagrammatic view illustrating a cross section of one embodiment of the. in-
  • Fig. 2 is a viewsimilar to Fig; 1 but show- If a plain cylinder of thinmetal. were used, the winding would necessarily'be-- so loose to avoid crushing the cylinder, that,
  • Fig. 3 is a diagrammatic view illustrating a longitudinal section-of a receptacle embodying the-present invention.
  • Fig. 4 is a View illustratingin-a different manner the container shown "in Fig. 3.
  • Fig. v5 is a view illustrating the crossing of two corrugations. .7 I Fig. 6 i a' view illustrating the effect as to different stresses of arranging the corrugationsoblique to the generatrices of the 'cyllndrical part of the vessel or receptacle.
  • Fig. 7. is a view in elevation of a receiver corrugated helically.-
  • Fig. 8 isa view illustrating for strengthening a container.
  • Fig. .9 is a-view of a container reinforced by the means shown in Fig.8, partof the reinforcing means being bro-ken away to show the underlying structure; and
  • Fig. 10 is a i w illustrating internal reinforcing means for the thinmetal cylinder?
  • the sheet metal is corrugated lengthwise of the cylinder 1 and is enclosed and compressedby. tightly wound wire 2 which in the cross-sectional view'of this figure appears as acircle in which the section of the corrugated metal is inscribed.
  • the pressure maybe increased until the sheet metal, which expands as well as. the wire, attains atension' stress compatible with its trength.
  • I suitably regulate the length and depth of the corrugations so thatthe sheet metal as well as the wire will be subjected to the proper stresses. I may even bring the stress exclusively upon the wire, so that the sheet metal part now serves solely as a con-" tainernf
  • the dimensions of the corrugations may be .so calculated.
  • the sheet sheet metal may enter into substantially com-' jplete contact with the wire, which is wound metal will burst in the events of an increased stress upon it, and before the wires have reached the breaking point.
  • the relative disposition of the wire and the corrugations of the metal should be such that the vessel may resume its normal shape when the tension which expanded it ceases.
  • the wire will contract and will thus compress the sheet metal, so that the metal must be guided in a certain measure in order that it may return to its-initial corrugated form.
  • I may employ suitable wires 3 laced in the lengthwise direction, one such wire being disposed in each outwardly facing trough 4 of said longitudinal corrugations.
  • the diameter of the wire must be less than the de th of the recess ortrough presented by tie corrugation.
  • Additional longitudinal wires 5 may be used in the manner indicated in Imay further employ transverse corrugations 6 in the metal as shown in Fig. 3 to impart greater circumferential stillness. In this event, the hooping may be wound under agreater tension. It will be evident that the circumferential rigidity of the cylinder depends upon the depth of the transverse corrugations.
  • the top and bottomof the vessel will preferably consist of hemispherical members or caps 7 of pressed steel. Between these end caps there is stretched a set of wires under tensile stress, and I further employ suitable means for connectin the said vessel with the apparatus in which the gas is used. To the central part of each end is fastened, as by welding,
  • a. member preferably of solid steel, in which is formed av tapped hole for the insertion of all such devices as expansion valves, pressure gauges, safety valves, or the like. 7
  • corrugations 10 oblique to the generatrices 11-11 of 'the cylindrical part of the vessel (see Figs. 6 and 7).
  • the corrugations may be considered as substantially straight.
  • a be the angle between the corrugations and the said generatrices; the stress due to the expansion of the sheet metal which acts directly across or perpendicular to the corrugations will have two components, one in the direction of the generatrlces and the other at right angles'thereto. If i is given a value near 26 degrees the other acute angle of the right triangle will be near 64 degrees, and consequently the second component will have about twice the value of the first. In these conditions, such lengthwise stress on the sheet metal is one-half the stress due to the resistance to the expansion of the cylindrical part. Internal pressure tends to exert tension on the sheet metal itselfbut before such action can take place directl the corrugations must be drawn'out. Suci expansion would act directly at right angles to the corrugations and the stress in this direction may be resolved into its components as described above.
  • each hoop of one set has the opening of the U turned outwardly and each hoop '16 of the other has" the opening of the U turned inwardly, the two sets of hoops being connected together at their flanged" ed es.
  • This arrangement offers the .crease their strength by the use strength w ich is required both in the longi tudinal and the transverse d1rect1ons, so as to prevent the rupture of the cylindrical body-as well as the tearing off of the end parts.
  • the cylinder 17 may have outwardly projecting, annular corrugations 18.
  • the said hoops may further beconnected' lto tension elements'which 'assure the perma nent contact between the attaching points of the wires of the longitudinal sets and the conical sets, and the sheet metalof the cylindrical part, in spite of the circumferential expansion of the cylindricalfpart whenthe" vessel is subjected topressur'eI-
  • This result maybe obtained use of another "form of the in- 'ich is: necessarily much less than thatofpthe wire.
  • absorbents W1 1 in tact permit of disposing of a much ater volume of at a stated pressure in a given space t an if the gas were simply compressed in a vessel of sufiicient strength.
  • the wei ht of the vessels arranged in accordance wi said method will be reduced from lrgs. to some 2.5 kgs. per cubic meter of gas contained therein the volume of the gas bain measured at the atmospheric ressure.
  • a container adapted to sustain heavy internal pressure comprising a relatively light and expansible envelope having inwardly projectin corru ations extending from end to end thereo wire extending from end to end of the envelope and having portions lyin in said corrugations, and an external rein orcement of wire so arranged around said envelope as to sustain the principal part of the stress due to the internal pressure as the envelope expands and approaches a circular cross section.
  • a container adapted to sustain heavy internal pressure comprising an expansible cylindrical envelope of sheet metal with corrugations extending from end to end thereof, and a hooping of wire extending around said corru ations and adapted to sue; tain theprincipa part of the stress dueto the internal pressure as the envelope expands.
  • a container adapted to sustain heavy intern l pressure comprising an] expansible the gas thus compressed, are
  • corrugated envelope having inwardly concave ends, wire arrangedtransversely around said envelope, and wire arranged externally and longitudinally of said envelope to hold said ends together and to cooperate with said transversely arranged wire in sustaining the principal part of the stress due to the internal pressure as said envelope expands.
  • a container adapted to sustain heavy internal pressure comprising an expansible longitudinally corrugated cylindrical envelo cap portions at the ends of said enve ope, wire extendin from cap to cap and having portions lying in the external troughs of said corrugations, and wire arranged transversely around said envelope and cooperating with said longitudinally arranged wire to sustain the principal part of the stress as the envelope expands due to internal pressure.
  • a container adapted to sustain heavy internal pressure comprising a relatively light and expansible envelope of corrugated sheet metal having closed ends, said envelope having a peripheral corrugation or trough adjacent each end, and external reinforcing means of wire so arranged around said envelo as to sustain the principal part of the longltudinal and peripheral stresses as the envelope expands due to internal pressure.
  • a container adapted to sustain heavy internal pressure comprising an expansible cylindrical enveio e of corrugated sheet metal having close ends, and transverse wire hoopin resistin the lon itudinal pressure on sai ends an outwar pressure on said envelope as the latter expands, said wire hooping comprising wire of U-sha ed cross section and the direction of the -shaped sections being alternately outward and. inward and successive loops of wire being lockedtogether in this manner.
  • a container adapted to sustain heavy internal pressure comprising an expansible longitudinally corrugated envelope of thin metal having closed ends, an outer reinforcementof wire to sustain the greatervpart of the stress as the envelope expands under ressure, and an inner bracing comprising ight hoops and wire connecting the hoops together and connected to the ends to prevent collapse ofthe cylinder.
  • a container adapted to sustain heavy internal pressure colnprisin an expansible cylindrical envelope of tiiin. corrugated metal, caps attached to said -envclope at its ends, an outer reinforcement of wire to sustain the greater part ofthe stress as the envelo expands under pressure, a longitudinal inner wire connected at its ends to the caps, and inner bracin comprising light hoops, wire connecting toggle meane to expand one of said oops, and connections between said toggle means and said longitudinal inner wire to operate e hoops to ether,

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
  • Wire Processing (AREA)
US86529A 1925-05-20 1926-02-06 Method and apparatus for the storage and the transportation of gas Expired - Lifetime US1651521A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR476459X 1925-05-20

Publications (1)

Publication Number Publication Date
US1651521A true US1651521A (en) 1927-12-06

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US86529A Expired - Lifetime US1651521A (en) 1925-05-20 1926-02-06 Method and apparatus for the storage and the transportation of gas

Country Status (5)

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US (1) US1651521A (fr)
BE (1) BE332293A (fr)
DE (1) DE476459C (fr)
FR (1) FR611097A (fr)
GB (1) GB252386A (fr)

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2460368A (en) * 1947-08-30 1949-02-01 Technical Coatings Inc Vent construction for airplane fuel tanks
US2480369A (en) * 1941-11-07 1949-08-30 Smith Corp A O Manufacture of multilayer cylinder for high-pressure vessels
US2507778A (en) * 1945-11-27 1950-05-16 Phillips Petroleum Co Pressure vessel
US2579183A (en) * 1943-06-29 1951-12-18 Freysainet Eugene Method for tensioning reinforcements
US2633414A (en) * 1947-06-16 1953-03-31 Pechiney Prod Chimiques Sa Protective liner for autoclaves
US2837456A (en) * 1952-02-29 1958-06-03 Kellogg M W Co Filament wound container
US3047191A (en) * 1957-11-26 1962-07-31 Hercules Powder Co Ltd Filament wound vessels and methods for forming same
US3074584A (en) * 1959-05-20 1963-01-22 Dorr Oliver Inc Pressure vessel
US3335902A (en) * 1964-12-28 1967-08-15 Continental Can Co Superimposed axial-circumferential beading of cans
US3446385A (en) * 1966-08-05 1969-05-27 Koppers Co Inc Filament wound reinforced pressure vessel
US5556601A (en) * 1990-11-19 1996-09-17 Institut Francais Du Petrole Process of manufacturing a tank of low unitary weight notably usable for stocking fluids under pressure
US5659941A (en) * 1991-02-01 1997-08-26 Institut Francais Du Petrole Process for manufacturing a light structure through the expansion of a metallic tank in an armored corrugated pipe
US20050006394A1 (en) * 2003-06-12 2005-01-13 Kazuo Fujihara High-pressure gas container
US20090152278A1 (en) * 2007-12-14 2009-06-18 Markus Lindner Inner shell for a pressure vessel
US20100230417A1 (en) * 2007-10-31 2010-09-16 Gastank Sweden Ab Vessel for a compressed gas and method for producing the vessel
US8316905B2 (en) 2004-02-18 2012-11-27 Avure Technologies Ab Press and a method for manufacturing a press
US8561829B1 (en) * 2009-10-23 2013-10-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Composite pressure vessel including crack arresting barrier
US20150114970A1 (en) * 2008-03-03 2015-04-30 Samsung Heavy Ind. Co., Ltd. Reinforcing member for corrugated membrane of lng cargo tank, membrane assembly having the reinforcing member and method for contructing the same
CN105443973A (zh) * 2015-11-09 2016-03-30 大连理工大学 薄壁金属内衬纤维复合材料缠绕压力容器及其制造工艺
US9618160B2 (en) 2009-02-06 2017-04-11 Hexagon Technology As Pressure vessel longitudinal vents
US10088110B2 (en) 2016-05-17 2018-10-02 Hexagon Technology As Pressure vessel liner venting via nanotextured surface
US20190049068A1 (en) * 2017-08-10 2019-02-14 Toyota Jidosha Kabushiki Kaisha High-pressure container and shell reinforcing layer wrapping method
US10544901B2 (en) 2016-04-06 2020-01-28 Hexagon Technology As Pressure vessel vented boss with sintered metal plug
US10627048B2 (en) 2015-12-16 2020-04-21 Hexagon Technology, As Pressure vessel dome vents
US11092285B2 (en) * 2019-09-17 2021-08-17 Genesis Io, Llc Pressurized gas container and process
US20230035247A1 (en) * 2021-07-27 2023-02-02 Airbus Operations S.L.U. Hydrogen tank for aircraft
US20230092930A1 (en) * 2021-07-08 2023-03-23 Mengjun WANG Carbon-fibre composite high-pressure hydrogen storage tank and manufacturing process thereof
US12135111B2 (en) * 2021-07-27 2024-11-05 Airbus Operations S.L.U. Hydrogen tank for aircraft

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE910897C (de) * 1939-12-15 1954-05-06 Basf Ag Hochdruckgefaess
DE827657C (de) * 1950-11-05 1952-01-10 Jur Max Wolf Dr Ing Dr Hochdruckbehaelter
DE1160455B (de) * 1956-07-27 1964-01-02 Csepel Vas Es Femmuevek Gewickelter Hochdruck-Gasbehaelter
DE102017222452A1 (de) * 2017-12-12 2019-06-13 Robert Bosch Gmbh Behälter

Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2480369A (en) * 1941-11-07 1949-08-30 Smith Corp A O Manufacture of multilayer cylinder for high-pressure vessels
US2579183A (en) * 1943-06-29 1951-12-18 Freysainet Eugene Method for tensioning reinforcements
US2507778A (en) * 1945-11-27 1950-05-16 Phillips Petroleum Co Pressure vessel
US2633414A (en) * 1947-06-16 1953-03-31 Pechiney Prod Chimiques Sa Protective liner for autoclaves
US2460368A (en) * 1947-08-30 1949-02-01 Technical Coatings Inc Vent construction for airplane fuel tanks
US2837456A (en) * 1952-02-29 1958-06-03 Kellogg M W Co Filament wound container
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Also Published As

Publication number Publication date
GB252386A (en) 1926-11-18
BE332293A (fr)
FR611097A (fr) 1926-09-20
DE476459C (de) 1929-05-17

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