WO2010072400A1 - Réservoir sous pression pour un agencement de réservoir de transport - Google Patents

Réservoir sous pression pour un agencement de réservoir de transport Download PDF

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Publication number
WO2010072400A1
WO2010072400A1 PCT/EP2009/009203 EP2009009203W WO2010072400A1 WO 2010072400 A1 WO2010072400 A1 WO 2010072400A1 EP 2009009203 W EP2009009203 W EP 2009009203W WO 2010072400 A1 WO2010072400 A1 WO 2010072400A1
Authority
WO
WIPO (PCT)
Prior art keywords
shell
pressure vessel
region
shells
bead
Prior art date
Application number
PCT/EP2009/009203
Other languages
German (de)
English (en)
Inventor
Rainer Metz
Original Assignee
WEW Westerwälder Eisenwerk GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by WEW Westerwälder Eisenwerk GmbH filed Critical WEW Westerwälder Eisenwerk GmbH
Priority to EP09799281A priority Critical patent/EP2238383B1/fr
Priority to ES09799281T priority patent/ES2375445T3/es
Priority to CA2716895A priority patent/CA2716895C/fr
Priority to PL09799281T priority patent/PL2238383T3/pl
Priority to AT09799281T priority patent/ATE529686T1/de
Priority to US12/937,342 priority patent/US20110031257A1/en
Priority to DK09799281.2T priority patent/DK2238383T3/da
Priority to JP2011541232A priority patent/JP5311520B2/ja
Publication of WO2010072400A1 publication Critical patent/WO2010072400A1/fr
Priority to ZA2010/06017A priority patent/ZA201006017B/en

Links

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
    • F17C1/08—Integral reinforcements, 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
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0147—Shape complex
    • F17C2201/0152—Lobes
    • 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
    • F17C2201/0147—Shape complex
    • F17C2201/0166—Shape complex divided in several chambers
    • 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
    • F17C2201/0147—Shape complex
    • F17C2201/0171—Shape complex comprising a communication hole between chambers
    • 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
    • F17C2201/03—Orientation
    • F17C2201/035—Orientation with substantially horizontal main axis
    • 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
    • F17C2203/0612—Wall structures
    • F17C2203/0614—Single wall
    • F17C2203/0617—Single wall with one layer
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/221—Welding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/011—Improving strength
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/018—Adapting dimensions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0165—Applications for fluid transport or storage on the road
    • F17C2270/0168—Applications for fluid transport or storage on the road by vehicles

Definitions

  • the present invention relates to a pressure vessel with a parallel, a longitudinally extending bead defining, juxtaposed part cylindrical shell shells shell constructed, whose front ends are each closed with a curved bottom.
  • Pressure vessel with part-circular cylindrical shell shells whose cross-section is reminiscent of a recumbent eight, are known for example from DE-A-36 06 247, DE-A-31 25 963 of DE-A-29 51 554 and EP-A 1 326.
  • Such pressure vessels are particularly suitable for road vehicle transport containers, such as tanker semi-trailers or for tank container arrangements, in which containers are required to exploit a space with reduced height particularly effective and at the same time ensure low pressure, weight-saving material use high pressure resistance.
  • the partially cylindrical shells are, for example, attached to each other opposite to this wall and connected or welded to this.
  • a pressure vessel according to claim 1, wherein a shell element is provided, which connects the shell shells, and the tension element together.
  • This shell element then closes the bead area - at the top as a roof element and at the bottom as a bottom element - and forms with these elements or the enclosed areas a profile support structure in the gusset area, which additionally acts to stabilize both against internal and external pressure loads and against envelope loads.
  • the measure is used according to claim 2.
  • a gusset element according to claim 6 is advantageous; especially if it is with an outer contour area of the inner Circumferential contour of the arched bottom follows, so can be used in this, and has an inner contour region which projects inwardly beyond the bead region into the interior of the container, so that the end wall peripheral contour of the jacket shell always runs on the facing surface of the gusset element.
  • the coat formed from the shells with its front ends in each case to the open end of the curved bottoms, in which the corresponding gusset elements are inserted flush mounted are clean, without requiring additional passport or notching would be required.
  • the contour regions meet at an acute angle in the crest or sole regions of the shell shells and there provide a pressure-technically advantageous reinforcement, which absorbs the stress peaks present there, caused by the internal pressure of the container.
  • the reinforcement is further improved and the stress peaks are further degraded, if at the ends of the gusset elements respectively rib-like extensions are provided which go beyond the common peripheral contour of the bottom and shell shell substantially following the apex or sole region, in which the voltage spike occur.
  • the shell shells on differently curved peripheral portions.
  • the depth of the bead which is formed at the interface between the longitudinally extending part-cylindrical shell shells, reduce and thus increase the useful volume of the pressure vessel, without the compressive strength would be substantially reduced.
  • the curvatures in the upper and lower bead area can vary from each other. That is, the bead depth is different at the bottom of the tank than at the top. A stronger curvature - narrower radius - leads to a lower bead and a lower curvature - larger radius - to a shallower bead. A flatter bead in the lower area, for example, for the complete emptying of the adjacent Sole areas of the individual shell shells be helpful. A deeper bead, however, gives such a pressure vessel in this area a higher dimensional stability, so that it can be stored, for example, along the tank soles extending saddle profiles - for example, the side members of a semitrailer or the loading skids for a hook lift system.
  • Claim 10 relates to a transport container assembly which is provided with a pressure vessel according to the invention.
  • FIG. 1 shows a perspective view of a pressure vessel according to the invention
  • Figure 2 is a perspective cross-sectional view (section A-A) of the pressure vessel from
  • FIG. 1 A first figure.
  • FIG. 3 shows a perspective longitudinal sectional view (section B-B) of the pressure vessel shown in FIG. 1,
  • FIG. 4 shows a perspective view of the pressure vessel from FIG. 1, in which a forehead bottom has been omitted
  • FIG. 5 shows a perspective view of the container shown in FIG. 4 without the gusset plates
  • Figure 6 is a perspective view of a center wall with inclined
  • Figure 7 shows the view of an alternative gusset element in two
  • Figure 8 is a schematic representation of two alternative cross-sectional embodiments of the cylindrical tank section
  • FIG. 9 shows a tank container unit with a container according to the invention
  • FIG. 10 shows a double-cylindrical cross-section according to the prior art
  • FIG. 11 shows an elliptical (left half) and a kofferfbrmigen (right half) cross-section according to the prior art
  • Figure 12 is an oval cross-section according to the prior art.
  • the pressure vessel 1 shown in Figures 1 to 5 comprises two part-cylindrical shell shells 2, 4, which, as seen in Figures 2 and 5, are welded in the longitudinal direction with a trained as a flat wall 6 tension member.
  • the flat wall 6 has the same length as the part-cylindrical shell shells 2 and 4.
  • Each of the jacket shells 2, 4 comprises differently curved peripheral sections 2a, 2b, 2c and 4a, 4b, 4c, respectively.
  • the peripheral portions 2a and 4a extend from the seam with the flat wall 6 to the apex line 7 of the respective shell shells 2 and 4.
  • the peripheral portions 2b and 4b respectively extend to the lower sole lines 9 of the shell shells 2, 4, of which the peripheral portions 2c and 4c extend to the flat wall 6.
  • the peripheral portions 2b and 4b in the belt area have a radius of curvature of 600-1300 mm, while the upper and lower
  • Circumferential sections 2a, 2c and 4a, 4c have a radius of curvature of 600-3000 mm.
  • radius ranges are for tank containers or vehicles with a max. Width of 2600 mm specified. Other dimensions may result in correspondingly different radii ranges and ratios, which are then adapted to the actual external dimensions of the tank containers or vehicles (rail, truck).
  • the peripheral portions 2a and 4a form an upper bead portion 8 and the peripheral portions 2c and 4c have a lower bead portion 10.
  • the upper end 12 and the lower end 14 of the flat wall 6 protrude into the bead areas 8 and 10; the lower end 14 to the level defined by the sole lines 9 of the shells 2 and 4 and the upper end 12 beyond the plane defined by the crests 7 of the shells 2 and 4 level. Both ends 12 and 14 are provided for stabilization with a fold 12a and 14a.
  • the flat wall 6 is provided with a passage opening 50, which is reinforced with a collar 52.
  • the ends of the shell shells 2 and 4 are closed with curved bottoms 16 and 18 ( Figures 1 and 3), which in turn can be inserted via a connected thereto end ring 20 in a container frame 22 ( Figure 1 and 9).
  • each case gusset elements 24 and 26 which are arranged as flat sheets transverse to the longitudinal direction.
  • the lower gusset elements 26 are each provided with an outer contour region 28 (FIG. 4) which follows the straight inner peripheral contour section of the domed bottom 16 and 18 and extends between the two sole lines 9 of the partially cylindrical shell shells 2 and 4.
  • An inner contour region 30 runs within the circumferential contours of the circumferential sections 2c and 4c which define the bead region 10.
  • the outer contour region 28 and the inner contour regions 30 extend approximately at an acute angle to one another and meet in the ends 32 which lie in the region of the sole regions (sole lines 9).
  • the outer contour region 34 also follows the straight upper peripheral contour section of the bottoms 16 and 18 and extends with its inner
  • Inner contour regions 36 to the ends 38 which ends analogous to the lower gusset elements 26 in the apex areas (apex lines 7). While the lower gusset elements 26 is arranged completely within the bottom contour 1, the outer contour region 34 of the upper gusset element 24 protrudes beyond the bottom contour and extends outside thereof approximately at the same height as the fold 12a.
  • Fig. 6 shows an embodiment (tank shells 2, 4 not shown) in which gusset elements 24a, 26a are provided, which also extend transversely to the container but are inclined in the longitudinal direction. Such an execution allows it as a tension element Serving flat wall 6 to shorten areas and thus saving material and weight. At the upper out of the tank gusset element 24a of the outer contour region 34a is bent, which is so coupled to the fold 12a and the end 12 of the flat wall 6 (welded).
  • openings 40 are provided in the typical container connections such as manhole, filling connections, ventilation connections, safety valve connections are used (see Fig. 4).
  • an additional shell element 42 is provided, which is at least partially welded at its side edges 44 in the apex areas with the shell shells 2 and 4 and at its front ends 46 with the upper gusset elements 24.
  • the middle of the shell element 42 extends in the longitudinal direction of an edging 47, which comes to lie approximately on the fold 12a and is fixed on this via hole welds 48.
  • the peripheral portions 2a, 4a, the upper end 12 of the flat wall 6 with the fold 12a and the shell member 42 form a stabilizing longitudinal support unit which is closed at its ends by the upper gusset elements 24 and thus additionally stabilized.
  • the shell shells 2 and 4 surrounds in the illustrated embodiment ( Figure 1, 2 and 4) a double jacket 5, which ends in the upper region (about the maximum level) of the pressure vessel 1 and the sole areas 2b, 4c and thus also the lower bead area 10, running flat between the sole lines 9, completely encloses.
  • This double jacket 5 prevents damage to the shells 2 and 4, the escape of cargo. It can be supplemented by (not shown) additional outdoor floors, which then also form a double jacket in the region of the curved floors 16 and 18.
  • the double jacket 5 can also be connected to the folded edge 14a at the lower end 14 of the flat wall 6 for further stabilization via hole welds.
  • a similar fixation can also take place in the sole regions via intermediate layers (eg double sheets) inserted there on the outer side of the shell shells 2 and 4, so that here as well a stabilizing carrier element is realized in the lower bead region 10.
  • the double jacket 5 is omitted.
  • a flat, curved or beveled shell element can be arranged in the lower bead region 10, which then defines a similar support structure as the upper shell element 42.
  • the ends 32, 38 of the gusset elements 24 and 26 each extend in the sole or apex areas of the shell shells 2 and 4, which also form the transitions at the same time, where the straight peripheral portions of the plates 16 and 18 merges into the curved peripheral portions , This point is therefore particularly critical in terms of printing technology.
  • a rib-like extension 132a, 132b is shown in the exemplary embodiment according to FIG. 7, which follows the common circumferential contour of bottoms 16, 18 and shell shells 2, 4 beyond the apex lines 7.
  • the gusset element 24 is enlarged overall and projects with the region 132a over the left-hand crest line 7.
  • the gusset element 24 is enlarged overall and projects with the region 132a over the left-hand crest line 7.
  • the embodiment b (right), only one lug 132b is provided which protrudes beyond the crest line 7.
  • FIG. 8 further cross-sectional variants are outlined, in which the cylindrical shell region comprising the shell shells 2, 4 and the flat wall 6, from a
  • the two-part embodiment B comprises two shell elements 2, 4 each having a planar portion 6a, 6b.
  • the shell shell ends on the crease lines 102, 104 and the planar portions 6a, 6b are welded to each other in the longitudinal direction of the container (along the joint 106).
  • the shell shells not only have independent radii of curvature, but in which circumferentially different wall thicknesses are provided. This can be compensated in the other (larger) radii of curvature usually higher compressive stresses.
  • This stress-resistant design allows further weight savings or higher pressure loads.
  • this outer jacket 5 can also be used as an effective component for receiving pressure loads. Prerequisite for this is a force-transmitting coupling between inner container and outer container. This is done for example via a between the indoor and
  • Exterior walls provided support grid (not shown), which point or line allows a power transmission between the container walls.
  • additional gusset plates for coupling can also be provided, which allow a particularly effective removal of the load peaks occurring on the inner wall into the outer wall.
  • FIG 9 shows the pressure vessel 1, in a tank container unit 100, in which it is coupled via the end rings 20 with this.
  • the illustrated tank container unit 100 is suitable for a hook lift and comprises loading skids 101 and an aggregate space 102 and a folding terrain unit 103, so that the illustrated unit can be used as a largely self-sufficient supply unit.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Packages (AREA)
  • Rigid Containers With Two Or More Constituent Elements (AREA)
  • Packaging Of Annular Or Rod-Shaped Articles, Wearing Apparel, Cassettes, Or The Like (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Discharge Heating (AREA)
  • Refuse Collection And Transfer (AREA)

Abstract

La présente invention concerne un réservoir sous pression (1) avec une enveloppe faite de viroles parallèles partiellement cylindriques (2, 4) juxtaposées et définissant une moulure (8, 10) orientée dans la direction longitudinale. Chacune des extrémités frontales est fermée par un fond bombé (16, 18). Entre les viroles partiellement cylindriques (2, 4) est placé un élément de traction prenant en particulier la forme d'une cloison plane (6; 6a, 6b) dont les bords (12, 14) respectivement supérieur et inférieur font saillie dans la zone de moulure respectivement supérieure et inférieure (8, 10) ou bien la traversent. Il est par ailleurs prévu un élément de coque (42) qui s'étend dans la direction longitudinale et relie les viroles (2, 4) et l'élément de traction (42) et qui est solidarisé au moins par endroits avec les viroles (2, 4) et avec le bord (12, 12a; 14, 14a), en particulier replié, de l'élément de traction (6), si bien qu'une structure porteuse est formée dans la zone de moulure (8, 10). L'invention concerne en outre un agencement de réservoir de transport, en particulier une unité de citerne (100) avec un réservoir sous pression selon l'invention (1).
PCT/EP2009/009203 2008-12-22 2009-12-21 Réservoir sous pression pour un agencement de réservoir de transport WO2010072400A1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
EP09799281A EP2238383B1 (fr) 2008-12-22 2009-12-21 Réservoir sous pression pour un agencement de réservoir de transport
ES09799281T ES2375445T3 (es) 2008-12-22 2009-12-21 Recipiente a presión para una disposición de un recipiente de transporte.
CA2716895A CA2716895C (fr) 2008-12-22 2009-12-21 Reservoir sous pression pour un agencement de reservoir de transport
PL09799281T PL2238383T3 (pl) 2008-12-22 2009-12-21 Zbiornik ciśnieniowy do transportowanego zestawu zbiornikowego
AT09799281T ATE529686T1 (de) 2008-12-22 2009-12-21 Druckbehälter für eine transportbehälteranordnung
US12/937,342 US20110031257A1 (en) 2008-12-22 2009-12-21 Pressure Container for a Transport Container Arrangement
DK09799281.2T DK2238383T3 (da) 2008-12-22 2009-12-21 Trykbeholder til et transportbeholderanordning
JP2011541232A JP5311520B2 (ja) 2008-12-22 2009-12-21 輸送コンテナ用の圧力容器
ZA2010/06017A ZA201006017B (en) 2008-12-22 2010-08-24 Pressure container for a transport container arrangement

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008064364.5 2008-12-22
DE102008064364A DE102008064364A1 (de) 2008-12-22 2008-12-22 Druckbehälter für eine Transportbehälteranordnung

Publications (1)

Publication Number Publication Date
WO2010072400A1 true WO2010072400A1 (fr) 2010-07-01

Family

ID=41818444

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/009203 WO2010072400A1 (fr) 2008-12-22 2009-12-21 Réservoir sous pression pour un agencement de réservoir de transport

Country Status (13)

Country Link
US (1) US20110031257A1 (fr)
EP (1) EP2238383B1 (fr)
JP (1) JP5311520B2 (fr)
AT (1) ATE529686T1 (fr)
CA (1) CA2716895C (fr)
CL (1) CL2010000916A1 (fr)
DE (1) DE102008064364A1 (fr)
DK (1) DK2238383T3 (fr)
ES (1) ES2375445T3 (fr)
PL (1) PL2238383T3 (fr)
RU (1) RU2463513C2 (fr)
WO (1) WO2010072400A1 (fr)
ZA (1) ZA201006017B (fr)

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CN105460444A (zh) * 2015-12-30 2016-04-06 西安轨道交通装备有限责任公司 一种裙座排水结构
WO2022094093A1 (fr) * 2020-10-29 2022-05-05 Noble Gas Systems, Inc. Système de support pour réservoirs conformables

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Publication number Priority date Publication date Assignee Title
JP5750406B2 (ja) * 2012-06-20 2015-07-22 株式会社神戸製鋼所 圧力容器
US8985376B2 (en) 2012-09-12 2015-03-24 Crown Tank Company, Llc Frac tanks
US9364696B2 (en) * 2013-01-01 2016-06-14 Oval Fire Products Corporation Regulatory compliant fire extinguisher
DE202015102776U1 (de) 2015-05-29 2016-08-30 Frauenthal Automotive Management Gmbh Druckbehälter, insbesondere Druckluftbehälter zur Speicherung von Druckluft eines druckluftbetriebenen Bremssystems eines Nutzfahrzeuges
EP3446025A1 (fr) * 2016-04-22 2019-02-27 United Technologies Corporation Ensemble cuve sous pression composite doté d'un ensemble buse intégré
CN109073151B (zh) * 2016-05-10 2020-08-04 瓦锡兰芬兰有限公司 双叶或多叶储罐
EP3558848B1 (fr) 2016-12-20 2023-01-25 Titan Trailers Inc. Construction de conteneur de fret cylindrique
WO2018112618A1 (fr) 2016-12-20 2018-06-28 Michael Kloepfer Semi-remorque cylindrique
USD915945S1 (en) 2016-12-20 2021-04-13 Michael Kloepfer Cylindrical semi-trailer
CA3218391A1 (fr) * 2017-09-22 2019-03-28 Titan Trailers Inc. Conteneur a marchandises quasi cylindrique et fabrication
DE202018103064U1 (de) * 2018-05-30 2019-09-02 Gofa Gocher Fahrzeugbau Gmbh Tankcontaineranordnung

Citations (5)

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RU2463513C2 (ru) 2012-10-10
RU2010143222A (ru) 2012-04-27
US20110031257A1 (en) 2011-02-10
PL2238383T3 (pl) 2012-05-31
EP2238383B1 (fr) 2011-10-19
DK2238383T3 (da) 2011-12-19
ATE529686T1 (de) 2011-11-15
DE102008064364A1 (de) 2010-07-01
CL2010000916A1 (es) 2011-04-08
ES2375445T3 (es) 2012-02-29
CA2716895C (fr) 2013-11-26
JP5311520B2 (ja) 2013-10-09
EP2238383A1 (fr) 2010-10-13
ZA201006017B (en) 2011-10-26
JP2012513343A (ja) 2012-06-14
CA2716895A1 (fr) 2010-07-01

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