EP2877776A1 - Récipient de transport pour fluides cryogéniques - Google Patents

Récipient de transport pour fluides cryogéniques

Info

Publication number
EP2877776A1
EP2877776A1 EP13740212.9A EP13740212A EP2877776A1 EP 2877776 A1 EP2877776 A1 EP 2877776A1 EP 13740212 A EP13740212 A EP 13740212A EP 2877776 A1 EP2877776 A1 EP 2877776A1
Authority
EP
European Patent Office
Prior art keywords
holding part
longitudinal axis
container
inner container
end wall
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.)
Granted
Application number
EP13740212.9A
Other languages
German (de)
English (en)
Other versions
EP2877776B1 (fr
Inventor
Christian INTERWIES
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ziemann Holvrieka GmbH
Original Assignee
Ziemann International 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 Ziemann International GmbH filed Critical Ziemann International GmbH
Publication of EP2877776A1 publication Critical patent/EP2877776A1/fr
Application granted granted Critical
Publication of EP2877776B1 publication Critical patent/EP2877776B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F17C3/00—Vessels not under pressure
    • F17C3/02—Vessels not under pressure with provision for thermal insulation
    • 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
    • F17C2201/03—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
    • F17C2201/054—Size medium (>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
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01—Mounting arrangements
    • F17C2205/0103—Exterior arrangements
    • F17C2205/0107—Frames
    • 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
    • F17C2205/0123—Mounting arrangements characterised by number of vessels
    • F17C2205/0126—One 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
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01—Mounting arrangements
    • F17C2205/0153—Details of mounting arrangements
    • F17C2205/0192—Details of mounting arrangements with external bearing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/228—Assembling processes by screws, bolts or rivets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/23—Manufacturing of particular parts or at special locations
    • F17C2209/232—Manufacturing of particular parts or at special locations of walls
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/03—Dealing with losses
    • F17C2260/031—Dealing with losses due to heat transfer

Definitions

  • Transport container used. They are double-walled and have an outer container with a cylindrical single-walled main body and two outwardly curved single-walled end walls, in which an inner container is housed, which is similar in shape and has slightly smaller dimensions (US 5,533,340).
  • a respective holding device is arranged, which are arranged coaxially to the longitudinal axis of the outer container and the inner container.
  • Each holding device is connected on the one hand to the adjacent end wall of the outer container and on the other hand to the adjacent end wall of the inner container.
  • the first holding device is formed in one piece and rigid.
  • the second holding device has two holding parts, by means of which the two end walls are displaceable relative to each other in the axial direction in order to compensate for the change in length of the inner container relative to the outer container due to the lower temperature of the fluid.
  • a connecting line is connected to an evacuation device, by means of which the space between the outer container and the
  • Inner container can be evacuated to provide thermal insulation for the inner container.
  • the first holding part is formed as a continuous hollow profile, which by a Circular cylinder is flattened at the top side.
  • the second holding part is formed by a pin which is matched to the hollow profile of the first holding part.
  • the shrunken pin is theoretically only along a Zylindermantellin, practically, due to the elastic deformation of the parts, in the range of a very narrow peripheral region on the cylindrical hollow profile. This results in a correspondingly high surface pressure. In any case, this is so high that a greater wear of the contact surfaces is inevitable in the frequently anticipated lateral accelerations. In addition, the shrunken pin no longer rests in the horizontal direction on the two inner walls of the cylindrical hollow profile.
  • the pin performs at each lateral acceleration of the transport container a relative movement relative to the cylindrical hollow profile, which in combination with the already greatly reduced contact area in addition to an even higher wear of both the pin as well as the hollow profile contributes. This limits the longest possible service life of the transport container very strong.
  • the invention has for its object to provide a transport container for cryogenic fluids, in which di dimensional changes of the inner container due to its reduced temperature less adversely affect the contact surfaces of the second holding device than is the case with the known transport container.
  • the contact surfaces of the first holding part and the cooperating abutment surfaces of the second holding part are flat and are arranged symmetrically to the vertical plane of the longitudinal axes of the outer container and the inner container V-shaped, retain these contact surfaces even with a dimensional changes of the inner container their planar shape and their V-shaped arrangement, so that the mutual full-surface investment and thus the relatively low surface pressure of these contact surfaces is always maintained.
  • the abutment surfaces of the second holding part only move parallel to the abutment surfaces of the first holding part, both in the axial direction and in the direction of the legs of the V-shape of the contact surfaces.
  • the contact surfaces are arranged in a V-shape, they can both the weight of the inner container and vertical downward acceleration forces as well as horizontal acceleration forces absorb equally well, without causing relative movements of the two holding parts occur.
  • the contact surfaces of the first holding part in the axial direction have a longitudinal extent, at least approximately equal to the sum of the axial length de Bearing surfaces of the second holding part and from the difference of the axial length of the inner container at ambient temperature and at operating temperature, it is ensured that the contact surfaces of the second holding part always fully abut the contact surfaces of the first holding part, so that in so far the surface pressure of the contact surfaces remains the same and relatively low. All these measures ensure that the wear of the contact surfaces remains relatively low over a longer period of time.
  • An embodiment of the transport container according to claim 2 ensures that the second holding device can also absorb vertically upward acceleration forces that exceed the simple gravitational acceleration. Due to the fact that the two contact surfaces and the two further contact surfaces as well as the second holding part are firmly connected to one another in the manner of a quadrilateral frame both in the case of the first holding part, both the abutment surfaces and the two other contact surfaces are firmly connected to one another second holding part stiffened and strengthened. That comes the dimensional stability of all levels
  • the second holding device can be easily adjusted to different operating conditions. With a larger angle of inclination and a corresponding larger spread angle ß higher vertical forces can be absorbed. With a smaller inclination angle ⁇ and a corresponding smaller spread angle ⁇ larger horizontal forces can be absorbed. In one embodiment of the transport container after
  • Claim 4 the holding parts are easier and more accurate to manufacture. In this embodiment, there is an average value for the capacity of vertical forces and horizontal forces.
  • the part of the holding device located above the longitudinal axis can also be easily adjusted to other requirements with regard to the capacity of vertical forces and horizontal forces, as is the case with the underlying part of the holding device.
  • An embodiment of the transport container according to claim 6 facilitates the manufacture and assembly of the entire holding device and achieves an average suitability for receiving vertical forces and horizontal forces.
  • An embodiment of the transport container according to claim 7 ensures that the second holding device is designed to save space.
  • the wear in particular of the arranged below the longitudinal axis of contact surfaces can be significantly reduced not only in a temperature-induced shrinkage or expansion of the inner container but also in the different acceleration forces occurring.
  • the heat transfer is reduced to the inner container.
  • the invention is based on a in the following
  • Figure 1 is a perspective view of the transport container with an outer container and an inner container housed therein.
  • FIG. 2 shows a longitudinal section of the transport container through the longitudinal axis of the two containers, without the usual installations of the inner container and without the usual lines.
  • FIG. 3 shows a detail enlargement according to the section line A in FIG. 2;
  • FIG. 4 shows a detail enlargement according to the sectioning line B in FIG. 2;
  • FIG. 5 shows a cross section of the transport container according to the section line D - D in FIG. 2 and FIG. 7;
  • Fig. 6 is a detail enlargement of Fig. 5;
  • FIG. 6a shows a first partial cutout from FIG. 6;
  • FIG. 6b shows a second partial cutout from FIG. 6
  • FIG. 7 shows a detail enlargement according to the section line C in FIG. 2 and according to the section line E - E in FIG. 5;
  • FIG. 8 shows a detail enlargement according to the sectioning line C in FIG. 2 and according to the section line F - F in FIG. 5;
  • the transport container 10 is shown as a whole in FIG. Its basic structure can be seen from Fig. 2. In it, however, the better overview because of the usual fittings and lines are not shown.
  • the transport container 10 has an outer container 11 and an inner container 12, which are arranged coaxially with each other.
  • the outer container 11 has a cylindrical single-walled main body 13 and two outwardly curved single-walled end walls 14 and 15, which are firmly welded together.
  • the inner container 12 also has a cylindrical single-walled main body 16 and two outwardly curved single-walled end walls 17 and 18, which are firmly welded together.
  • the outer container 11 and the inner container 12 have a common longitudinal axis 19th
  • a first holding device 21 is present, which is arranged coaxially to the longitudinal axis 19.
  • This first holding device 21 is firmly welded both to the end wall 14 of the outer container 11 and to the end wall 17 of the inner container 12 (FIG. 4).
  • the two containers 11 and 12 are fixedly connected together at this end.
  • a second holding device 22 is present, which is also arranged coaxially to the longitudinal axis 19.
  • the second holding device 22 has two holding parts, which are designed and arranged such that the two end walls 15 and 18 are displaceable in the axial direction relative to each other. They are described in greater detail with reference to FIGS. 5 to 9.
  • the first holding device 21 forms virtually a fixed bearing for the two containers 11 and 12 and the second holding device 22 forms quasi a movable bearing for the two containers 11 and 12.
  • the Base body 13 of the outer container 11 is provided on its outside with a helical reinforcement 23. It is formed by a hollow profile 24 which is open toward the base body 13 (FIG. 3), whose edges 25 are welded continuously to the base body 13, with adjacent spiral sections having a predetermined mutual distance.
  • This reinforcement 23 serves on the one hand to prevent buckling of the cylindrical Grundgropers 13 of the outer container 11 when the space between the outer container 11 and the inner container 12 is evacuated to thermally insulate the inner container 11 relative to the outer container 12. On the other hand, it serves the purpose of a leak of the
  • Inner container 12 occurring pressure increase in the outer container 11 to catch.
  • outside reinforcement 23 can be avoided on the inside of the outer container 11 arranged reinforcements and thereby a larger interior can be achieved.
  • the first holding device 21 is formed mainly by a cylindrical holding tube 26, which is welded on the one hand to the outside of the end wall 17 of the inner container 12 and on the other hand with the end wall 14 of the outer container 11.
  • a closure plate 28 is used, which has the same thickness and curvature as the end wall 14, and with the inside of the
  • an insulating material 29 is applied and fixed on the outer side of the end wall 14 in order to minimize the unavoidable heat transfer.
  • the holding device 22 is not cylindrical, as in the prior art, but quadrangular. It has in the preferred embodiment the shape of a square placed on top.
  • the second holding device 22 has an outer first holding part 31 (FIG. 6 a) and an inner second holding part 31. Part 32 (Fig. 6b), which are arranged coaxially with each other in the same axial region of the transport container 10 (Fig. 6).
  • the inner contour of the outer holding part 31 and the outer contour of the inner holding part 32 are coordinated so that at room temperature of the outer container 11 and the inner container 12, the two holding parts 31 and 32 can be assembled without difficulty and at any time in the axial direction relative to each other are displaceable.
  • the first holding part 31 (FIG. 6 a) has two flat abutment surfaces 33 and 34 which are located below the longitudinal axis 19, which are aligned parallel to the longitudinal axis 19 and face the longitudinal axis 19, which have a predetermined inclination angle ⁇ of one another Include 90 ° and are aligned symmetrically to the vertical plane 35 of the longitudinal axis 19.
  • the second holding part 32 (FIG. 6b) has, in a corresponding manner, two planar abutment surfaces 36 and 37 which are located below the longitudinal axis 19 of the inner container 12, which are aligned parallel to the longitudinal axis 19 and remote from the longitudinal axis 19 Contradictive angle to the inclination angle ⁇ have a spread angle ß, equal to the extended by 180 ° angle of inclination
  • the contact surfaces 33 and 34 are formed by the true outside of a retaining strip 41 and 42, respectively.
  • the abutment surfaces 36 and 37 are formed by the true outside of a retaining strip 43 and 44, respectively.
  • Holding member 32 is provided with two other abutment surfaces 47 and 48, of which the abutment surfaces 45 and 46 of the
  • the two other contact surfaces 45 and 46 close to each other an inclination angle ⁇ , which is equal to the inclination angle ⁇ of the contact surfaces 33 and 34.
  • the two other abutment surfaces 47 and 48 have a
  • Contact surfaces 45 and 46 and the other abutment surfaces 47 and 48 are aligned symmetrically to the vertical plane 35 of the longitudinal axis 19.
  • the other contact surfaces 45 and 46 are by the true outside of a retaining strip 51 and 52, respectively educated.
  • the other abutment surfaces 47 and 48 are formed by the true outside of a retaining strip 53 and 54, respectively.
  • the retaining strips 41 and 42 and the retaining strips 51 and 52 are welded together, so that they form a rigid outer square frame 55.
  • the retaining strips 43 and 44 and the retaining strips 53 and 54 are welded together, so that they form a rigid inner square frame 56.
  • the quadrilateral frame 55 of the first holding part 31 has on the side remote from the end wall 17 of the outer container 11 a flat boundary surface or end face 57 (FIG. 7), which is aligned normal to the longitudinal axis 19.
  • On the end wall 17 side facing the boundary surface of the square frame 55 is tuned to the concave inner side of the end wall 17 of the outer container 11.
  • the square frame 56 of the second holding part 32 has on the side remote from the end wall 18 of the inner container 12 side a flat boundary surface or end face 58, which is aligned normal to the longitudinal axis 19.
  • the boundary surface of the quadrilateral frame 56 matched to the convex outside of the end wall of the inner container 12.
  • the quadrilateral frame 55 of the first holding part 31 is welded on its outside with a stiffening ring 61 which reinforces the quadrangular frame 55 at the same time and whose ground plan has the shape of a quadrangular ring (FIG. 6 a).
  • the square frame 56 of the second support member 32 is welded on its inside with a stiffening plate 62 (Fig. 6b), which reinforces the square frame 56 at the same time and whose floor plan has the shape of a square whose corners are cut off for welding reasons.
  • the stiffening ring 61 is arranged in the region of the free end of the outer square frame 55 (FIG. 8).
  • the stiffening disk 62 is arranged in the region of the free end of the inner square frame 56 (FIG. 7).
  • a plate-shaped strut 63 is welded (Fig. 6a), which is also welded to the inside of the end wall 17 of the outer container 11 (Fig. 7).
  • the end wall 14 of the outer container 11 (FIG. 4) has, in order to increase its rigidity in the region of the first holding device 21, a central surface section 64 whose wall thickness is greater than that of the surface section 65 surrounding it.
  • the end wall 17 of the inner container 12 has a central
  • the end wall 15 of the outer container 11 has a central one
  • the Front wall 18 of the inner container 12 has a central surface portion 71, whose wall thickness is greater than that of the surrounding surface portion 72. All these measures ensure that the level
  • a sliding element 73 is arranged on the outer side of the retaining strips 43, 44, 53 and 54 of the inner quadrilateral frame 56.
  • the sliding elements 73 are made of tetrafluoroethylene, are plate-shaped and have a rectangular plan. Each sliding element 73 is inserted into a recess 74, which is matched to its plan view, on the side edges 75 of which the sliding element 73 rests.
  • the sliding elements 73 are screwed with at least two countersunk screws 76 with the associated retaining strip, which are provided with corresponding threaded holes 77.
  • This embodiment of the transport container 10, in which all the retaining strips of the inner square frame 56 are provided with a sliding member 73, is especially in difficult transport conditions into consideration, in which strong horizontal acceleration forces are superimposed by equally strong vertically upward acceleration forces, so that the inner square frame 56 abuts against the above the longitudinal axis 19 arranged bearing surfaces 45 and 46 of the outer square frame 55 and the sliding elements abutting 73 of the abutment surfaces 47 and 48 slide along it.
  • an embodiment not shown in the drawing can be used are, in which only the arranged below the longitudinal axis 19 abutment surfaces 36 and 37 of the inner square frame 56 are provided with a sliding member 73.
  • a number of support plates 78 are welded to the end walls 14 and 15 of the outer container 11, by means of the transport container 10, each with a support frame 79 with standardized

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Packages (AREA)

Abstract

L'invention concerne des récipients de transport tels qu'ils sont spécialement mis en œuvre pour le transport de fluides cryogéniques, lesdits récipients ayant une double paroi et comportant un récipient extérieur lequel est pourvu d'un corps de base cylindrique et de deux parois frontales et dans lequel est logé un récipient intérieur d'une forme similaire. Un dispositif de support est disposé à chacune des extrémités du récipient intérieur. Le premier dispositif de support est réalisé de manière à être rigide et à être relié à la paroi frontale adjacente du récipient extérieur. Le deuxième dispositif de support comporte deux parties de support lesquelles permettent de déplacer les deux parois frontales axialement l'une par rapport à l'autre. La partie de support mobile est réalisée sous forme d'un doigt cylindrique qui est tenu par un corps profilé en forme de cylindre creux. En raison de la basse température du récipient intérieur, le doigt subit un rétrécissement concernant également son diamètre, faisant en sorte que les surfaces de contact se réduisent, dans la pratique, à une partie très étroite des surfaces circonférentielles concernées. Ainsi, la pression rapportée à la surface est très élevée, et les accélérations horizontales se produisant lors du transport provoquent une usure importante des surfaces de contact. Selon l'invention, ce problème est résolu en mettant en œuvre un dispositif de support (22) mobile dont la première partie de support (31) comporte deux surfaces d'appui planes (33 ; 34) qui coopèrent avec deux surfaces d'appui planes (36 ; 37) de la deuxième partie de support (32) lesquelles sont disposées en forme de V et orientées de manière à être symétriques par rapport au plan vertical (35) de l'axe longitudinal (19). Même lorsque la deuxième partie de support (32) subit un rétrécissement, les surfaces de contact conservent leur forme plane, permettant ainsi de maintenir une faible pression rapportée à la surface et une faible usure.
EP13740212.9A 2012-07-25 2013-07-22 Récipient de transport pour fluides cryogéniques Not-in-force EP2877776B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012014709.0A DE102012014709A1 (de) 2012-07-25 2012-07-25 Transportbehälter für kryogene Fluide
PCT/EP2013/002156 WO2014015969A1 (fr) 2012-07-25 2013-07-22 Récipient de transport pour fluides cryogéniques

Publications (2)

Publication Number Publication Date
EP2877776A1 true EP2877776A1 (fr) 2015-06-03
EP2877776B1 EP2877776B1 (fr) 2019-02-20

Family

ID=48874246

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13740212.9A Not-in-force EP2877776B1 (fr) 2012-07-25 2013-07-22 Récipient de transport pour fluides cryogéniques

Country Status (3)

Country Link
EP (1) EP2877776B1 (fr)
DE (1) DE102012014709A1 (fr)
WO (1) WO2014015969A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014206370B4 (de) 2014-04-03 2022-05-25 Bayerische Motoren Werke Aktiengesellschaft Druckbehälter mit einem Innen- und einem Außenbehälter
DE102017210722B4 (de) * 2017-06-26 2020-05-14 Bayerische Motoren Werke Aktiengesellschaft Kraftfahrzeug und Druckbehälter mit divergierendem Verbindungsrohr
EP4180706A1 (fr) * 2021-11-10 2023-05-17 Zero Emissions Aerospace Limited Réservoir cryogénique
EP4235012A1 (fr) * 2022-02-25 2023-08-30 Airbus Operations (S.A.S.) Réservoir comprenant des enceintes interne et externe ainsi qu au moins un système de liaison à lames radiales souples reliant lesdites enceintes
DE102022208593A1 (de) 2022-08-18 2024-02-29 Magna Energy Storage Systems Gesmbh Kryotankvorrichtung

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799425A (en) * 1951-07-24 1957-07-16 Bendix Aviat Corp Receptacle for volatile liquids
US2729357A (en) * 1953-05-06 1956-01-03 Cambridge Corp Vacuum jacketed container
DE1551602A1 (de) * 1967-04-26 1970-03-19 Messer Griesheim Gmbh Doppelwandiger Behaelter fuer tiefkalte,verfluessigte Gase
US3698200A (en) * 1970-12-16 1972-10-17 Air Prod & Chem Cryogenic storage dewar
US4038832A (en) * 1975-09-08 1977-08-02 Beatrice Foods Co. Liquefied gas container of large capacity
DE3001922A1 (de) * 1980-01-19 1981-07-23 Linde Ag, 6200 Wiesbaden Behaelter fuer tiefkalte verfluessigte gase
US5533340A (en) 1994-04-12 1996-07-09 Hydro-Quebec Double-walled container for transporting and storing a liquified gas
DE19935361A1 (de) * 1999-07-29 2001-02-22 Detlef Bornemann Palette für den Transport und/oder die Lagerung von Gasflaschen oder dgl.
EP1230511B1 (fr) * 1999-10-29 2005-06-01 Mallinckrodt Inc. Unite a oxygene liquide portable avec orientations fonctionnelles multiples
AT414164B (de) * 2001-04-27 2006-09-15 Schwingenschloegel Ges M B H Tank
CA2441775C (fr) * 2003-09-23 2004-09-28 Westport Research Inc. Contenant pour fluide cryogenique
CN2702156Y (zh) * 2004-04-15 2005-05-25 中国国际海运集装箱(集团)股份有限公司 高真空绝热低温液化气体储罐及其外壳结构
DE102004060591B4 (de) * 2004-12-16 2016-04-07 Magna Steyr Fahrzeugtechnik Ag & Co. Kg Tank für kryogene Medien sowie Verfahren und Vorrichtung zu dessen Zusammenbau
GB0703693D0 (en) * 2007-02-26 2007-04-04 Jahre Group As Support structure
US8356786B2 (en) * 2008-06-12 2013-01-22 GM Global Technology Operations LLC Flexible laminated suspension bracket for composite type 4 tanks

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2014015969A1 *

Also Published As

Publication number Publication date
DE102012014709A1 (de) 2014-01-30
WO2014015969A1 (fr) 2014-01-30
EP2877776B1 (fr) 2019-02-20

Similar Documents

Publication Publication Date Title
DE2707891C3 (de) Behälter nach Art eines Containers, mit einem Tank
EP2877776B1 (fr) Récipient de transport pour fluides cryogéniques
DE202012007223U1 (de) Transportbehälter für kryogene Fluide
DE102010006220A1 (de) Teleskopische Abdeckung
DE2642227B1 (de) Klemmelement
EP3331777B1 (fr) Dispositif et procédé de stockage et/ou de transport d'articles en forme de plaque
CH627872A5 (de) Einrichtung zur lagerung von kernbrennelementen.
DE8708486U1 (de) Schutztürvorrichtung für Luftschutzanlagen und Atomarkraftwerke
DE102014103930A1 (de) Vorrichtung zum Aufnehmen und Lagern von Behältnissen
EP0502361A1 (fr) Dispositif de blindage de tranchée
DE202012002498U1 (de) Tür, Metallkonstruktionsprofil einer Zarge oder eines Rahmens für eine Tür oder ein Fenster
AT518057B1 (de) Wärmetauschervorrichtung
DE3048951C2 (de) Solarkollektor mit evakuiertem Innenraum
DE202008007467U1 (de) Abstützvorrichtung, insbesondere Unterstellbock
DE202004021811U1 (de) Schichtenspeicher mit einem Gehäuse und einer Isolierung
DE2203237A1 (de) Zusammengesetztes waermeisolierendes profil fuer fensterrahmen, tuerrahmen oder dgl
AT518089B1 (de) Umhüllungseinheit, insbesondere für thermisch zu dämmende Körper
DE2636002A1 (de) Mehrlappiger tank
DE2941454C2 (de) Hebevorrichtung für Hubtische
DE29504288U1 (de) Schutzvorrichtung zur Rückhaltung von Flüssigkeiten
DE102012009263A1 (de) Transportbehälter für unter Druck stehende Fluide
CH660413A5 (de) Rollenlager zur auflagerung von heiss- oder kaltgehenden rohrleitungen.
DE2637011B2 (de) Doppelwandiger Tank
DE102022107962A1 (de) Modulares Thekenauslagesystem zum Kühlen von Lebensmitteln und Thekenauslagevorrichtung
DE10004835C2 (de) Druckstabiler Temperierbehälter

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20141218

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: ZIEMANN HOLVRIEKA GMBH

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20170612

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20180816

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

INTC Intention to grant announced (deleted)
GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

INTG Intention to grant announced

Effective date: 20190104

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502013012223

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1098657

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190315

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190220

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190620

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190520

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190620

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190520

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190521

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20190702

Year of fee payment: 7

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502013012223

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20191121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20190722

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190722

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190722

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190722

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1098657

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190722

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190722

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502013012223

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210202

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20130722

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190220