Transport container with coolable thermal shield

Abstract

The invention relates to a transport container (1) for helium (He), comprising an inner container (6) for receiving the helium (He); a coolant container (14) for receiving a cryogenic fluid (N2); an outer container (2) in which the inner container (6) and the coolant container (14) are received; a thermal shield (21) in which the inner container (6) is received and which can be actively cooled using the cryogenic fluid (N2), said thermal shield (21) having at least one cooling line (26) which is fluidically connected to the coolant container (14) and in which the cryogenic fluid (N2) can be received in order to actively cool the thermal shield (21); and at least one return line (34, 35), by means of which the at least one cooling line (26) is fluidically connected to the coolant container (14) in order to return the cryogenic fluid (N2) back to the coolant container (14).

Claims

1. A transport container (1) for helium (He) comprising: an inner container (6) for receiving the helium (He), a coolant container (14) for receiving a cryogenic fluid (N2), an outer container (2) in which the inner container (6) and the coolant container (14) are received, and a thermal shield (21) in which the inner container (6) is received and which can be actively cooled using the cryogenic fluid (N2), said thermal shield (21) having at least one cooling line (26), which is fluidically connected to the coolant container (14) and in which the cryogenic fluid (N2) can be received in order to actively cool the thermal shield (21), and at least one return line (34, 35), by means of which the at least one cooling line (26) is fluidically connected to the coolant container (14) in order to return the cryogenic fluid (N2) back to the coolant container (14), wherein an inside diameter (d34, d35) of the at least one return line (34, 35) is larger than an outside diameter (d26) of the at least one cooling line (26).

2. The transport container according to claim 1, wherein the at least one cooling line (26) is fluidically connected to a liquid zone (19) of the coolant container (14), and wherein the at least one return line (34, 35) is fluidically connected to a gas zone (18) of the coolant container (14).

3. The transport container according to claim 1, wherein the at least one return line (34, 35) opens into the coolant container (14) above, with respect to a direction of gravity (g), the at least one cooling line (26).

4. The transport container according to claim 1, wherein a lowest point of the at least one cooling line (26) is fluidically connected to the coolant container (14).

5. The transport container according to claim 1, wherein a highest point of the at least one cooling line (26) is fluidically connected to the coolant container (14) with the aid of the at least one return line (34, 35).

6. The transport container according to claim 1, wherein the inside diameter (d26) of the at least one cooling line (26) is larger than 10 millimeters.

7. The transport container according to claim 1, wherein the at least one return line (34, 35) is inclined in the direction of the coolant container (14) at an angle of inclination (β).

8. The transport container according to claim 1, wherein the at least one return line (34, 35) is connected to the thermal shield (21) and arranged between the thermal shield (21) and the outer container (2).

9. The transport container according to claim 1, wherein, during operation of the transport container (1), the cryogenic fluid (N2) boils to actively cool the thermal shield (21) in the at least one cooling line (26), so that gas bubbles, arising in the at least one cooling line (26), of a gaseous phase (GN2) of the cryogenic fluid (N2) convey a liquid phase (LN2) of the cryogenic fluid (N2) into the at least one return line (34, 35), so as to return the gaseous phase (GN2) of the cryogenic fluid (N2) and/or the liquid phase (LN2) of the cryogenic fluid (N2) back to the coolant container (14).

10. The transport container according to claim 1, wherein a first return line (34) and a second return line (35) are provided which run parallel to one another.

11. The transport container according to claim 1, wherein the coolant container (14) has a bleed valve (36) for bleeding off a gaseous phase (GN2) of the cryogenic fluid (N2) from the coolant container (14).

12. The transport container according to claim 1, wherein the inner container (6) is completely surrounded by the thermal shield (21).

13. The transport container according to claim 12, wherein the thermal shield (21) has a cover section (24) which is separate from the coolant container (14) and is arranged between the inner container (6) and the coolant container (14).

14. The transport container according to claim 1, wherein the coolant container (14) is arranged outside the thermal shield (21).

15. The transport container according to claim 1, wherein an intermediate space (12) is provided between the outer container (2) and the inner container (6) and between the outer container (2) and the coolant container (14).

16. The transport container according to claim 1, wherein the thermal shield (21) is fluid-permeable and a gap (25) is provided between the inner container (6) and the thermal shield (21), and said gap (25) is fluidically connected to the intermediate space (12).

17. The transport container according to claim 1, wherein the at least one cooling line (26) comprises two perpendicular sections (27, 28), extending in a direction of gravity (g), and two oblique sections (29, 30).

18. The transport container according to claim 1, wherein two oblique sections (29, 30) have an angle of inclination α of 3° to 15° relative to a horizontal.

19. The transport container according to claim 1, wherein the at least one return line (34, 35) is inclined at an angle of inclination β of 4° to 15° relative to a horizontal.

20. The transport container according to claim 10, wherein the first return line (34) and the second return line (35) are inclined at an angle of inclination β of 4° to 15° relative to a horizontal.

Description

(1) Further advantageous embodiments of the transport container are the subject matter of the subclaims and of the exemplary embodiments of the transport container described below. In addition, the transport container is explained in more detail on the basis of preferred embodiments, with reference to the accompanying figures.

(2) FIG. 1 shows a schematic view of an embodiment of a transport container;

(3) FIG. 2 shows a further schematic view of the transport container in FIG. 1; and

(4) FIG. 3 shows a schematic sectional view of the transport container according to the section line III-III of FIG. 2.

(5) In the figures, the same or functionally equivalent elements have been assigned the same reference symbols, unless indicated otherwise. FIG. 1 shows a highly simplified schematic view of an embodiment of a transport container 1 for liquid helium He. FIG. 2 shows a further, highly simplified schematic view of the transport container 1, and FIG. 3 shows a schematic sectional view of the transport container 1 along the section line III-III of FIG. 2. Hereafter, reference is made to FIGS. 1 through 3 at the same time.

(6) The transport container 1 can also be referred to as a helium transport container. The transport container 1 can also be used for other cryogenic fluids. Examples of cryogenic fluids—or cryogens, for short—are the aforementioned liquid helium He (boiling point at 1 bara: 4.222 K=−268.929° C.), liquid hydrogen H2 (boiling point at 1 bara: 20.268 K=−252.882° C.), liquid nitrogen N2 (boiling point at 1 bara: 7.35 K=195.80° C.) or liquid oxygen O2 (boiling point at 1 bara: 9.18 K=182.97° C.).

(7) The transport container 1 comprises an outer container 2. The outer container 2 can be made of stainless steel, for example. The outer container 2 can have a length L2 of 10 meters, for example. The outer container 2 comprises a tubular or cylindrical base section 3, which is closed at the end face on both sides with the aid of a cover section 4, 5—in particular, with the aid of a first cover section 4 and a second cover section 5. The base section 3 can have a circular or approximately circular geometry in cross-section. The cover sections 4, 5 are curved. The cover sections 4, 5 are curved in opposite directions, so that both cover sections 4, 5 are curved outwards with respect to the base section 3. The outer container 2 is fluid-tight, and, in particular, gas-tight. The outer container 2 has a central axis or an axis of symmetry M1, in relation to which the outer container 2 is designed to be rotationally symmetrical.

(8) The transport container 1 further comprises an inner container 6 for receiving the helium He. The inner container 6 is not shown in FIG. 2. The inner container 6 is likewise made of stainless steel, for example. A gas zone 7 with vaporized helium He and a liquid zone 8 with liquid helium He can be provided in the inner container 6, as long as the helium He is in the two-phase region. The inner container 6 is fluid-tight, and, in particular, gas-tight, and can comprise a bleed valve for controlled pressure reduction. Like the outer container 2, the inner container 6 comprises a tubular or cylindrical base section 9, which is closed at the end face on both sides by cover sections 10, 11,—in particular, a first cover section 10 and a second cover section 11. The base section 9 can have a circular or approximately circular geometry in cross-section. Like the outer container 2, the inner container 6 is designed to be rotationally symmetrical with respect to the axis of symmetry M1. The inner container 6 is completely enclosed by the outer container 2. An evacuated gap or intermediate space 12 is provided between the outer container 2 and the inner container 6.

(9) The transport container 1 further comprises a cooling system 13 (FIG. 2) with a coolant container 14. The intermediate space 12 is also provided between the coolant container 14 and the outer container 2. As mentioned above, the intermediate space 12 is evacuated. The intermediate space 12 completely envelops the inner container 6 and the coolant container 14.

(10) A cryogenic fluid, such as nitrogen N2, is received in the coolant container 14. Hereafter, the cryogenic fluid is therefore referred to as nitrogen N2. The coolant container 14 comprises a tubular or cylindrical base section 15, which can be designed to be rotationally symmetrical with respect to the axis of symmetry M1. The base section 15 can have a circular or approximately circular geometry in cross-section. The base section 15 is closed at the end face by a cover section 16, 17 in each case, and, in particular, by a first cover section 16 and a second cover section 17. The cover sections 16, 17 can be curved. In particular, the cover sections 16, 17 are curved in the same direction. The coolant container 14 can also have a different design. The coolant container 14 is arranged outside the inner container 6, but inside the outer container 2.

(11) A gas zone 18 with vaporized or gaseous nitrogen GN2 and a liquid zone 19 with liquid nitrogen LN2 can be provided in the coolant container 14. Viewed in a direction of gravity g, the gas zone 18 is arranged above the liquid zone 19. The gaseous nitrogen GN2 can also be referred to as the gaseous phase of the nitrogen N2 or of the cryogenic fluid. The liquid nitrogen LN2 can also be referred to as the liquid phase of the nitrogen N2 or of the cryogenic fluid. Viewed in an axial direction A of the transport container 1, the coolant container 14 is arranged next to the inner container 6. The axial direction A is positioned to be parallel to the axis of symmetry M1 or coincides therewith. The axial direction A from the first cover section 4 of the outer container 2 can be oriented in the direction of the second cover section 5 of the outer container 2. A gap or an intermediate space 20, which can be part of the intermediate space 12, is provided between the inner container 6—in particular, between the second cover section 11 of the inner container 6—and the coolant container 14—in particular, the first cover section 16 of the coolant container 14. This means that the intermediate space 20 is likewise evacuated.

(12) The transport container 1 furthermore comprises a thermal shield 21 associated with the cooling system 13. The thermal shield 21 is arranged in the evacuated intermediate space 12 provided between the inner container 6 and the outer container 2. The thermal shield 21 is actively coolable or is actively cooled with the aid of the nitrogen N2. In the present case, active cooling is to be understood as meaning that the nitrogen N2 for cooling the thermal shield 21 is conducted through or guided along said thermal shield. Here, the thermal shield 21 is cooled to a temperature which approximately corresponds to the boiling point of the nitrogen N2.

(13) The thermal shield 21 comprises a cylindrical or tubular base section 22, which is closed on both sides by a cover sections 23, 24,—in particular, a first cover section 23 and a second cover section 24—that close the base section at the end face. Both the base section 22 and the cover sections 23, 24 are actively cooled with the aid of the nitrogen N2. The base section 22 can have a circular or approximately circular geometry in cross-section. The thermal shield 21 is preferably likewise designed to be rotationally symmetrical with respect to the axis of symmetry M1.

(14) Viewed in the axial direction A, the second cover section 24 of the thermal shield 21 is arranged between the inner container 6—in particular, the second cover section 11 of the inner container 6—and the coolant container 14—in particular, the first cover section 16 of the coolant container 14. The thermal shield 21—in particular, the second cover section 24 of the thermal shield 21—is a component separate from the coolant container 14. This means that the thermal shield 21—in particular, the second cover section 24 of the thermal shield 21—is not part of the coolant container 14. The intermediate space 12 completely envelops the thermal shield 21.

(15) The first cover section 23 of the thermal shield 21 faces away from the coolant container 14. The first cover section 23 of the thermal shield 21 is arranged between the first cover section 4 of the outer container 2 and the first cover section 10 of the inner container 6. Thereby, the thermal shield 21 is self-supporting. This means that the thermal shield 21 is supported on neither the inner container 6 nor the outer container 2. For this purpose, a support ring can be provided on the thermal shield 21, which is suspended on the outer container 2 via supporting rods—in particular, tension rods. Furthermore, the inner container 6 can be suspended on the support ring via further supporting rods—in particular, tension rods. The heat transfer through the mechanical supporting rods is partially realized by the support ring. The support ring has pockets that allow a largest possible thermal length of the supporting rods. The coolant container 14 can include feedthroughs for the mechanical supporting rods.

(16) The thermal shield 21 is fluid-permeable. This means that a gap or intermediate space 25 between the inner container 6 and the thermal shield 21 is fluidically connected to the intermediate space 12. The intermediate spaces 12, 25 can thus be evacuated at the same time. The intermediate space 25 completely envelops the inner container 6. An insulating element, which is not shown in FIGS. 1 through 3, can be arranged in the intermediate space 25. This insulating element can be or comprise a so-called MLI (multilayer insulation). Boreholes, apertures, or the like can be provided in the thermal shield 21 to allow the intermediate spaces 12, 25 to be evacuated simultaneously. The thermal shield 21 is preferably made of a high-purity aluminum material.

(17) The second cover section 24 of the thermal shield 21 shields the coolant container 14 completely with respect to the inner container 6. This means that, when viewed from the inner container 6 towards the coolant container 14—in particular, when viewed in the axial direction A—the coolant container 14 is completely covered or shielded by the second cover section 24 of the thermal shield 21. In particular, the thermal shield 21 completely surrounds the inner container 6. This means that the inner container 6 is arranged completely within the thermal shield 21, wherein the thermal shield 21 is not fluid-tight, as already mentioned above.

(18) As FIG. 2, in which the inner container 6 is not shown, further shows, the thermal shield 21 comprises at least one cooling line 26 for actively cooling the inner container. The cooling line 26 is associated with the cooling system 13. Preferably, several such cooling lines 26, e.g., six such cooling lines 26, are provided. However, the number of cooling lines 26 is arbitrary. The cooling line 26 can comprise two perpendicular sections 27, 28 extending in the direction of gravity g and two oblique sections 29, 30. The perpendicular sections 27, 28 can be provided on the cover sections 23, 24 and/or on the base section 22 of the thermal shield 21. The oblique sections 29, 30 can likewise be provided on the cover sections 23, 24 and/or on the base section 22. The section 27 is fluidically connected to the section 29, and the section 30 is fluidically connected to the section 28.

(19) The cooling line 26 is connected to the thermal shield 21, both mechanically and thermally. For this purpose, the cooling line 26 can be integrally bonded to the thermal shield 21. In the case of integral bonds, the bonding partners are held together by atomic or molecular forces. Integral bonds are non-releasable connections that can be separated only by destroying the bonding means or the bonding partners. Integral bonding can be achieved, for example, by adhesive bonding, soldering, welding, or vulcanization. The cooling line 26 is, or the cooling lines 26 are, preferably welded, soldered, or adhesively bonded to the thermal shield 21.

(20) The cooling line 26 is fluidically connected to the coolant container 14 with the aid of a connecting line 31 so that, when the coolant container 14 is filled, the nitrogen N2 is pushed from the coolant container 14 into the cooling line 26. The connecting line 31 is part of the cooling line 26. The cooling line 26 may also be directly in connection with the coolant container 14. The connecting line 31 opens into a distributor 32, from which the section 27 and the section 30 of the cooling line 26 branch off. The distributor 32 forms, with respect to the direction of gravity g, a lowest point of the cooling line 26. The distributor 32 can thus also be referred to as the lowest point of the cooling line 26. This lowest point of the cooling line 26 is fluidically connected to the liquid zone 19 of the coolant container 14 with the aid of the connecting line 31. In the process, the connecting line 31 can open into a lowest point, with respect to the direction of gravity g, of the coolant container 14. The section 29 and the section 28 of the cooling line 26 meet at a collector 33, which forms, with respect to the direction of gravity g, a highest point of the cooling line 26. The collector 33 can thus also be referred to as the highest point of the cooling line 26.

(21) As previously mentioned, the cooling lines 26 are provided on both the base section 22 and the cover sections 23, 24 of the thermal shield 21. Alternatively, the cover sections 23, 24 are materially connected to the base section 22 in one piece—in particular, integrally. For example, the cover sections 23, 24 can be welded to the base section 22. Since the cover sections 23, 24 are materially connected to the base section 22 in one piece, i.e., integrally, the cover sections 23, 24 can also be cooled by heat conduction.

(22) The cooling line 26, and, in particular, the oblique sections 29, 30 of the cooling line 26, have an incline with respect to a horizontal H1 which is arranged to be perpendicular to the direction of gravity g and parallel to the axis of symmetry M1. In particular, the oblique sections 29, 30 are inclined in the direction of the coolant container 14. The sections 29, 30 preferably have an angle of inclination α of more than 3° to the horizontal H. The angle of inclination α can be 3° to 15°, or even more. In particular, the angle of inclination α can also be exactly 3°. The angle of inclination α can also be referred to as the first inclination angle. In particular, the sections 29, 30 have a positive incline in the direction of the collector 33, so that gas bubbles arising in the cooling line 26 when the nitrogen N2 boils rise to the collector 33. A phase separator, which is arranged outside the outer container 2, and designed to separate the gaseous nitrogen GN2 from the liquid nitrogen LN2 and to bleed the gaseous nitrogen GN2 into the environment, can be connected to the collector 33. However, such a phase separator is dispensed with here.

(23) An insulating element, which is not shown in FIGS. 1 through 3 and fills the intermediate space 12, can be arranged in the intermediate space 12. This insulating element is provided on the outer side of the thermal shield 21 and can fill the intermediate space 12. The insulating element preferably completely fills the intermediate space 12 in the region of the inner container 6, so that the insulating element makes contact there with the thermal shield 21 on the outside, and with the outer container 2 on the inside. The insulating element encloses the thermal shield 21, except for the second cover section 24 thereof, i.e., it encloses the first cover section 23 and the base section 22. Furthermore, the cylindrical base section 15 and the second cover section 17 of the coolant container 14 are enclosed by the insulating element. The insulating element is preferably likewise a so-called MLI, or can comprise an MLI. Like the thermal shield 21, the insulating element can be actively cooled. The active cooling takes place with the aid of the cryogenic gaseous nitrogen GN2. For the active cooling of the insulating element, a further cooling line can be led through it. The cooling line can be helical or spiral-shaped.

(24) Furthermore, the transport container 1 comprises at least one return line 34, 35 (FIG. 3). Preferably, a first return line 34 and a second return line 35 are provided. However, the number of return lines 34, 35 is arbitrary. With the aid of the return lines 34, 35, the cooling line 26 is, or the cooling lines 26 are, fluidically connected to the coolant container 14, in order to return the nitrogen N2 to the coolant container 14 again after passage through the cooling line 26 or the cooling lines 26. The return lines 34, 35 can be provided on the outer side of the thermal shield 21. The return lines 34, 35 are at least mechanically connected to the thermal shield 21 and are preferably arranged between the thermal shield 21 and the outer container 2. Alternatively, the return lines 34, 35 can also be thermally connected to the thermal shield 21.

(25) The return lines 34, 35 are inclined in the direction of the coolant container 14. In particular, the return lines 34, 35 are inclined at an angle of inclination β relative to a horizontal H2. The horizontal H2 is arranged to be parallel to the horizontal H1 or coincides therewith. The angle of inclination β can also be referred to as the second angle of inclination. The angle of inclination β can be 4°, for example. The angle of inclination β can be 4° to 15°, or even more. In particular, the angle of inclination β can also be exactly 4°. The return lines 34, 35 are preferably associated with the cooling system 13.

(26) Unlike the cooling line 26 or the cooling lines 26, which are fluidically connected to the liquid zone 19 of the coolant container 14, the return lines 34, 35 are fluidically connected to the gas zone 18 of the coolant container. This means that, with respect to the direction of gravity g, the cooling lines 34, 35 open into the coolant container 14 above the cooling line 26, and, in particular, above the connecting line 31 of the cooling line 26. The collector 33, which represents the highest point of the cooling line 26, is fluidically connected to the coolant container 14 with the aid of the return lines 34, 35. For this purpose, such a collector 33 can be provided on, for example, both sides of the thermal shield 21. The return lines 34, 35 preferably run parallel to one another. Here, an inside diameter d34, d35 of the return lines 34, 35 is larger than an inside diameter d26 of the cooling line 26. The inside diameter d26 of the cooling line 26 is preferably larger than 10 millimeters. The inside diameter d26 can be 12 millimeters, for example.

(27) The cooling system 13 further comprises a bleed valve 36, with the aid of which the gaseous nitrogen GN2 can, depending upon the pressure, be bled off from the coolant container 14. The bleed valve 36 is suitable for bleeding off the gaseous nitrogen GN2 to the environment. Alternatively, the aforementioned, actively-cooled insulating element, which is arranged between the outer container 2 and the thermal shield 21, can be connected to the bleed valve 36. Bled off cryogenic gaseous nitrogen GN2 is then conducted through the insulating element to actively cool it. The gaseous nitrogen GN2 heated in the process can then be discharged into the environment after passing through the cooling line of the insulating element. Since the gaseous nitrogen GN2 is then no longer cryogenic, but heated, when exiting the insulating element, undesirable icing of the exit site can be prevented.

(28) The operating principle of the transport container 1 will be explained below. Before filling the inner container 6 with helium He, the thermal shield 21 is first cooled at least approximately or completely to the boiling point (1.3 bara, 7.95 K) of the liquid nitrogen LN2 with the aid of cryogenic nitrogen N2, which initially is gaseous, and later liquid. The inner container 6 is not yet actively cooled. As the thermal shield 21 cools, the residual vacuum gas still present in the intermediate spaces 12, 20, 25 is frozen out at the thermal shield 21. As a result, when the inner container 6 is filled with the helium He, the residual vacuum gas can be prevented from freezing out on, and thus contaminating, the inner container 6. As soon as the thermal shield 21 and the coolant container 14 are completely cooled, and the coolant container 14 is completely filled with nitrogen N2 again, the inner container 6 is filled with the liquid helium He.

(29) The transport container 1 can now be moved onto a transport vehicle, such as a truck or a ship, for transporting the helium He. In the process, the thermal shield 21 is continuously cooled with the aid of the liquid nitrogen LN2. The liquid nitrogen LN2 boils in the cooling line 26 or in the cooling lines 26. Gas bubbles formed in the process are supplied as gaseous nitrogen GN2 to the highest point of the cooling system 13, viz., the collector 33. It is always ensured, in the process, that the cooling line 26 is, or the cooling lines 26 are, supplied with liquid nitrogen LN2 across the entire length thereof, and thereby has or have a temperature corresponding approximately to the boiling point of the nitrogen N2.

(30) The gas bubbles entrain liquid nitrogen LN2 from the cooling line 26 or from the cooling lines 26 and thus convey it into the return lines 34, 35. The liquid nitrogen LN2 is entrained by the resulting gas bubbles to a static height of approximately two meters. This results, not in continuous, but in discontinuous conveyance of the liquid nitrogen LN2. The liquid nitrogen LN2 is conveyed in a surge-like manner or by way of surges. The liquid nitrogen LN2 conveyed into the return lines 34, 35 and the gaseous nitrogen GN2 are returned to the coolant container 14 via the return lines 34, 35. The liquid nitrogen LN2 partially vaporizes in the return lines 34, 35. Non-vaporized fractions of the liquid nitrogen LN2 fall back into the coolant container 14. Since the return lines 34, 35 have a larger inside diameter d34, d35 than the cooling line 26, the entrained liquid nitrogen LN2 can be conveyed freely into the return lines 34, 35.

(31) This results in a natural circulation of the nitrogen N2. This means that the nitrogen N2 is conveyed in a circuit by the cooling line 26, or the cooling lines 26, and the return lines 34, 35 without a pump that has movable parts.

(32) The liquid nitrogen LN2 is conveyed only with the aid of the gaseous nitrogen GN2. The cooling line 26 or the cooling lines 26 and the return lines 34, 35 act as a so-called bubble pump or mammoth pump, which is suitable for conveying the liquid nitrogen LN2. This previously described, natural circulation functions without, or at least nearly without, overpressure. The pressure in the coolant container 14 can thus be lowered from the usually required 1.3 bara to 1.1 bara. This reduction of pressure in the coolant container 14 results in a decrease in the boiling temperature of the liquid nitrogen LN2 by 1.5 K. The heat transferred to the helium He is thereby reduced by approximately 5%, so that the helium holding time increases significantly, viz., by approximately three days, compared with an arrangement without such return lines 34, 35.

(33) In the case of the transport container 1, it is, advantageously, possible to dispense with a phase separator for separating the liquid nitrogen LN2 from the gaseous nitrogen N2. Such a phase separator comprises moving components, which are subject to wear. This means that the phase separator has a limited service life. By dispensing with a phase separator, the costs both for producing and for maintaining such a transport container 1 are thus reduced. Furthermore, by dispensing with the phase separator, which is usually arranged on the outer side of the outer container 2 as an additional component, damage to the phase separator is also ruled out. Handling of the transport container 1 is thereby simplified. The heat transfer into the cooling system 13 caused by the phase separator is also not negligible. For this reason as well, dispensing with the phase separator is advantageous.

(34) Because cryogenic gaseous nitrogen is discharged only at one location, viz., at the bleed valve 36, the active cooling of the insulating element arranged between the thermal shield 21 and the outer container 2 is easier to implement, since only one cooling line has to be run. If such an actively-cooled insulating element is provided, only heated gaseous nitrogen GN2 leaves the transport container 1, so that, in addition to the drastically increased holding time for the liquid nitrogen LIN2, no undesirable icing of the transport container 1 can occur, as already mentioned above.

(35) Although the present invention has been described on the basis of exemplary embodiments, it can be modified in a variety of ways.

REFERENCE SYMBOLS USED

(36) 1 Transport container 2 Outer container 3 Base section 4 Cover section 5 Cover section 6 Inner container 7 Gas zone 8 Liquid zone 9 Base section 10 Cover section 11 Cover section 12 Intermediate space 13 Cooling system 14 Coolant container 15 Base section 16 Cover section 17 Cover section 18 Gas zone 19 Liquid zone 20 Intermediate space 21 Thermal shield 22 Base section 23 Cover section 24 Cover section 25 Intermediate space 26 Cooling line 27 Section 28 Section 29 Section 30 Section 31 Connecting line 32 Distributor 33 Collector 34 Return line 35 Return line 36 Bleed valve A Axial direction d26 Inside diameter d34 Inside diameter d35 Inside diameter g Direction of gravity GN2 Nitrogen H1 Horizontal H2 Horizontal He Helium LN2 Nitrogen L2 Length M1 Axis of symmetry N2 Nitrogen α Angle of inclination β Angle of inclination