HELICALLY COILED HEAT EXCHANGER

Abstract

The invention relates to a heat exchanger for indirect heat exchange between a first and a second medium, with a shell space for receiving the first medium, and a tube bundle arranged in the shell space and for receiving the second medium. The tubes are helically wound in a number of tube layers onto a core tube. At least one spacer is provided by means of which a first tube layer that is situated further outwards in the radical direction is supported on a neighbouring, second tube layer that is situated further inwards. The at least one spacer has a flow-directing region designed to deflect part of the first medium flowing along a tube of the first tube layer in the direction of the second tube layer situated further inwards in the radical direction.

Claims

1. A heat exchanger (1) for the indirect exchange of heat between a first and a second medium (S, S), having a shell space (M) for accommodating the first medium (S), a tube bundle (2) which is arranged in the shell space (M) and which has a plurality of tubes (20) for accommodating the second medium (S), wherein the respective tube (20) is helically coiled onto a core tube such that the tube bundle (2) has multiple tube layers (201, 202, 203) arranged one on top of the other, and at least one spacer (6), via which a first tube layer (201) of the tube bundle (2) situated further outward in the radial direction (R) of the tube bundle (2) is supported against an adjacent second tube layer (202) situated further inward in the radial direction (R) of the tube bundle (2), characterized in that the at least one spacer (6) has a flow-guiding means (6a) which is configured to divert a part of the first medium (S), which part flows along the first tube layer (201) in the shell space (M), into the direction of the second tube layer (202) situated further inward in the radial direction (R).

2. The heat exchanger as claimed in claim 1, characterized in that the means (6a) has an end side (6a) of the spacer (6), which end side connects a front side (6b), averted from the core tube (21), of the spacer (6) to a rear side (6c), facing the core tube (21), of the spacer (6).

3. The heat exchanger claim 2, characterized in that the end side (6a) has an inclination toward the second tube layer (202) such that a part of the first medium (S), which part flows along the tube (20) of the first tube layer (201) and against the end side (6a), is diverted by the end side (6a) into the direction of the second tube layer (202).

4. The heat exchanger as claimed in claim 1, characterized in that the means (6a) has at least one guiding element (62) which is fixed to a base (60) of the spacer (6), which base extends along the longitudinal axis (L) and via which base the first tube layer (201) is supported against the second tube layer (202).

5. The heat exchanger as claimed in claim 4, characterized in that the at least one guiding element (62) forms an impact surface (6a) which has an inclination toward the second tube layer (202) such that a part of the first medium (S), which part flows along the tube (20) of the first tube layer (201) and against the impact surface (6a), is diverted by the impact surface (6a) into the direction of the second tube layer (202).

6. The heat exchanger as claimed in claim 4, characterized in that the at least one guiding element (62) extends sectionally between adjacent tube sections of the second tube layer (202).

7. The heat exchanger as claimed in claim 4, characterized in that the at least one guiding element (62) is, in relation to the flow direction of said part of the first medium (S), arranged on an edge section (60a) of the spacer (6), which section is situated upstream or downstream.

8. The heat exchanger as claimed in claim 1, characterized in that the core tube (21) extends along a longitudinal axis (L).

9. The heat exchanger as claimed in claim 8, characterized in that the heat exchanger (1) has a shell (10) which surrounds the shell space (M) and which extends coaxially with respect to the core tube (21) along the longitudinal axis (L).

10. The heat exchanger as claimed in claim 8, characterized in that the at least one spacer (6) and/or said means (6a) extends along the longitudinal axis (L).

11. The heat exchanger as claimed claim 1 insofar as, characterized in that said means (6a) is configured to divert a part of the first medium (S), which part flows along the first tube layer (201) from the top downward, into the direction of the second tube layer (202).

12. The heat exchanger as claimed in claim 1, characterized in that the means has a plurality of channels (6a) which are provided in the at least one spacer (6) and which are configured to divert a part of the first medium (S), which part flows along the first tube layer (201) from the top downward, into the direction of the second tube layer (202).

13. The heat exchanger as claimed in claim 1, characterized in that the heat exchanger (1) has a plurality of spacer elements (6) between the first and the second tube layer (201, 202), wherein the spacer elements (6) each have a flow-guiding means (6a) which is configured to divert a part of the first medium (S), which part flows along the first tube layer (201) in the shell space (M), into the direction of the second tube layer (202) situated further inward in the radial direction (R).

14. The heat exchanger as claimed in claim 1, characterized in that the heat exchanger (1) has spacer elements (6) between multiple or between all the adjacent tube layers (201, 202, 203) of the heat exchanger (1), wherein the respective spacer element (6) has a flow-guiding means (6a) which is configured to divert a part of the first medium (S), which part flows along a tube layer (201) of the in each case adjacent tube layers (201, 202), which layer is situated further outward in the radial direction (R) of the tube bundle (2), in the shell space (M), into the direction of that tube layer (202) of the two adjacent tube layers (201, 202) which is situated further inward in the radial direction (R).

15. The heat exchanger as claimed in claim 14, characterized in that the number of spacers (6) arranged between the adjacent tube layers (201, 202, 203) is constant, wherein in each case multiple spacers (6) are arranged one on top of the other in a radial direction (R) of the tube bundle (2) for the purpose of supporting the tube layers (201, 202, 203).

Description

[0029] Further details and preferences of the invention are explained by the following descriptions of figures of exemplary embodiments on the basis of the figures.

[0030] In the figures:

[0031] FIG. 1 shows a partially sectional view of a helically coiled heat exchanger according to the invention with flow-influencing spacers;

[0032] FIG. 2 shows an embodiment of the spacers according to the invention, with the respective spacer having an inclined end side for diverting the first medium;

[0033] FIG. 3 shows a further embodiment of the spacers according to the invention, with the respective spacer having a guiding element for diverting the first medium;

[0034] FIG. 4 shows a modification of the embodiment shown in FIG. 3; and

[0035] FIG. 5 shows a further embodiment of spacers according to the invention, which have channels for diverting the first medium.

[0036] FIG. 1 shows a helically coiled heat exchanger 1. This has a shell 10 which encloses a shell space M of the heat exchanger 1. The shell 10 extends along a vertical longitudinal or cylinder axis L and surrounds a tube bundle 2 which is arranged in the shell space M and which, in relation to the longitudinal axis L, is to be acted on by a fluid first medium S from above such that said medium to come into indirect heat-exchanging contact with at least one second medium S conducted in the tube bundle 2. Here, the tube bundle 2 is formed from multiple tubes 20, which are each helically coiled around a core tube 21 such that the tube bundle has multiple tube layers 201, 202, . . . arranged one on top of the other in the radial direction R of the tube bundle 2 (cf. FIGS. 2 to 4). In this case, the core tube 21 extends coaxially with respect to the shell 10, wherein the radial direction R of the tube bundle 2 is perpendicular to the longitudinal axis L or the core tube 21 and points outward to the shell 10.

[0037] The tube layers 201, 202, . . . thus formed and arranged one on top of the other in the radial direction R of the tube bundle 2 are supported against one another via spacers 6, which extend along the longitudinal axis L and which are preferably formed as webs, such that the loads of the tube layers 201, 202, . . . are introduced into the core tube 21 via the spacers 6. Furthermore, the tube bundle 2 may be surrounded by a so-called jacket 3 in order to prevent the first medium S from being able to flow past the tube bundle 2 on the outside. The first medium S may, for example, be fed into the shell space M via a connecting piece 101 provided laterally on the shell 10, and extracted from the shell space M via a further connecting piece 102 provided laterally on the shell 10. For the most uniform possible distribution of the first medium S over a top side O of the tube bundle 2, which top side extends transversely with respect to the longitudinal axis L, it is possible for a distribution device (not shown in more detail here), for example of a known type, to be provided in the shell space M above the tube bundle 2. Furthermore, the second medium S conducted in the tube bundle 2 may be introduced into the tube bundle 2 via a connecting piece 103 provided on the shell 10, and extracted from the tube bundle 2 via a further connecting piece 105 provided on the shell 10. For the case that multiple media are to be conducted in the tube bundle 2, the tubes 20 may be gathered into corresponding groups 104, which groups then each conduct one of the media.

[0038] Owing to the above-mentioned effects, it is possible even in the case of a uniform distribution of the first medium S over the top side O of the tube bundle 2 for a non-uniform distribution of the first medium S in the radial direction R of the tube bundle 2 to occur.

[0039] In order to counteract said non-uniform distribution, it is provided according to the invention that the heat exchanger 1 has at least one spacer 6 via which a first tube layer 201 situated further outward in the radial direction R of the tube bundle 2 is supported against a second tube layer 202 situated further inward in the radial direction R, wherein the spacer 6 has a flow-guiding means 6a which is configured to divert a part of the first medium S, which part flows along a tube 20 of the first tube layer 201 in the shell space M, into the direction of the further inwardly situated second tube layer 202.

[0040] As per the exemplary embodiment shown in FIG. 2, said means 6a is for example an end side 6a of the spacer 6, which end side connects a front side 6b, averted from the core tube 21, of the spacer 6 to a rear side 6c, facing the core tube 21, of the spacer 6, wherein said end side 6a has an inclination toward the second tube layer 202 such that that part of the first medium S which flows along the tube 20 of the first tube layer 201 and against the end side 6a is diverted by the end side 6a into the direction of the second tube layer 202. The inclination of the end side 6a in relation to the first tube layer 201 is in this case characterized by an acute angle W which the second end side 6a includes with the second tube layer 202 or with those tube sections of the second tube layer 202 which are adjacent to the spacer 6.

[0041] Preferably, a plurality of spacers 6 of the above-described type is provided between in each case two adjacent tube layers 201, 202, . . . , wherein the number of spacers 6 arranged between two tube layers 201, 202, . . . is preferably constant and the spacers 6 from different tube layers are preferably arranged one on top of the other in the radial direction R in order that the load of the tube layers 201, 202, . . . arranged one on top of the other can be reliably dissipated to the core tube 21 via the spacers 6.

[0042] As is further shown in FIG. 2, the tubes 20 in the tube layers 201, 202, . . . may have a different coiling direction. The result of this is that it is possible for the first medium S to flow in a different direction in the adjacent tube layers 201, 202 along the respective tube 20. The end side 6a of the respective spacer 6 is then oriented such that the respective part of the first medium S which is to be diverted inward flows against the respective end side 6a.

[0043] As is further shown in FIG. 2, it is possible for the at least one or the respective spacer 6 to have projections 61 which project outward in the radial direction R from an edge section of a base 60 of the respective spacer 6. Said projections 61 serve for establishing a desired vertical spacing of the tube coils in the respective tube layer. Furthermore, the projections 61 may form a part of the end side 6a of the respective spacer 6. The end side 6a of the respective spacer 6 may therefore be arranged at least sectionally between the adjacent tube sections of the in each case further outwardly situated tube layer 201.

[0044] FIG. 3 shows a further embodiment of the invention, in which the at least one spacer 6 has at least one guiding element 62, for example in the form of a baffle plate, which is fixed to a (for example web-like) base 60 of the at least one spacer 6, which base extends along the longitudinal axis L, wherein it is preferably the case here that the base 60 performs the load-dissipating function, that is to say the in each case further outwardly arranged (first) tube layer 201 is supported via said base 60 against the (second) tube layer 202 situated therebelow, while the guiding element 62 preferably performs the flow-guiding or flow-diverting function and forms said means 6a of the spacer 6, which here is formed as an impact surface 6a of the guiding element 62, said surface having an inclination toward the (second) tube layer 202 situated further inward in the radial direction R (or an inclination in relation to the adjacent tube sections of the second tube layer 202), such that that part of the first medium S which flows along the tube 20 of the first tube layer 201 and against the impact surface 6a is diverted by the impact surface 6a into the direction of the further inwardly situated (second) tube layer 202. Owing to the inclination, the impact surface 6a of the guiding element 62 includes an acute angle W with the in each case radially further inwardly situated (second) tube layer 202.

[0045] The guiding element 62 may be a separate element which is fixed to the base 60 of the respective spacer 6, specifically preferably to an end side 60a of the base 60, which end side connects a rear side, which faces the core tube 21 and against which the further inwardly situated (second) tube layer 202 bears, to a front side of the base 60, against which front side the further outwardly situated (first) tube layer 201 bears. However, the guiding element 62 may also be formed integrally with the base 60 (from one piece).

[0046] Analogously to FIG. 2, it is also possible, as per FIG. 3, for a plurality of spacers 6 to in turn be provided, wherein the spacers 6 from different tube layers are preferably arranged one on top of the other in the radial direction R (see above).

[0047] Furthermore, FIG. 3 also shows a situation in which the flow direction of that part of the first medium S which flows along the tube 20 of the respective tube layer 201, 202, . . . is different from tube layer to tube layer owing to the coiling direction of the respective tube 20, wherein, as per FIG. 3, it is preferably provided that the respective guiding element 62 is, in relation to the flow direction of that part of the first medium S which is to be diverted, provided on, or fixed to, an end side 60a of the base 60 of the respective spacer 6, which end side is situated downstream. In this case, said impact surface 6a in particular faces the respective base 60 and ensures in particular a diversion of a part of the first medium S after said part has passed the respective base 60 on the rear side of the respective base 60.

[0048] FIG. 4 shows a modification of the guiding elements 62, wherein here, in contrast to FIG. 3, the guiding elements 62 are each provided on an end side 60a of the base 60 of the respective spacer 6, which end side is situated upstream, and wherein here the impact surface 6a of the respective guiding element 62 is averted from the associated base 60 and has, in relation to the in each case further inwardly situated (second) tube layer 202, an inclination such that it includes an acute angle W with said tube layer.

[0049] Both in the embodiment as per FIG. 3 and in the embodiment as per FIG. 4, it is preferably provided that the guiding element 62 of the respective spacer 6 extends sectionally between adjacent tube sections of the in each case further inwardly situated tube layer 202. Instead of a guiding element 62, it is possible in both embodiments (FIG. 3 and FIG. 4) for the respective spacer 6 also to have a corresponding plurality of guiding elements 62, which then in each case project into the intermediate space between two adjacent tube sections of the in each case further inwardly arranged tube layer 202, . . . .

[0050] Finally, FIG. 5 shows an embodiment of spacers 6 according to the invention, which, as before, are arranged between adjacent tube layers 201, 202, . . . of the heat exchanger 1 (see above), wherein here the flow-guiding means 6a is formed by channels 6a (or has such channels), which are each configured to divert a part of the first medium S, which part flows along the first or outer tube layer 201 from the top downward, into the direction of the second or radially further inwardly situated tube layer 202. For this purpose, said channels preferably descend to the further inwardly situated (second) tube layer 202. The channels 6a may be provided for example on an end side 60a of the respective spacer 6 or a base of the respective spacer 6. The spacers 6 may also in turn have projections 61 which project from the respective base 60 in the radial direction R and which define a vertical spacing of adjacent tube coils or adjacent tube sections of the tubes 20 in the direction of the longitudinal axis L of the shell.

[0051] The spacers 60 may only have said channels 6a as flow-guiding means. However, said channels 6a may also be present in the spacers 6 of FIGS. 1 to 4 as additional flow-guiding components.

TABLE-US-00001 List of reference signs 1 Helically coiled heat exchanger 2 Tube bundle 3 Jacket 6 Spacer 6a Means (for example end side, impact surface, channel) 6b Front side 6c Rear side 10 Shell 20 Tubes 21 Core tube 60 Base 61 Projection 62 Guiding element 60a End side of base 101, 102, 103, 105 Connecting piece 104 Tube group 201, 202 Adjacent tube layers M Shell space O Top side S First medium .sup.S Second medium R Radial direction L Longitudinal axis (vertical) W Angle