EP0523039B1 - Unloaded heat exchanger tube sheet - Google Patents

Unloaded heat exchanger tube sheet Download PDF

Info

Publication number
EP0523039B1
EP0523039B1 EP90908144A EP90908144A EP0523039B1 EP 0523039 B1 EP0523039 B1 EP 0523039B1 EP 90908144 A EP90908144 A EP 90908144A EP 90908144 A EP90908144 A EP 90908144A EP 0523039 B1 EP0523039 B1 EP 0523039B1
Authority
EP
European Patent Office
Prior art keywords
connecting member
shell
heat exchanger
tube sheet
membrane
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.)
Expired - Lifetime
Application number
EP90908144A
Other languages
German (de)
French (fr)
Other versions
EP0523039A1 (en
Inventor
Sune Malm
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP0523039A1 publication Critical patent/EP0523039A1/en
Application granted granted Critical
Publication of EP0523039B1 publication Critical patent/EP0523039B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/22Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/0236Header boxes; End plates floating elements
    • F28F9/0241Header boxes; End plates floating elements floating end plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00Safety or protection arrangements; Arrangements for preventing malfunction
    • F28F2265/26Safety or protection arrangements; Arrangements for preventing malfunction for allowing differential expansion between elements

Definitions

  • the present invention relates to a heat exchanger having a heat exchanger vessel with a shell and, disposed inside the shell, at least one tube sheet to which a number of heat exchanger tubes are connected and whose edge portion is sealingly connected to the shell.
  • the invention more specifically relates to an arrangement in which the tube sheet is connected to the shell by means of a flexible connecting member.
  • the tube sheet In a conventional heat exchanger, the tube sheet (or tube sheets, since there generally are two such sheets) normally has the largest wall thickness of the construction. The reason for this is that the tube sheet edge portion fixed to the shell is subjected to substantial loads as a result of differences in thermal expansion between the shell and the tubes mounted in the tube sheet. Moreover, the edge portion of the tube sheet must be capable of withstanding pressure from one side. The load of such a pressure, which may be an external pressure or an internal pressure, is taken up in the form of bending stresses in the edge portion of the tube sheet, which necessitates a considerable wall thickness of the tube sheet.
  • Patent Specification US-A-1,876-401 describes a heat exchanger as defined in the preamble clause of claim 1, the connecting member being a highly flexible gasket and comprising circular sections having associated circle centres on alternate sides of the connecting member.
  • the connecting member generally operates as a bellows means.
  • the object of the present invention is to provide a heat exchanger of the type stated in the introduction to this specification, which substantially overcomes the problems discussed above, while simultaneously yielding further essential advantages in constructional respects.
  • a heat exchanger having a heat exchanger vessel with a shell and, disposed inside the shell, at least one tube sheet to which a number of heat exchanger tubes are connected and whose edge portion is sealingly connected to the shell by means of a flexible connecting member, such that thermal expansion between the shell and the tube sheet can be taken up as bending of the connecting member which is designed as part of a toroid having a cross-section of arched configuration, said heat exchanger, being characterised in that the connecting member is in the form of a thin membrane shell of metallic material, generally steel and preferably stainless steel, and of continuous curvature, said membrane shell having substantially the shape of a quarter circle, at least in the unloaded state, such that loads deriving from pressure differences across the connecting member can be taken up as general membrane stresses in the connecting member.
  • the quarter-circle shape imparts to the connecting member the essential property of being able to withstand substantially the same pressure exerted from one side, against either the concave or the convex side thereof, while also ensuring good resilience. Further, this construction entails economy of material.
  • the connecting member arrangement according to the invention means that thermal expansion can readily be taken up as bending of the pliable connecting member, while at the same time pressure exerted from one side can be taken up as general membrane stresses well distributed over the membrane of the connecting member.
  • general membrane stresses as used herein has the current meaning adopted in the art.
  • the arrangement according to the invention makes it possible to cope with thermal displacement and pressure loads from one side without the occurrence of any major forces or moments in the construction.
  • the tube sheet itself will not be subjected to any substantial forces or moments from its edge portion. It can therefore be made much thinner than the tube sheets of conventional constructions.
  • the thickness of the tube sheet can be reduced down to 10-20% of normal thickness. This reduction in thickness by up to 90% entails very substantial cuts of the costs for material and, in many cases, also of the manufacturing costs.
  • the tube sheet is thin, the holes made in it for mounting the tubes can be punched instead of drilled.
  • the number of tubes mostly being very large, this means that the operation of forming holes in the tube sheet is highly facilitated and becomes considerably less costly.
  • the thin, shell-like connecting member can easily be fixed to the edge of the tube sheet and to the shell of the heat exchanger vessel, e.g. by welding.
  • the connecting member can also be designed as a continuous extension of the tube sheet or a part of the shell, in which case such an extension may have a tube sheet or shell wall thickness reduced to a suitable extent. Integrating the connecting member with the tube sheet or the shell wall permits using highly simplified and less expensive manufacturing techniques.
  • the invention also yields a very compact construction with a small gap between the edge of the tube sheet and the shell wall, which means that the interior of the heat exchanger can be utilised more efficiently.
  • the connecting member according to the invention preferably has a uniform thickness throughout its membrane surface.
  • the connecting member may of course comprise special edge fixing means for fixing to the tube sheet and to the shell.
  • a stiffening ring or flange can be provided at the edge of the tube sheet outside the tubes. This ring or flange may be rigidly or elastically fixed to the tube sheet. It may also form a continuous extension of the tube sheet.
  • Fig. 1 is a schematic, vertical longitudinal section of a horizontal heat exchanger including an arrangement according to the invention.
  • Fig. 2 is a schematic part-sectional view showing an embodiment of a connecting member according to the invention.
  • Figs 3-9 are views similar to Fig. 2, but illustrating alternative embodiments of a connecting member according to the invention.
  • Fig. 1 schematically shows a vertical longitudinal section of a horizontal heat exchanger incorporating an connecting member arrangement according to the invention.
  • the heat exchanger comprises in conventional manner a cylindrical shell 1; two bonnets 2 and 3 fixed to the shell by means of flange joints 5; two tube sheets 7, 8, the planes of which are perpendicular to the axis of the shell 1 and which are disposed at each end of the shell; tubes 9 fixed in holes in the tube sheets and extending between the tube sheets parallel to the axis of the shell; baffles 11, 12, 13 parallel to the tube sheets 7, 8 and distributed along the tubes 9; an inlet 15 at the top of the shell 1 at one side thereof for supplying a first heat exchanger fluid; an outlet 17 at the bottom of the shell at the other side thereof for evacuating the first heat exchanger fluid; an inlet 19 centrally disposed in the bonnet 3 for supplying a second heat exchanger fluid to pass through a first set of tubes 9 to the space inwardly of the bonnet 2; and an outlet 21 disposed at the bottom
  • the central baffle 12 is fixed to the shell, and the tubes 9 in turn are fixed to the baffle 12 at the point where they pass through it.
  • the baffles 11 and 13 are fixed to the baffle 12 by means of spacer rods 25, but are movable relative to the shell.
  • the tubes 9 pass through holes in the baffles 11 and 13, these holes being slightly larger than the tubes, such that the tubes 9 and the baffles 11 and 13 are movable in relation to each other.
  • the baffles 11, 12, 13 do not extend over the entire circular cross-section and are so alternatingly adjoining the shell 1 that the first heat exchanger fluid is caused to follow an alternating downward and upward flow path about the tubes 9, as indicated by the arrows 27.
  • the second heat exchanger fluid is supplied to the first limited set of tubes 9 from the inlet 19 by means of a tubular duct 26.
  • This consists of two telescopic tube parts 29, 30.
  • the part 29 is connected to the inlet 19, and the part 30 is connected to the tube sheet, around the associated tubes.
  • the part 29 can be displaced within the part 30 in connection with thermally-conditioned displacements of the tube sheet 8, a seal 31 ensuring adequate sealing with respect to the space inwardly of the bonnet 3.
  • the seal 31 may be a simple gland-type seal, since the pressure exerted across it does not exceed the pressure drop of the second heat exchanger fluid during its passage through the tubes 9.
  • the flow path of the second heat exchanger fluid is indicated by the arrows 28.
  • Figs 2-9 all schematically illustrate the provision of a metallic, shell-like connecting member 23, viz. in an enlarged partial section taken along a diameter, parallel to the axis of the shell 1.
  • the section is taken at right angles to the centre axis of the connecting member 23 designed as a shell portion of an annular toroid.
  • the connecting member 23 is a thin membrane shell of metal having the cross-sectional shape of a quarter circle, i.e. a 90° circular arc (in the unloaded state).
  • the edges of the membrane shell are extended and fixed to the lower, i.e. "outer" edge surface 31 (in the Figure) of the tube sheet 8 and to the inner surface of the shell 1. Said edges are connected tangentially both to the inner surface of the shell 1 and to the tube sheet 8.
  • the connection is performed by welding, as shown in the respective Figures.
  • the membrane shell is located below the plane of the tube sheet 8, i.e. on the outside thereof.
  • An “external” pressure exerted from one side is readily taken up as membrane stresses, as indicated by arrows 33.
  • an "internal" pressure from one side can just as easily be taken up as membrane stresses thanks to the configuration of the membrane shell.
  • the membrane shell is connected orthogonally both to the tube sheet 8 and to the shell 1, and the extended fixing portion 37 of the membrane shell 23 is connected tangentially to a shell flange 5 and provided with a gasket 39 on its underside.
  • the fixing portion of the membrane shell at the tube sheet 8 is extended so as to project on the opposite side of the tube sheet 8.
  • the thus projecting portion 35 has been found to improve the mounting strength and stability.
  • the membrane shell 23 and the extended portion 35 thereof are welded to the edge of the tube sheet 8 at its upper and lower side, respectively.
  • An "internal" pressure exerted from one side is indicated by arrows 34.
  • Fig. 4 shows an embodiment of the same general type as that in Fig. 2, but the connecting member 23 here is a continuous extension of the tube sheet 8.
  • This extension has a reduced wall thickness and protrudes from the upper side (i.e. "inner side") of the tube sheet 8.
  • the free end surface 41 of the tube sheet is concave in conformity with the curvature of the membrane shell 23 so as to provide a smooth transition. In this manner, it is possible to avoid detrimental stress concentrations.
  • the opposite end of the membrane shell 23, which is welded to the shell 1 is thickened by the curvature of the membrane shell continuing a slight distance after the 90° arc.
  • the weld joint 43 is located in the plane of the inner wall of the shell 1.
  • Fig. 5 shows an embodiment which is analogous with that of Fig. 2, although it is here a matter of an "internal" pressure exerted from one side.
  • the curvature or arch of the membrane shell 23 thus is reversed, facing downwards, i.e. outwards.
  • the pressure thus acts within the concave, arched membrane shell to achieve the optimum membrane stress effect.
  • the membrane shell according to the invention can also take up pressure exerted only from the opposite, convex side.
  • the connecting member 23 here is a continuous extension of the shell 1.
  • the transition to the shell 1 is designed in the same way as the transition to the tube sheet 8 in Fig. 4.
  • the membrane shell 23 is welded to the lower part of the end edge surface.
  • the end edge surface 45 otherwise is concave with a smooth transition from the curvature of the membrane shell 23, whereby to avoid detrimental stress concentrations.
  • Fig. 6 shows an embodiment which is analogous with that of Fig. 1, although modified in two respects.
  • the membrane shell 23 is welded to the lower part of the end edge surface of the tube sheet (as in Fig. 5), and the end edge surface is formed with a continuously connected, circumferential groove 47.
  • an annular cylindrical stiffening ring 49 is rigidly mounted (in this case welded) on the upper side of the tube sheet 8 directly at the circumferential edge of the sheet.
  • the ring 49 projects inwards, i.e. in the opposite direction with respect to the membrane shell 23, orthogonally to the tube sheet 8.
  • Fig. 7 shows an embodiment which is analogous (although reversed) with respect to that of Fig. 3. It is however intended for "internal" pressure and includes a stiffening ring 49 as in Fig. 6.
  • the stiffening ring is however resiliently mounted by being welded to the projecting portion 35 of the membrane shell 23.
  • a circumferential groove 51 eliminating stress concentrations is provided on the underside of the tube sheet 8 in the immediate vicinity of the weld 53 between the tube sheet 8 and the membrane shell 23.
  • the groove 51 and the weld 53 provide a smooth, curved transition between the membrane shell 23 and the tube sheet 8.
  • Fig. 8 shows an embodiment which is analogous with that of Fig. 5, but, additionally, provided with a stiffening ring 49, as in Fig. 6.
  • Fig. 9 shows an embodiment in which the membrane shell 23 is tangentially connected by welding to the shell 1 at one end, while its other end is welded to the free end surface 55 of a fixed stiffening ring 49 projecting downwards from the lower edge portion of the tube sheet 8.
  • the ring does not project at right angles from the tube sheet, but obliquely inwardly towards the centre of the heat exchanger, i.e. away from the shell 1.
  • the lowermost portion 57 of the ring is bent backwards so as to be perpendicular to the plane of the tube sheet 8.
  • An annular concave groove 59 is connected to the upper weld between the membrane shell 23 and the ring portion 57, whereby to avoid detrimental stress concentrations.
  • this arrangement means that the gap 61 between the shell 1 and the edge of the tube sheet 8 can be reduced, thus improving the utilisation of the interior of the heat exchanger.
  • the heat exchanger shown in Fig. 1 uses two movable tube sheets, which entails a horizontal heat exchanger, as well as the illustrated, preferred arrangement of the baffles.
  • Other embodiments are however conceivable within the scope of the inventive concept.
  • Movable baffles are then mounted in conventional manner by means of spacer members in the stationary tube sheet.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

An arrangement in a heat exchanger having a heat exchanger vessel with a shell (1) and, disposed inside the shell, at least one tube sheet (8) to which a number of heat exchanger tubes (9) are connected and whose edge portion is sealingly connected to the shell by means of a flexible connecting member (23). The connecting member is designed as part of a toroid having a cross-section of arched configuration, which exhibits a continuous curvature and has the shape of a quarter circle, such that loads deriving from pressure differences across the connecting member can be taken up in the form of general membrane stresses in the connecting member and such that thermal expansion between the shell and tube sheet can be taken up as bending of the connecting member.

Description

    FIELD OF THE INVENTION
  • The present invention relates to a heat exchanger having a heat exchanger vessel with a shell and, disposed inside the shell, at least one tube sheet to which a number of heat exchanger tubes are connected and whose edge portion is sealingly connected to the shell. The invention more specifically relates to an arrangement in which the tube sheet is connected to the shell by means of a flexible connecting member.
  • BACKGROUND OF THE INVENTION
  • In a conventional heat exchanger, the tube sheet (or tube sheets, since there generally are two such sheets) normally has the largest wall thickness of the construction. The reason for this is that the tube sheet edge portion fixed to the shell is subjected to substantial loads as a result of differences in thermal expansion between the shell and the tubes mounted in the tube sheet. Moreover, the edge portion of the tube sheet must be capable of withstanding pressure from one side. The load of such a pressure, which may be an external pressure or an internal pressure, is taken up in the form of bending stresses in the edge portion of the tube sheet, which necessitates a considerable wall thickness of the tube sheet.
  • With a view to reducing the stresses due to expansion, certain heat exchangers have been provided with expansion bellows in the shell side. Although this means that the problems linked with thermal expansion are overcome, there instead arise other problems in that the load caused by internal overpressure increases.
  • It has also been suggested to connect the tube sheet to the shell by means of a flexible connecting member, such as bellows means or a flat membrane, so as to obviate the expansion problems. This does however not solve the problems of pressure exerted from one side.
  • Patent Specification US-A-1,876-401 describes a heat exchanger as defined in the preamble clause of claim 1, the connecting member being a highly flexible gasket and comprising circular sections having associated circle centres on alternate sides of the connecting member. Thus, the connecting member generally operates as a bellows means.
  • OBJECT OF THE INVENTION
  • The object of the present invention is to provide a heat exchanger of the type stated in the introduction to this specification, which substantially overcomes the problems discussed above, while simultaneously yielding further essential advantages in constructional respects.
  • SUMMARY OF THE INVENTION
  • According to the invention, the object stated above is achieved by a heat exchanger having the features recited in the accompanying claims.
  • According to the invention, there is thus provided a heat exchanger having a heat exchanger vessel with a shell and, disposed inside the shell, at least one tube sheet to which a number of heat exchanger tubes are connected and whose edge portion is sealingly connected to the shell by means of a flexible connecting member, such that thermal expansion between the shell and the tube sheet can be taken up as bending of the connecting member which is designed as part of a toroid having a cross-section of arched configuration, said heat exchanger, being characterised in that the connecting member is in the form of a thin membrane shell of metallic material, generally steel and preferably stainless steel, and of continuous curvature, said membrane shell having substantially the shape of a quarter circle, at least in the unloaded state, such that loads deriving from pressure differences across the connecting member can be taken up as general membrane stresses in the connecting member. The quarter-circle shape imparts to the connecting member the essential property of being able to withstand substantially the same pressure exerted from one side, against either the concave or the convex side thereof, while also ensuring good resilience. Further, this construction entails economy of material.
  • In other words, the connecting member arrangement according to the invention means that thermal expansion can readily be taken up as bending of the pliable connecting member, while at the same time pressure exerted from one side can be taken up as general membrane stresses well distributed over the membrane of the connecting member. The expression "general membrane stresses" as used herein has the current meaning adopted in the art.
  • The arrangement according to the invention makes it possible to cope with thermal displacement and pressure loads from one side without the occurrence of any major forces or moments in the construction. In particular, the tube sheet itself will not be subjected to any substantial forces or moments from its edge portion. It can therefore be made much thinner than the tube sheets of conventional constructions. Typically, it has been found that when using the arrangement according to the invention, the thickness of the tube sheet can be reduced down to 10-20% of normal thickness. This reduction in thickness by up to 90% entails very substantial cuts of the costs for material and, in many cases, also of the manufacturing costs. Thus, since the tube sheet is thin, the holes made in it for mounting the tubes can be punched instead of drilled. The number of tubes mostly being very large, this means that the operation of forming holes in the tube sheet is highly facilitated and becomes considerably less costly.
  • The thin, shell-like connecting member can easily be fixed to the edge of the tube sheet and to the shell of the heat exchanger vessel, e.g. by welding. The connecting member can also be designed as a continuous extension of the tube sheet or a part of the shell, in which case such an extension may have a tube sheet or shell wall thickness reduced to a suitable extent. Integrating the connecting member with the tube sheet or the shell wall permits using highly simplified and less expensive manufacturing techniques. The invention also yields a very compact construction with a small gap between the edge of the tube sheet and the shell wall, which means that the interior of the heat exchanger can be utilised more efficiently.
  • The connecting member according to the invention preferably has a uniform thickness throughout its membrane surface. In addition to the toroid membrane, the connecting member may of course comprise special edge fixing means for fixing to the tube sheet and to the shell. In order to further reduce the loads on the tube sheet in the tubed area and to bridge minor untubed areas at the edge portion of the tube sheet, a stiffening ring or flange can be provided at the edge of the tube sheet outside the tubes. This ring or flange may be rigidly or elastically fixed to the tube sheet. It may also form a continuous extension of the tube sheet.
  • Other features and advantages of the heat exchanger according to the invention will appear from the following description of exemplifying embodiments thereof with reference to the accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Fig. 1 is a schematic, vertical longitudinal section of a horizontal heat exchanger including an arrangement according to the invention. Fig. 2 is a schematic part-sectional view showing an embodiment of a connecting member according to the invention. Figs 3-9 are views similar to Fig. 2, but illustrating alternative embodiments of a connecting member according to the invention.
  • DESCRIPTION OF EMBODIMENTS
  • Fig. 1 schematically shows a vertical longitudinal section of a horizontal heat exchanger incorporating an connecting member arrangement according to the invention. The heat exchanger comprises in conventional manner a cylindrical shell 1; two bonnets 2 and 3 fixed to the shell by means of flange joints 5; two tube sheets 7, 8, the planes of which are perpendicular to the axis of the shell 1 and which are disposed at each end of the shell; tubes 9 fixed in holes in the tube sheets and extending between the tube sheets parallel to the axis of the shell; baffles 11, 12, 13 parallel to the tube sheets 7, 8 and distributed along the tubes 9; an inlet 15 at the top of the shell 1 at one side thereof for supplying a first heat exchanger fluid; an outlet 17 at the bottom of the shell at the other side thereof for evacuating the first heat exchanger fluid; an inlet 19 centrally disposed in the bonnet 3 for supplying a second heat exchanger fluid to pass through a first set of tubes 9 to the space inwardly of the bonnet 2; and an outlet 21 disposed at the bottom of the bonnet 3 for evacuating the second heat exchanger fluid after it has been recycled through a second set of tubes 9 to the space inwardly of the bonnet 3. At their peripheral outer edges, the tube sheets 7 and 8 are flexibly fixed to the shell 1 by means of special connecting members 23, which will be described in more detail below with reference to Figs 2-9.
  • The central baffle 12 is fixed to the shell, and the tubes 9 in turn are fixed to the baffle 12 at the point where they pass through it. The baffles 11 and 13 are fixed to the baffle 12 by means of spacer rods 25, but are movable relative to the shell. The tubes 9 pass through holes in the baffles 11 and 13, these holes being slightly larger than the tubes, such that the tubes 9 and the baffles 11 and 13 are movable in relation to each other. The baffles 11, 12, 13 do not extend over the entire circular cross-section and are so alternatingly adjoining the shell 1 that the first heat exchanger fluid is caused to follow an alternating downward and upward flow path about the tubes 9, as indicated by the arrows 27.
  • The second heat exchanger fluid is supplied to the first limited set of tubes 9 from the inlet 19 by means of a tubular duct 26. This consists of two telescopic tube parts 29, 30. The part 29 is connected to the inlet 19, and the part 30 is connected to the tube sheet, around the associated tubes. The part 29 can be displaced within the part 30 in connection with thermally-conditioned displacements of the tube sheet 8, a seal 31 ensuring adequate sealing with respect to the space inwardly of the bonnet 3. It is understood that the seal 31 may be a simple gland-type seal, since the pressure exerted across it does not exceed the pressure drop of the second heat exchanger fluid during its passage through the tubes 9. The flow path of the second heat exchanger fluid is indicated by the arrows 28.
  • The inventive flexible connection of the tube sheets 7, 8 to the shell 1 by means of the connecting member 23 appears more clearly from Figs 2-9 drawn on a larger scale. In these Figures, the same reference numerals as in Fig. 1 are used for the same or equivalent constructional elements.
  • Figs 2-9 all schematically illustrate the provision of a metallic, shell-like connecting member 23, viz. in an enlarged partial section taken along a diameter, parallel to the axis of the shell 1. In other words, the section is taken at right angles to the centre axis of the connecting member 23 designed as a shell portion of an annular toroid.
  • In Fig. 2, the connecting member 23 is a thin membrane shell of metal having the cross-sectional shape of a quarter circle, i.e. a 90° circular arc (in the unloaded state). The edges of the membrane shell are extended and fixed to the lower, i.e. "outer" edge surface 31 (in the Figure) of the tube sheet 8 and to the inner surface of the shell 1. Said edges are connected tangentially both to the inner surface of the shell 1 and to the tube sheet 8. Here, as in the other embodiments, the connection is performed by welding, as shown in the respective Figures. In this case, the membrane shell is located below the plane of the tube sheet 8, i.e. on the outside thereof. An "external" pressure exerted from one side is readily taken up as membrane stresses, as indicated by arrows 33. However, an "internal" pressure from one side can just as easily be taken up as membrane stresses thanks to the configuration of the membrane shell.
  • In the embodiment of Fig. 3, the membrane shell is connected orthogonally both to the tube sheet 8 and to the shell 1, and the extended fixing portion 37 of the membrane shell 23 is connected tangentially to a shell flange 5 and provided with a gasket 39 on its underside. Moreover, the fixing portion of the membrane shell at the tube sheet 8 is extended so as to project on the opposite side of the tube sheet 8. The thus projecting portion 35 has been found to improve the mounting strength and stability. As shown in the Figure, the membrane shell 23 and the extended portion 35 thereof are welded to the edge of the tube sheet 8 at its upper and lower side, respectively. An "internal" pressure exerted from one side is indicated by arrows 34.
  • Fig. 4 shows an embodiment of the same general type as that in Fig. 2, but the connecting member 23 here is a continuous extension of the tube sheet 8. This extension has a reduced wall thickness and protrudes from the upper side (i.e. "inner side") of the tube sheet 8. The free end surface 41 of the tube sheet is concave in conformity with the curvature of the membrane shell 23 so as to provide a smooth transition. In this manner, it is possible to avoid detrimental stress concentrations. For the same purpose, the opposite end of the membrane shell 23, which is welded to the shell 1, is thickened by the curvature of the membrane shell continuing a slight distance after the 90° arc. The weld joint 43 is located in the plane of the inner wall of the shell 1.
  • Fig. 5 shows an embodiment which is analogous with that of Fig. 2, although it is here a matter of an "internal" pressure exerted from one side. The curvature or arch of the membrane shell 23 thus is reversed, facing downwards, i.e. outwards. Also in this embodiment, the pressure thus acts within the concave, arched membrane shell to achieve the optimum membrane stress effect. It should however be emphasised that the membrane shell according to the invention can also take up pressure exerted only from the opposite, convex side.
  • The connecting member 23 here is a continuous extension of the shell 1. The transition to the shell 1 is designed in the same way as the transition to the tube sheet 8 in Fig. 4. At the tube sheet 8, the membrane shell 23 is welded to the lower part of the end edge surface. The end edge surface 45 otherwise is concave with a smooth transition from the curvature of the membrane shell 23, whereby to avoid detrimental stress concentrations.
  • Fig. 6 shows an embodiment which is analogous with that of Fig. 1, although modified in two respects. First, the membrane shell 23 is welded to the lower part of the end edge surface of the tube sheet (as in Fig. 5), and the end edge surface is formed with a continuously connected, circumferential groove 47. Second, an annular cylindrical stiffening ring 49 is rigidly mounted (in this case welded) on the upper side of the tube sheet 8 directly at the circumferential edge of the sheet. The ring 49 projects inwards, i.e. in the opposite direction with respect to the membrane shell 23, orthogonally to the tube sheet 8.
  • Fig. 7 shows an embodiment which is analogous (although reversed) with respect to that of Fig. 3. It is however intended for "internal" pressure and includes a stiffening ring 49 as in Fig. 6. In this case, the stiffening ring is however resiliently mounted by being welded to the projecting portion 35 of the membrane shell 23. Further, a circumferential groove 51 eliminating stress concentrations is provided on the underside of the tube sheet 8 in the immediate vicinity of the weld 53 between the tube sheet 8 and the membrane shell 23. The groove 51 and the weld 53 provide a smooth, curved transition between the membrane shell 23 and the tube sheet 8.
  • Fig. 8 shows an embodiment which is analogous with that of Fig. 5, but, additionally, provided with a stiffening ring 49, as in Fig. 6.
  • Fig. 9, finally, shows an embodiment in which the membrane shell 23 is tangentially connected by welding to the shell 1 at one end, while its other end is welded to the free end surface 55 of a fixed stiffening ring 49 projecting downwards from the lower edge portion of the tube sheet 8. The ring does not project at right angles from the tube sheet, but obliquely inwardly towards the centre of the heat exchanger, i.e. away from the shell 1. The lowermost portion 57 of the ring is bent backwards so as to be perpendicular to the plane of the tube sheet 8. An annular concave groove 59 is connected to the upper weld between the membrane shell 23 and the ring portion 57, whereby to avoid detrimental stress concentrations. As is readily appreciated, this arrangement means that the gap 61 between the shell 1 and the edge of the tube sheet 8 can be reduced, thus improving the utilisation of the interior of the heat exchanger.
  • The heat exchanger shown in Fig. 1 uses two movable tube sheets, which entails a horizontal heat exchanger, as well as the illustrated, preferred arrangement of the baffles. Other embodiments are however conceivable within the scope of the inventive concept. Thus, it is possible to provide one stationary and one movable tube sheet, in which case the heat exchanger can be arranged vertically with the tubes hanging or standing in the stationary tube sheet. Movable baffles are then mounted in conventional manner by means of spacer members in the stationary tube sheet.

Claims (9)

  1. A heat exchanger having a heat exchanger vessel with a shell (1) and, disposed inside the shell, at least one tube sheet (7, 8) to which a number of heat exchanger tubes (9) are connected and whose edge portion is sealingly connected to the shell (1) by means of a flexible connecting member (23), such that thermal expansion between the shell (1) and the tube sheet (7, 8) can be taken up as bending of the connecting member which is designed as part of a toroid having a cross-section of arched configuration, characterised in that the connecting member (23) is in the form of a thin membrane shell of metallic material and of continuous curvature, which has substantially the shape of a quarter circle, at least in the unloaded state, such that loads deriving from pressure differences across the connecting member (23) can be taken up as general membrane stresses in the connecting member.
  2. A heat exchanger as claimed in claim 1, charac erised in that the connecting member (23) is connected to the edges of the shell (1) and to a flange joint (5) of the tube sheet (8).
  3. A heat exchanger as claimed in claim 2, charac terised in that the connecting member (23) is connected to an edge surface (31) of the tube sheet (8), the connecting member being extended (35) so as to project on the opposite side of said edge surface with respect to the main extent of the connecting member.
  4. A heat exchanger as claimed in claim 1, charac terised in that the connecting member (23) is connected to the inner surface of the shell (1) and to the lower edge surface (31) of the tube sheet (8).
  5. A heat exchanger as claimed in claim 4, charac terised in that the connecting member is a continuous extension of the shell wall (1).
  6. A heat exchanger as claimed in claim 4, char acterised in that the connecting member is a continuous extension of the tube sheet.
  7. A heat exchanger as claimed in any one of the preceding claims, characterised in that an annular or flange-shaped stiffening means (49) is fixed at the edge portion of the tube sheet (8).
  8. A heat exchanger as claimed in claim 7, charac terised in that said stiffening means (49) is elastically fixed to the tube sheet (8).
  9. A heat exchanger as claimed in claims 3 and 8, characterised in that said stiffening means (49) is fixed to the extended portion (35) of the connecting member (23).
EP90908144A 1988-10-05 1990-04-04 Unloaded heat exchanger tube sheet Expired - Lifetime EP0523039B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE8803537A SE462815B (en) 1988-10-05 1988-10-05 DEVICE FOR HEAT EXCHANGER, WHICH HAS A TUBPLATE THAT SEALS THE CONNECTOR TO AN OUTER COAT WITH A FLEXIBLE CONNECTING ELEMENT WHICH SECTIONAL SECTION IS ESSENTIALLY THE FORM OF A QUARTER CIRCLE
PCT/SE1990/000225 WO1991015728A1 (en) 1988-10-05 1990-04-04 Unloaded heat exchanger tube sheet

Publications (2)

Publication Number Publication Date
EP0523039A1 EP0523039A1 (en) 1993-01-20
EP0523039B1 true EP0523039B1 (en) 1995-03-01

Family

ID=20373532

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90908144A Expired - Lifetime EP0523039B1 (en) 1988-10-05 1990-04-04 Unloaded heat exchanger tube sheet

Country Status (5)

Country Link
EP (1) EP0523039B1 (en)
DE (1) DE69017472T2 (en)
ES (1) ES2068387T3 (en)
SE (1) SE462815B (en)
WO (1) WO1991015728A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE462815B (en) * 1988-10-05 1990-09-03 Sune Malm DEVICE FOR HEAT EXCHANGER, WHICH HAS A TUBPLATE THAT SEALS THE CONNECTOR TO AN OUTER COAT WITH A FLEXIBLE CONNECTING ELEMENT WHICH SECTIONAL SECTION IS ESSENTIALLY THE FORM OF A QUARTER CIRCLE
DE4142375A1 (en) * 1991-12-20 1993-07-08 Siemens Ag COOLING AIR COOLER FOR GAS TURBINES
FR2772468B1 (en) * 1997-12-17 2000-03-03 Packinox Sa PLATE HEAT EXCHANGER
DE102005037156A1 (en) * 2005-08-06 2007-02-08 Daimlerchrysler Ag heat exchangers
DE102006042936A1 (en) * 2006-09-13 2008-03-27 Modine Manufacturing Co., Racine Heat exchanger, in particular exhaust gas heat exchanger
DE102011018846A1 (en) * 2011-01-19 2012-07-19 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial piston motor and method for operating an axial piston motor
DE102015014446A1 (en) * 2015-11-07 2017-05-11 Linde Aktiengesellschaft heat exchangers
DE102016200634A1 (en) * 2016-01-19 2017-07-20 Mahle International Gmbh Heat exchanger
CN114234701A (en) * 2021-12-31 2022-03-25 河南恒天久大实业有限公司 Heat exchanger with telescopic tube plate
CN114189174B (en) * 2022-02-15 2022-05-13 四川大学 Thermoelectric conversion device and system
CN115013195A (en) * 2022-06-30 2022-09-06 东风马勒热系统有限公司 Exhaust gas recirculation cooler adopting split type air outlet main sheet

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE179852C1 (en) * 1962-01-01
US1876401A (en) * 1932-09-06 chatfield
US1740318A (en) * 1927-12-24 1929-12-17 Gen Electric Condenser boiler
US1831454A (en) * 1930-08-15 1931-11-10 Ingersoll Rand Co Condenser
US2152266A (en) * 1937-05-14 1939-03-28 Andale Co Heat exchange equipment
DE1013676B (en) * 1953-05-11 1957-08-14 Metallgesellschaft Ag Radiator
FR1211918A (en) * 1957-12-23 1960-03-18 Foster Wheeler Ltd advanced heat exchangers
FR1370042A (en) * 1963-06-17 1964-08-21 Parsons C A & Co Ltd Improvements to tubular heat exchangers
BE758439A (en) * 1969-11-14 1971-04-16 Snecma PLATE HEAT EXCHANGER
CH545665A (en) * 1972-05-05 1974-02-15
FR2415790A1 (en) * 1978-01-27 1979-08-24 Westinghouse Electric Corp Heat exchanger with outer chamber and inner tubes - joined by a tube plate with a flexible part to reduce thermal stresses
SE462815B (en) * 1988-10-05 1990-09-03 Sune Malm DEVICE FOR HEAT EXCHANGER, WHICH HAS A TUBPLATE THAT SEALS THE CONNECTOR TO AN OUTER COAT WITH A FLEXIBLE CONNECTING ELEMENT WHICH SECTIONAL SECTION IS ESSENTIALLY THE FORM OF A QUARTER CIRCLE

Also Published As

Publication number Publication date
ES2068387T3 (en) 1995-04-16
DE69017472D1 (en) 1995-04-06
WO1991015728A1 (en) 1991-10-17
SE8803537L (en) 1990-04-06
DE69017472T2 (en) 1995-08-31
SE462815B (en) 1990-09-03
SE8803537D0 (en) 1988-10-05
EP0523039A1 (en) 1993-01-20

Similar Documents

Publication Publication Date Title
EP0523039B1 (en) Unloaded heat exchanger tube sheet
US3537411A (en) Double shelled chimney stack
US3762302A (en) Non-polluting chimney
US4598667A (en) Cooled tube wall for metallurgical furnace
US3425582A (en) Jacketed vessel
US3275181A (en) Mechanical coupling device, especially for pressure vessels
US2916182A (en) Lined tube and plate connection
US4170263A (en) Tube sheet connection to vessel containing a bundle of tubes
CN213018297U (en) Composite ceramic expansion joint
US3841207A (en) Non-polluting chimney
JP4837201B2 (en) Shell ring, reactor pressure vessel having a cylindrical shell comprising a plurality of shell rings, and method for assembling shell rings
CN112588207B (en) Vertical radial flow reactor
CN211175331U (en) Reinforced corrugated pipe joint expansion device
CN210344675U (en) Unrestrained bending-resistant metal corrugated expansion joint
CN210800395U (en) Self-balancing expansion joint
WO2016155582A1 (en) Tube heat exchanger tube-header sealing structure
CN215447569U (en) Sealing connection structure of heat exchange tube and tube plate for reboiler
CN112128502A (en) Expansion joint with high stability
US4638768A (en) Steam generator tubesheet/channel head/centerstay assembly
CN111608267A (en) Hollow hub node of assembled suitable for rectangle member aluminum alloy grid structure
JPS6210625Y2 (en)
CN112539403B (en) Fire tube type evaporator for recovering flue gas waste heat
CN219570838U (en) Novel flexible structure for sealing jacket of pressure vessel
CN213599920U (en) Expansion joint crack prevention heat exchanger and high-temperature high-pressure dyeing machine with same
JP6258068B2 (en) Reinforcing member, piping seal structure and building

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: 19920921

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): CH DE ES FR GB IT LI

17Q First examination report despatched

Effective date: 19930419

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

ITF It: translation for a ep patent filed
AK Designated contracting states

Kind code of ref document: B1

Designated state(s): CH DE ES FR GB IT LI

REF Corresponds to:

Ref document number: 69017472

Country of ref document: DE

Date of ref document: 19950406

ET Fr: translation filed
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2068387

Country of ref document: ES

Kind code of ref document: T3

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

Ref country code: GB

Payment date: 19970403

Year of fee payment: 8

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

Ref country code: CH

Payment date: 19970411

Year of fee payment: 8

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

Ref country code: ES

Payment date: 19970414

Year of fee payment: 8

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

Ref country code: FR

Payment date: 19970425

Year of fee payment: 8

Ref country code: DE

Payment date: 19970425

Year of fee payment: 8

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: 19980404

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 EXPIRATION OF PROTECTION

Effective date: 19980406

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

Ref country code: LI

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

Effective date: 19980430

Ref country code: FR

Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

Effective date: 19980430

Ref country code: CH

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

Effective date: 19980430

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

Effective date: 19980404

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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: 19990202

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20000201

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

Ref country code: IT

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

Effective date: 20050404