EP3814713A1 - Ensemble tube pour un dispositif échangeur de chaleur de type à tube - Google Patents

Ensemble tube pour un dispositif échangeur de chaleur de type à tube

Info

Publication number
EP3814713A1
EP3814713A1 EP19745318.6A EP19745318A EP3814713A1 EP 3814713 A1 EP3814713 A1 EP 3814713A1 EP 19745318 A EP19745318 A EP 19745318A EP 3814713 A1 EP3814713 A1 EP 3814713A1
Authority
EP
European Patent Office
Prior art keywords
tube
tubes
along
wall portions
tube assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP19745318.6A
Other languages
German (de)
English (en)
Other versions
EP3814713B1 (fr
Inventor
Mircea Dinulescu
Jens KITZHOFER
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.)
Apex International Holding BV
Original Assignee
Apex International Holding BV
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 Apex International Holding BV filed Critical Apex International Holding BV
Publication of EP3814713A1 publication Critical patent/EP3814713A1/fr
Application granted granted Critical
Publication of EP3814713B1 publication Critical patent/EP3814713B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/0041—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for only one medium being tubes having parts touching each other or tubes assembled in panel form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0062—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements

Definitions

  • the invention relates to a tube assembly for a tube-type heat exchanger device, and to a tube-type heat exchanger device that includes such a tube assembly.
  • HE heat exchanger
  • One known type is the plate-type HE device, which comprises flat and parallel plates that form heat transfer (HT) areas and flat fluid channels in between each pair of plates.
  • the plate-type HE device can be made relatively compact and allows the fluids to flow in a uniform and non-detached manner on both sides of the HE device.
  • high mechanical stresses may occur in the plates, even at moderate pressure differential on the two sides of the plate.
  • a plate-type HE device is unable to cope with high overpressures in the flowing fluids.
  • the allowed overpressures are limited to a range of 0.5 to 1 .5 bar gauge (barg).
  • Another known type is the conventional tube-type HE device, in which the heat transfer areas are formed by an array of cylindrical tubes.
  • An advantage of conventional tube-type HE devices lies in their ability to cope with high overpressures inside the tubes (e.g. hundreds of bars). The fluid flows are highly non-uniform outside the tubes of this conventional HE device.
  • the conventional tube-type HE is bulky and imposes great demands on manufacturing efforts and costs.
  • Chinese patent document CN104101235 describes a tube-type HE device that comprises a housing and HE tubes with rectangular cross-sections. These rectangular tubes are arranged alongside but at distances from each other.
  • the housing comprises two oppositely disposed mounting plates onto which opposite distal ends of the rectangular tubes are mounted.
  • Each mounting plate is provided with an array of rectangular fluid discharge holes, each hole being fluidly connected to a fluid passage that extends through a respective tube.
  • This known HE device has low mechanical strength, sub-optimal heat-transfer efficiency, and is relatively difficult to manufacture.
  • a HE assembly for a tube-type HE device.
  • the tube assembly comprises a plurality of tubes.
  • Each tube includes a bounding wall that surrounds a flow passage along a nominal axis in a first direction.
  • This bounding wall has two lateral wall portions on opposite sides along the flow passage, as well as two further wall portions on further opposite sides along the flow passage.
  • the tubes are adjacently arranged into tube rows that co-extend along the first direction to define first fluid channels.
  • the tube rows are mutually spaced along a third direction to define second fluid channels between adjacent pairs of tube rows.
  • At least one tube row is formed of tubes that are consecutively arranged along a second direction, so that the lateral wall portions of the tubes adjoin, and that the further wall portions of the tubes jointly define outer surfaces that border respective second fluid channels.
  • the proposed tube assembly forms an alternating (interleaved) arrangement of first and second fluid channels, with first channels formed by a row of adjacent tubes, and with second channels formed by spaces between distinct tube rows.
  • the complementary surface shapes of the lateral wall portions of the tubes allow these tubes to adjoin and be (interconnected to form a tube row.
  • the flow passages of the tubes in a tube row may jointly form one first fluid channel that provides passage to a first fluid with initial physical properties (e.g. composition, pressure, temperature, velocity, etc.).
  • the adjacent flow passages of tubes in one tube row may provide passage to distinct fluids.
  • the first fluid may flow through a first selection of the tubes in this row, and a further fluid with different composition, pressure, temperature, and/or velocity may flow through a further (i.e. distinct) selection of the tubes in this row.
  • combining tubes with complementary lateral surfaces into rows of laterally adjoining tubes yields a compact tube arrangement that can sustain high pressures for the first fluid(s) inside the first channels, and which is highly resistant to mechanical stress exerted on the tube rows.
  • the arrangement of rows with closely adjoining tubes i.e. without passages between tubes in the same row) prevents fluid in one second channel from passing between two tubes and mixing with fluid in the next second channel, which would cause unwanted pressure differentials near tube edges.
  • the adjoining tubes do not increase the flow resistance in a mannerthat negatively impacts the heat transfer efficiency.
  • the ordered tube arrangement may further ensure that the flow distributions for the first and second fluids remain relatively uniform and non-detached inside the first and second channels as well as outside the inlets and outlets of the HE device.
  • the lateral tube wall portions have a convex cross-sectional shape. More preferably, the lateral tube wall portions are flat (i.e. planar). The further tube wall portions may be flat as well.
  • the tubes may for instance have rectangular cross-sectional shapes, for which the contiguous further wall portions lie parallel and in line to define planar boundaries for the second fluid channels.
  • the bounding walls of several or all of the tubes may have cross-sectional shapes that form closed convex curves viewed in cross-sections perpendicular to the length of the tube. Consequently, each of these bounding walls has no undercut shape or other inflection points, viewed in cross-sections transverse to the direction of fluid flow through the tubes.
  • the outer surfaces of adjacent tubes are interrupted by level variations (for instance grooves or protrusions) in the third direction, which are elongated in the first direction along the tubes but localized in the second direction, and which are adapted to generate local turbulence in the second fluid flow that passes through a second fluid channel along the outer surfaces when the tube-type HE device is in operation.
  • the tubes in the tube row extend transversely to an associated second fluid channel that is bordered by the outer surfaces of these tubes. At least two of these outer surfaces may be interrupted by a level variation in the third direction.
  • This level variation extends in the first direction along a boundary line between two directly adjacent tubes, and is adapted to generate local turbulence in the second fluid flow that passes predominantly in the second direction through the second fluid channel and across the outer surfaces and the level variation, when the tube-type HE device is in operation.
  • a transition from laminar to turbulent flow in a fluid passing the HT plates may be triggered at Reynolds numbers below 10000.
  • Such a transition typically involves a sequence of stages that may be described as 1) Tollmien Schlichting waves, 2) deformed Tollmien Schlichting waves with three- dimensional vorticity, 3) three-dimensional breakdown, 4) turbulent spots, and 5) fully turbulent flow.
  • “fully developed” means that transverse cross-sectional velocity and velocity fluctuation distributions of a turbulent fluid stream at various downstream positions are essentially identical.
  • the local level variations between and along pairs of adjacent tubes which are highly localized in the direction along the second fluid flow, disrupt the boundary layer of the second fluid flow (i.e. the flow layers close to the further tube wall portions).
  • the local turbulent flow perturbations triggered by the level variations improve the attachment of the second fluid flow to the outer surfaces of the further tube wall portions, thus enhancing the heat transfer efficiency.
  • the level variations may be provided between each pair of adjacent tubes, or between selected pairs of adjacent tubes.
  • the level variations may be formed by grooves that are receded with respect to the outer surfaces of the further tube wall portions, or by ridges that are elevated with respect to the outer surfaces.
  • the bounding wall of at least one of the tubes includes one or more edge portions, each edge portion interconnecting a lateral wall portion and a further wall portion.
  • An outer surface of such edge portion delineates a groove between the tube and a directly adjacent tube. This groove extends along the first direction, and is recessed along the third direction with a groove depth relative to the further wall portions, to form one of the level variations for generating local turbulence in the second fluid flow.
  • the depth of the groove may be in a range between 5% and 20% of a height of the corresponding second fluid channel.
  • One or more of the edge portions may be formed by a single-curved fold of the bounding wall, having a radius of curvature in a range between 5% and 20% of the height of the second fluid channel.
  • the radius of curvature and the resulting groove depth may for instance be about 1 -4 millimeters, preferably 1 -2 millimeters, and for instance 1 .5 millimeters.
  • the folded edge portion which is situated between a lateral wall portion and a further wall portion of the tube, may thus define a rounded outer surface. If the edge portions of two directly adjacent tubes are rounded, the resulting groove has a curved V-shape that causes relatively little pressure drop in the second flow.
  • one or more of the edge portions may be formed by a folded edge portion that has a chamfered outer surface.
  • the resulting depth of the chamfer relative to the outer tube surface may again be in a range between 5% and 20% of a height of the second fluid channel. If the edge portions of two directly adjacent tubes are chamfered, the resulting groove has a straight V-shape that yields increased heat transfer but at the expense of a larger pressure drop.
  • one or more of the tube rows comprises at least one plate structure that is fixed to and interposed between two tubes, and extends along the first and third directions.
  • This plate structure protrudes along the third direction with a height relative to at least one of the outer surfaces of the further tube wall portions and into part of the respective second fluid channel, to form one of the level variations for generating local turbulence in the second fluid flow.
  • the height of the protrusion may be in a range between 10% and 20% of a height of the corresponding second fluid channel.
  • the plate structure protrudes only into a part of the respective second fluid channel near the outer wall surface, to trigger turbulent flow perturbations in the boundary layer of the second fluid flow close to the further tube wall portions, while shortening or even bypassing the above sequence of stages.
  • the plate structures may extend in the first direction along essentially the entire length of the tubes.
  • the structures may protrude relative to the further wall portions to define height profiles along the third direction that vary with position along the first direction. These height profiles may alternate along the positive and negative third direction as function of position along the first direction.
  • the height profiles may include symmetrical or asymmetrical shapes, and may for instance (viewed along the second direction) resemble a sine profile, a chirped profile, or a profile with a sequence of edges that are mutually oriented at non-zero angles to define sharp corners. These sharply cornered edges induce small-scale flow perturbations along both transverse directions (X and Z) in the impinging second flow.
  • the height profile may for instance define a polygonal contour.
  • polygonal implies that a projection of a protruding part in the plate structure has the shape of (part of) a simple polygon (e.g. a triangle, tetragon, pentagon, etc.).
  • a profile with a polygonal contour has relatively sharp edges in the plane perpendicular to the direction of the second fluid flow.
  • the plate structure protrudes in opposite directions along the third direction relative to both the outer surfaces of the further wall portions into part of the second fluid channels on both sides of the at least one tube row.
  • the tubes are interconnected by being mutually fixed via weld lines that extend along lateral edges of the respective lateral wall portions of the tubes.
  • the lateral edges may be leading lateral edges located at inlets of the flow passages, or trailing lateral edges located at outlets of the flow passages, or both.
  • the tubes may be interconnected without using direct bonds along the length of the lateral tube walls.
  • the tubes can be connected together via welding along their leading and/or trailing lateral tube edges, which allows for simple and efficient construction methods.
  • the welding can be performed one a tube-by-tube basis, or in a continuous manner along multiple tubes that have been properly aligned in advance.
  • the tube assembly comprises spacers that extend in the second flow direction and along the further wall portions of the tubes, and extend in the third direction along a full height of a respective second fluid channel, to provide non-zero mutual spacing between the tube rows along the third direction.
  • the tube assembly may thus be formed by simple construction methods that involve repetitive and alternating stacking of rows of tubes and spacers.
  • the spaces are preferably formed by elongated members, each having upper and lower surfaces that are substantially flat and mutually parallel, to support and be supported along edges of mutually parallel tube rows.
  • Lateral surfaces of such elongated spacer members may have a flat, polygonal, or curved shape.
  • the lateral surface that faces inwards towards the second fluid channel may for instance have a single concave shape, to form a smooth transition with the above- and below- situated flat tube arrays, and to form a second fluid channel with a cross-sectional contour resembling a stadium.
  • the lateral surface facing outwards may have a concave shape with upper and lower edges projecting laterally outwards and being aligned with the lateral surfaces of the outer tubes, to provide crests that facilitate welding of the spacer member to the above- and below-situated tube rows.
  • the spacers may be formed by bars with regular polygonal (e.g. rectangular) cross-sections.
  • the spacers may include leading spacers located at or near leading further edges of the further wall portions at inlets of the flow passages, or trailing spacers located at or near trailing further edges of the further wall portions at outlets of the flow passages, or both.
  • the spacers and tubes may consist essentially of the same material. This mitigates in-plane differential thermal expansion effects between a spacer and the tube rows directly connected thereto, when the HE device is in operation.
  • the tube assembly comprises a further tube row formed of tubes that are consecutively arranged along the second direction.
  • This further tube row is adjacent to the at least one row and aligned therewith relative to the second direction, so that lateral wall portions of the tubes in the adjacent tube rows line up in the third direction.
  • the weld lines may form continuous weld lines that extend along consecutive adjacent lateral edges of the lateral wall portions as well as across the spacers.
  • each of the tubes in the at least one tube row are fixed to an adjacent leading spacer via a further weld line along the leading further edges of the tubes and a leading surface of the leading spacer, or to an adjacent trailing spacer via a further weld line along the trailing further edges of the tubes and a trailing surface of the trailing spacer, or both.
  • each of the tubes comprises a leading section that extends along the respective flow passage from a respective inlet, a trailing section extending along the flow passage from a respective outlet, and a medial section extending along the flow passage between the leading and trailing sections.
  • At least one of the further tube wall portions may converge along the third direction towards the nominal axis in the leading section, so that the flow passage narrows with position along the first direction.
  • at least one of the further wall portions of the tubes may diverge along the third direction away from the nominal axis in the trailing section, so that the flow passage widens with position along the first direction.
  • adjacent tube rows of tubes may adjoin along leading further edges of the further tube wall portions located at inlets of the flow passages.
  • these adjacent tube rows may adjoin along trailing further edges of the further tube wall portions located at outlets of the flow passages. Throughout the medial sections, the adjacent tube rows are mutually spaced in the third direction, to enclose the second fluid channels.
  • the adjacent tube rows may be mutually fixed via continuous further weld lines along the leading further edges, and/or via continuous further weld lines along the trailing further edges. Fixing tube rows with continuous further weld lines along the leading and/or trailing further edges obviates the need for intermediary spacers and reduces the number of required welding operations. Also in this case, the tubes may be interconnected without using direct bonds along the length of the lateral tube walls.
  • the bounding wall of each tube has a substantially uniform thickness in the second and third directions.
  • the wall thickness may for instance range from 0.5 to 5 millimeters, preferably between 1 and 2 millimeters, and for instance be approximately 1 .5 millimeters.
  • these plate structures may have a thickness in the second direction that is comparable to or smaller than the tube wall thickness, and one or two orders of magnitude smaller than a total width of a tube.
  • the plate thickness may for instance be in a range from 0.1 to 2 millimeters, and more particular between 0.2 and 0.5 millimeters.
  • the bounding wall of each tube forms a unitary wall structure, in which each of the lateral wall portions extends on both its opposite edge regions via an interconnecting edge portion into a respective one of the further wall portions. These edge portions may form the rounded or chamfered outer surfaces.
  • the bounding wall of each tube has substantially quadrilateral cross- sectional shapes, and preferably substantially rectangular cross-sectional shapes, in planes perpendicular to the first direction.
  • the cross-sectional shapes of distinct tubes may be identical or different.
  • the tubes may have a width DU1 along the second direction Y and a height DZ1 along the third direction Z.
  • a ratio of DU1 to DZ1 may range from 1 to 10, thus allowing a wide range of differential overpressures in the first fluid flows (e.g. about 2 to 30 barg) to be accommodated by the tubes.
  • the ratio of DU1 to DZ1 ranges between 1 and 5.
  • at least one of the further wall portions of the tubes in the at least one row comprises a medial wall region that is displaced along the third direction and away from the nominal axis, to define a local widening of the flow passage relative to the lateral wall portions and a local narrowing of the second fluid channel.
  • the resulting local deformations of the medial wall regions confer a periodically undulated form upon the second fluid channel.
  • the resulting periodic height alternation along the second channel imparts a pulsating effect on the second fluid flow when the HE device is in operation.
  • the further wall portions of the tubes may for instance be deformed so that each pair of tubes on opposite sides of the second fluid channel defines a Venturi profile viewed in cross-section along the second and third directions Y, Z.
  • the resulting second fluid channels may thus be bounded in the third direction Z by a plurality of Venturi-shaped walls that form a repeating pattern along the second flow direction.
  • the tubes may consist essentially of a metal, a metal alloy, a ceramic, or a glass. Tubes formed from these materials can be made thermally and mechanically stable, and able to withstand high temperature and pressure conditions.
  • the tubes are formed from semi-finished tubes that consists essentially of metal or metal alloy, which are coated one or more sides of the tube with an enamel material, for instance a vitreous enamel (i.e. glass) layer, prior to arranging the tubes into the tube rows.
  • an enamel material for instance a vitreous enamel (i.e. glass) layer
  • Ceramics, full-glass, and enameled tube materials allow the tube assembly to operate in hostile environments in which at least one of the fluids is corrosive.
  • the bounding wall of the tube forms a unitary (i.e. monocoque) structure.
  • unitary tubes may for instance be formed by known methods, e.g. by extrusion or casting methods, or by folding an elongated rectangular plate blank at least three times (preferably four times) along substantially parallel folding lines in a developable (i.e. single curved) manner and laterally closing the resulting tubular shape by bonding the long edges of the folded blank.
  • edge bonding may be achieved via known welding techniques, for instance high frequency electric welding, tungsten inert gas (TIG) welding, metal inert gas (MIG) welding, laser welding, etc.
  • a tube-type HE device comprising a frame, and a tube assembly according to the first aspect, which is mounted on an inner side of the frame.
  • the tubes in a tube row may either be straight, or be bent to form first channels that jointly curve and change direction along the flow path of the first fluid while maintaining lateral contact, for instance to form tube rows with a macroscopically Z-type, U- type, or undulated shape.
  • the shapes of the second fluid channels may be varied along the flow path of the second fluid, by placing specifically shaped (e.g. curved) internal guiding vanes at various positions inside the second fluid channels, and/or by forming inlets and outlets of the second fluid channels at positions and with widths that span only part of the full width of the second fluid channels.
  • the first fluid channels may thus be formed into macroscopically curved configurations, for instance of the Z-type, or U-type.
  • the cross- sectional shape of the tube arrangement may be made to deviate from a uniform rectangular shape, by varying the widths of the distinct tube rows as function along the third direction, and/or by using spacer members with outer lateral surfaces that are slanted or curved to interconnect the above- and below-situated tube rows having edges that are mutually displaced.
  • Figure 1 shows a tube-type HE device according to an embodiment.
  • Figure 2a shows part of a tube assembly according to an embodiment.
  • Figures 2b and 2c show cross-sectional views of wall portions of adjacent tubes from the tube assembly in Figure 2a.
  • Figure 3 shows part of a tube assembly according to another embodiment.
  • Figure 4 shows part of a tube assembly according to yet another embodiment.
  • Figure 5a shows a cross-sectional view of part of a tube assembly according to another embodiment.
  • Figure 5b shows a plate structure from the tube assembly of Figure 5a.
  • Figure 6 shows a cross-sectional view of part of a tube assembly according to yet another embodiment.
  • Figure 7 shows a cross-sectional view of part of a tube assembly according to yet another embodiment.
  • Figure 1 schematically shows a perspective view of an embodiment of a heat exchanger
  • the HE device 10 is of a tube-type, and includes a mounting frame 14 and a tube assembly 12 that is mounted in a receiving space enclosed by the frame 14.
  • the tube assembly 12 defines a plurality of first fluid channels 22 that provide passage to a first fluid flow 26, and a plurality of second fluid channels 24 that provide passage to a second fluid flow 28.
  • the exemplary HE device 10 shown in figure 1 is of a cross-flow type, wherein the first and second fluid channels 22, 24 open up in an alternating manner on different but adjacent sides of the tube assembly 12. These first and second fluid channels 22, 24 form two distinct channel groups, which are connectable to distinct supply and discharge conduits (not shown) for fluid streams with different temperatures and compositions. In industrial applications, the temperatures and compositions of the fluids that make up the first and second fluid flows 26, 28 differ to such an extent that mixture of these fluids should be avoided.
  • the preferred connections of the fluid channels 22, 24 to hot or cold fluid supply and discharge conduits will be determined by the desired operating conditions of the HE device 10 via methods known to the skilled person.
  • the frame 14 comprises two end panels 18a, 18b and four support members 16.
  • the end panels 18 may be structurally reinforced plates that protect outer surfaces of the HE device 10.
  • the end panels 18 are located on opposite sides of the tube assembly 12, and are oriented substantially parallel with the first and second fluid channels 22, 24.
  • the tube assembly 12 has a box-shaped outer contour, and the support members 16 are formed by four support beams 16a, 16b, 16c (16d) that are located at four corners of the HE device 10.
  • the beams 16 are connected to the end panels 18 in respective beam connection regions 17, and jointly form a frame structure that encloses the receiving space in which the tube assembly 12 is mounted.
  • the upper end panel 18a in figure 1 is depicted in an exploded arrangement, and only three support beams 16a-c, one beam connection region 17d and part of sealing bellows 20d are shown.
  • the heat exchanger 10 has sealing means 20a, 20b, 20c, 20d that are formed by bellows structures 20.
  • Each bellows structure is provided between a corresponding beam 16 and a corner edge of the tube assembly 12, and extends along this corresponding beam 16 and the end panels 18.
  • the bellows structures 20 serve to prevent leakage between, the first fluid flows 26 in the first channels 22 on the one hand, and the second fluid flows 28 in the second channels 24 on the other hand.
  • the bellows structures 20 are sufficiently rigid to hold the tube assembly 12 in a fixed orientation between the frame components 16, 18 when the HE device 10 is in an inoperative state.
  • the bellows structures 20 are slightly flexible so that the tube assembly 12 is allowed to move and deform along the first and second directions X, Y relative to the beams 16 over a predetermined limited extent.
  • the bellows 20 accommodate local differential expansion effects between the tube assembly 12 and the frame 14 during operation of the HE device 10.
  • Further sealing means (not shown) similar to the bellows 20 may be provided between the end panels 18 and corresponding adjacent upper or lower edges of the tube assembly 12. These further sealing means may also be sufficiently rigid to hold the tube assembly 12 in a fixed orientation between the frame components 16, 18 when the HE device 10 is in an inoperative state, but slightly flexible so that the tube assembly 12 is allowed to move and deform along the third direction Z relative to the end panels 18 over a limited extent.
  • the connections and orientations of the sealing means 20 may be adapted to the desired properties of the fluid flows 26, 28 and operating conditions of the HE device 10.
  • FIG. 2a schematically shows details of the exemplary tube assembly 12 from the HE device 10 of figure 1 .
  • the tube assembly 12 comprises a plurality of tubes 30ij, which are grouped into a plurality of tube rows 32i.
  • i represents an index associated with distinct tube rows 32i
  • j 1 ,
  • the tube assembly 12 further comprises a plurality of spacers 54i, 55i arranged between vertically nearest tube rows 32i and 32i-1 .
  • Each tube 30 includes a bounding wall 34 that surrounds a flow passage 36.
  • This flow passage 36 extends in the first direction X and is centered on a nominal tube axis A.
  • each tube 30 consists essentially of solid metal, and is formed as a rectangular structure with a shape in the first direction X that is elongated relative to its dimensions in the second and third directions Y, Z.
  • the cross-sectional shape of the tube wall 34 perpendicular to the first direction X is substantially rectangular.
  • This wall 34 includes two lateral wall portions 40, 41 on opposite lateral sides along the flow passage 36 (associated with the second direction Y), and two further wall portions 42, 43 on further opposite sides along the flow passage 36 (associated with the third direction Z).
  • Each lateral wall portion 40/41 extends on both its opposite edge regions into a respective further wall portions 42/43.
  • each tube 30 forms a unitary structure, and each tube wall 34 has a substantially uniform thickness Dt.
  • the tubes 30 all extend along the first direction X, such that the flow passages 36 jointly define first fluid channels 22 (see figure 1). Multiple tubes 30 are grouped and positioned alongside each other to form respective tube rows 32. Distinct tube rows 32 are mutually spaced along the third direction Z, such that a second fluid channel 24 is defined between each vertically adjacent pair of tube rows 32.
  • the tubes 30ij in each respective tube row 32i are joined and consecutively arranged along the second direction Y, so that the lateral wall portions 40, 41 of the tubes 30 adjoin.
  • the flow passages 36 through the tubes 30 of one row 32 jointly form a linear array that defines one of the first fluid channels 22.
  • the lateral wall portions 40, 41 of adjacent tubes 30 directly abut along their lateral outer surfaces, without an intervening structure being present between adjoining tubes 30.
  • the upper further wall portions 42 of the tubes 30 in the row 32 lie in line and are substantially level, and define outer wall surfaces 44 that bound a second fluid channel 24 on an upper side of this row 32.
  • the lower further wall portions 43 of the tubes 30 in the tube row 32 lie in line and are substantially level, and define outer wall surfaces 45 that bound another second fluid channel 24 on a lower side of this row 32.
  • the outer surfaces 44, 45 of adjacent tubes 30 are interrupted by V-shaped grooves 62, 63 that extend in the first direction X in the direction of the tubes 30, but which extend only down/up to about 1 to 2 millimeters from the outer surfaces 44, 45. These grooves 62, 63 serve to generate local turbulence 64, 65 in the second fluid flows 28 that pass through the second fluid channels 24 when the tube-type HE device 10 is in operation.
  • Adjoining tubes 30 in each row 32 are mutually fixed by weld lines 60 that extend along leading lateral edges 46, 47 of the respective tube wall portions 40, 41 . The leading lateral edges 46, 47 are located at the inlet 38 of the corresponding tube 30 (i.e.
  • the spacers are rectangular spacer bars 54, 55 that are formed from the same metal as the tubes 30.
  • the spacer bars 54, 55 extend in the second flow direction Y along consecutive further tube wall portions 42/43 in a row 32.
  • the spacer bars 54, 55 include leading spacer bars 54 located at or near leading further edges 48/49 of the further wall portions 42/43 at the inlets 38, and trailing spacer bars 55 located at or near trailing further edges 52/53 of the further wall portions 42/43 at the outlets 39.
  • a second fluid channel 24i is bounded in the first direction X between a leading bar 54i and a trailing bar 55i.
  • a height of the spacer bars 54, 55 along the third direction Z approximately equals a height DZ1 of the tubes 30, so that the second fluid channels 24 have heights DZ2 that are similar to the tube height DZ1 .
  • the tubes 30 in distinct tube rows 32 are aligned in a lateral- vertical fashion, so that lateral wall portions 40, 41 of vertically adjacent tubes 30 line up in the third direction Z.
  • the weld lines 58 and/or 59 can thus be made in a continuous manner, to extend along consecutive adjacent lateral wall edges 46-47 and/or 50-51 , as well as across multiple spacer bars 54 and/or 55.
  • the leading/trailing surfaces 56/57 of the spacer bars 54/55 are arranged slightly receded inwards along the first direction X relative to the leading/trailing wall edges 46-49/50-53 of the tubes 30.
  • the tubes 30 in each tube row 32 are fixed to an adjacent leading spacer bar 54 via a further weld line 60 near to and parallel with the leading further tube edges 48/49 and along a leading surface 56 of the leading spacer bar 54.
  • the tubes 30 in each tube row 32 are fixed to an adjacent trailing spacer bar 55 via another further weld line 61 near to and parallel with the trailing further tube edges 52/53 and along a trailing surface 57 of the trailing spacer bar 55.
  • leading/trailing surfaces 56/57 may be level in the first direction X relative to the leading/trailing wall edges 46- 49/50-53.
  • the further weld lines 60/61 may extend directly along the leading/trailing further tube edges 48, 49 or 52, 53.
  • FIG. 2b schematically shows a cross sectional view of two adjacent tubes 30 having lateral wall portions 40, 41 that are mutually fixed by a weld line 58.
  • Each of the lateral wall portions 40, 41 has a leading lateral edge 46 resp. 47 that is tapered slightly outward relative to the flow passages 36 of the corresponding tubes 30.
  • the tapered leading lateral edges 46, 47 of adjoining tubes 30 together form a V-groove inside and along which welding material is applied to form a robust mechanical connection.
  • Figure 2c illustrates the grooves 62, 63 between the outer wall surfaces 44, 45 in more detail.
  • the tubes 30 are formed by unitary wall structures, with edge portions 66, 67 that each connect a respective lateral wall portion 40/41 to a further wall portion 42/43.
  • the edge portions 66, 67 are curvedly bent with a radius of curvature R of about 1 .5 millimeters, yielding a depth AZg of the grooves 62, 63 along the third direction Z and relative to the corresponding further wall portion 42, 43 which in this example is about 10% of a characteristic height DZ2 of the second channels 24.
  • Figure 3 shows another embodiment of a tube assembly 1 12.
  • Features in this tube assembly 1 12 that have already been described above with reference to the tube assembly 12 (see figures 1 -2b) may also be present in the tube assembly 1 12 in figure 3, and will not all be discussed here again.
  • like features are designated with similar reference numerals preceded by 100 to distinguish the embodiments.
  • each of the tubes 130 comprises a leading section 168 that extends from a respective inlet 138 into the associated flow passage 136, a trailing section 170 that extends from a respective outlet 139 into the flow passage 136, and a medial section 169 that extends along the flow passage 136 between the leading and trailing sections 168, 170.
  • the further wall portions 142, 143 of the tubes 130 converge in the third direction Z towards the nominal axis A, so that the flow passage 136 has a flared cross- sectional shape in a XZ-plane that narrows down with increasing X.
  • the further wall portions 142, 143 diverge in the third direction Z away from the nominal axis A, so that the flow passage 136 has a flared cross-sectional shape in the XZ-plane that widens along increasing X.
  • adjacent tube rows 132 are joined along leading further edges 148, 149 of the further tube wall portions 142, 143 located at the inlets 138, and along trailing further edges 152, 153 of the further wall portions 142, 143 located at the outlets 139.
  • Continuous further weld lines 160, 161 are provided along the leading further edges 148, 149 and the trailing further edges 152, 153 respectively.
  • the tube rows 132 remain mutually spaced in the third direction Z throughout the medial sections 169, so that the further tube wall portions 142, 143 of vertically adjacent tube rows 132 bound the second fluid channels 124 along the third direction Z.
  • Figure 4 shows another embodiment of a tube assembly 212.
  • Features in this tube assembly 212 that have already been described above for the preceding embodiments (see figures 1 -3) may also be present in the tube assembly 212 in figure 4, and will not all be discussed here again.
  • like features are designated with similar reference numerals preceded by 200 to distinguish the embodiments.
  • This embodiment largely corresponds to the embodiment from figure 3, but in this case, the further wall portions 242, 243 converge and diverge along only part of the leading and trailing sections 268, 270.
  • each of the further wall portions 242, 243 comprises a non-inclined planar part that extends parallel to the planar parts of the further wall portions 242, 243 in the medial section 269.
  • the further wall portions 242, 243 may include similar non-inclined planar parts at the outlet of the trailing section (not shown). The planar parts facilitate in the positioning and aligning of vertically adjacent tube rows 232, and provide larger surfaces along which the tube rows can be connected.
  • FIG. 4 illustrates that plate structures 274 may also be arranged in between adjacent pairs of tubes 230, which also serve to promote local turbulence 264 in the second fluid flow 228 that passes the outer wall surfaces 244. Further details on these plate structures 274 are discussed below with reference to figures 5a-b and 6.
  • Intermediate spacers 272 may be provided inside the second fluid channels 224, and extending between adjacent tube rows 232. Such intermediate spacers 272 have lower ends that abut outer surfaces 244 of upper further tube wall portions 242, and upper ends that abut outer surfaces 245 of lower further wall portions 243 of above-lying tubes. The intermediate spacers 272 keep the tube rows 232 mutually spaced in the third direction Z, so that a relatively uniform height DZ2 of the second fluid channels 224 is maintained along the length of the tubes 230.
  • the intermediate spacers are plate spacers 272, each being formed by a plate that is relatively thin (e.g.
  • each plate spacer 272 is mechanically attached via a welding line 273b, 273c to the upper further wall portion 242b2, 242c2 of the corresponding tube 230b2, 230c2, and extends along neighboring tubes 230b, 230c in the same tube row 232b, 232c to be supported by the respective further wall portions 242b, 242c, without being permanently attached thereto.
  • intermediate spacers 272 may be varied within one second channel 224 and/or in any or all of the other second channels 224, to maintain desired spacing of the tubes within the second fluid channels 224.
  • the intermediate spacers 272 in vertically adjacent second channels 224 are lined up along the third direction Z.
  • first groups of tubes in each tube row 232 provide passage to a first fluid 226, and second groups of tubes in each tube row provide passage to a further fluid 227 that has different physical properties than the first fluid 226.
  • the first group in the first tube row 232a may include i.a. tube 230a1
  • the second group in the first tube row 232a may include i.a. tube 230a2.
  • Additional tubes 230 may be present, but these are not shown in the figures).
  • the first groups associated with the first fluid 226 (not shaded in figure 4) and the second groups associated with the further fluid 227 (shaded in figure 4) may for instance be arranged in a staggered pattern along the second direction Y.
  • the HE device may be provided with a supply manifold (not shown) that is fluidly coupled to an inlet side 238 of the tube assembly 212, and which is configured to convey the first and further fluids 226, 227 towards and into the flow passages 236 of corresponding first and second groups of tubes 230.
  • the HE device may be provided with a discharge manifold (not shown) that is fluidly coupled to an outlet side of the tube assembly 212, and which is configured to convey the first and further fluids 226, 227 out of and away from the flow passages 236 of corresponding first and second groups of tubes.
  • a discharge manifold (not shown) that is fluidly coupled to an outlet side of the tube assembly 212, and which is configured to convey the first and further fluids 226, 227 out of and away from the flow passages 236 of corresponding first and second groups of tubes.
  • Figures 5a-5b show yet another embodiment of a tube assembly 312. Features that have been described in preceding embodiments may also be present in the tube assembly 312 and will not all be discussed here again. Like features have similar reference numerals, but preceded by 300.
  • This tube assembly 312 comprises grooves 362, 363 as well as plate structures 374 for locally generating small scale turbulences 364, 365 in the second fluid flows 328 that pass along the further wall portions 342, 343 when the tube-type HE device is in operation.
  • the distribution of plates 374 and grooves 362, 363 may be varied to balance between optimal heat transfer performance (i.e. plates/grooves between each pair of tubes) and spatial compactness (i.e. no plates/grooves between any pair of tubes).
  • the plate structures 374 are interposed between two tubes 330, and fixed to the tubes 330 via a known welding technique e.g. electric resistance welding.
  • Each plate structure 374 extends in the first direction X along the two bordering tubes 330, and protrudes with a first height profile F1 and/or a second height profile F2 in the third direction Z relative to the upper and/or lower further tube wall portion 342, 343 into the corresponding second fluid channel 324.
  • the protruding plate portions 376, 377 may extend perpendicular to the further wall portions 342-343, or may be tilted at an angle a in a range 0° ⁇ a ⁇ 180° relative to the further wall portions 342-343.
  • the wall 334 of each tube 330 has a substantially uniform thickness Dt of about 1 .5 millimeters.
  • the plate structures 374 have a thickness Dp that is about 0.2 millimeters (i.e. smaller than the wall thickness Dt).
  • Each of the rectangular tubes 330 has a tube width DU1 along the second direction Y and a tube height DZ1 along the third direction Z.
  • a ratio of DU1 to DZ1 ranges between 2 and 3.
  • the second channel 324 has a height DZ2 along the third direction Z, which is comparable to the tube height DZ1 .
  • Figure 5a shows a channel height DZ2 that is larger than the tube height DZ1 , only for illustration purposes).
  • Plate structures 374 protrude along the third direction ⁇ Z with heights DZr relative to the outer surfaces 344, 345 of further tube wall portions 342, 343, which heights DZr are about 10% of the second channel height DZ2.
  • Figure 5b shows a cross-section of a plate structure 374 in a downstream view along the second direction Y.
  • the plate structure 374 extends in the first direction X along essentially the entire length of the tubes 330, and has upper and lower protrusions 376, 377 relative to both upper and lower further wall portions 342, 343, to define profiles F1 , F2 that vary in height as a function of position along the first direction X.
  • the height profiles F1 , F2 alternate between constant low values that are level with the outer surface 344/345 of the tube 330, and constant extreme values that protrude with respective heights DZr1/DZr2 relative to the outer surface 344/345, thus forming rectangular teeth patterns.
  • the resulting periodic height profiles F1 , F2 with sharply angled edges serve to induce local flow turbulences along both XY- and YZ planes and with a periodic pattern along the channel width, to efficiently promote laminar-to- turbulent transitions in the second fluid flows 328 near the further wall portions 342, 343.
  • Other plate structures 374 in the tube assembly 312 may have different height profiles.
  • the protrusions 376, 377 on both sides of the structure 374 are vertically aligned, and the periodicities of the protrusions 376, 377 on plate structures 374 in adjacent tube rows 330 are essentially identical and in phase.
  • the sequence of local vertical constrictions will be periodic and symmetric on both sides of the second fluid channel 324.
  • Figure 5b also schematically shows localized welding regions 378a, 378b, which are provided along and centered on a nominal centerline of the plate structure 374. This centerline extends along the first direction X, and forms a mirror or rotational symmetry axis of the plate structure 374 relative to the third direction Z.
  • the plate structure 374 is fixed in these welding regions 378 to its two enclosing tubes via electric resistance welding.
  • Figure 6 shows a cross-sectional view downstream along the first direction X of yet another embodiment of a tube assembly 412.
  • Features in embodiments described above may also be present in the tube assembly 412 and will not all be discussed here again.
  • Like features are designated with similar reference numerals preceded by 400.
  • each tube 430 forms a unitary structure.
  • Each lateral wall portion 440 or 441 extends on both its opposite edge regions via a curved edge portion 466, 467 into a respective one of the further wall portions 442 or 443, to form a tubular geometry with rounded edges.
  • the curved edge portions of two adjacent tubes 430 jointly define a groove 462 or 463 that extends along the first direction X, and which is recessed along the third direction Z relative to the further wall portions 442 or 443.
  • These grooves 462 or 463 are adapted to generate local turbulences 464, 465 in the second fluid flows 428 that pass along the further wall portions 442 or 443 when the tube-type HE device is operational.
  • These local turbulences 464, 465 will break the boundary layer in the second fluid flow 428, and improve the attachment of the flow to the further tube wall portions 442-443, to enhance the heat transfer efficiency.
  • edge portions 466, 467 can be chosen differently, to change the intensity and characteristics of the generated local turbulences 464, 465.
  • grooves 462, 463 are formed on both sides of the tube row 432 and between each pair of tubes 430. Other patterns of tubes and grooves may be conceived, though.
  • the upper and lower further wall portions 442, 443 of the tubes 430 comprise upper and lower medial wall regions 480, 481 that are displaced away from the nominal axis A and along the third direction Z, to define a local widening of the flow passage 436 relative to the lateral wall portions 440, 441 and a local narrowing of the second fluid channel 424.
  • the tubes 430 have a tube height DZ1 near the lateral wall portions 440, 441 , and the second channel 424 has a height DZ2 along the third direction Z.
  • the tubes 430 At the upper and lower medial wall regions 480-481 , the tubes 430 have a height DZ3 > DZ1 , and the second channel 424 has a height DZ4 ⁇ DZ2.
  • a ratio of DZ2 to DZ4 is preferably larger than zero but smaller than 1.2, to avoid flow recirculation zones in the expanded part of the second channel 424.
  • the local deformations of the medial wall regions 480- 481 confer upon the second fluid channel 424 a periodically undulated shape with a symmetric unit cell, for which the height alternates as function of position along the second direction Y.
  • This resulting periodic local narrowing of the second fluid channel 424 imparts a pulsating effect on the second fluid flow 428 (via Bernoulli's principle) between the turbulence trigger points near the grooves 462, 463.
  • the resulting cross-sectional shape of the tubes 430 perpendicular to the first direction X is gradually and smoothly curved and has two inflections points around the medial wall region 480, 481.
  • the local slope of the further wall portions 442, 443 towards the third direction Z and relative to and away from the second direction Y may be described by a set of local angles b.
  • the angle b preferably stays within a range of -4° ⁇ b ⁇ +4° to ensure that the wall curvature remains smooth and relatively small, and to prevent flow separation effects in the second fluid flow 428.
  • the smoothly curved tube converges towards an elliptical shape, thereby reducing the flow resistance for the first fluid flow 426 inside the flow passages 436 and the pressure drop in the first fluid flow 426 across the tubes 430.
  • the outward displacement of the upper and lower medial wall regions 480, 481 away from the nominal axis A along Z and local widening of the flow passage 436 may be obtained by initially deforming a plurality of individual semi-finished tubes with rectangular cross-sections, and assembling the obtained deformed tubes into a tube assembly.
  • the semifinished tube may initially be sealingly enclosed within inner walls of a rigid casing, such that the inner casing walls abut only the lateral wall portions 440, 441 of the tube 430, while enclosing the further wall portions 442, 443 of the tube 430 at distances of about 1 ⁇ 2 ⁇ (DZ3 - DZ1) without abutting.
  • compressed gas e.g. air
  • a substantial overpressure can be applied to the flow passage 436 relative to the region inside the inner casing that surrounds the tube 430.
  • the resulting forces may force and thereby permanently deflect the upper and lower medial wall regions 480, 481 locally outwards from the initial tube wall shape over the available deflection distance 1 ⁇ 2 ⁇ (DZ3 - DZ1), until these regions abut the inner casing walls.
  • the bounding walls 434 of the tubes 430 are formed of stainless steel with a thickness Dt of 2 millimeters or more
  • the outward displacement of the upper and lower medial wall regions 480, 481 may be obtained by subjecting the tube 430 to an overpressure inside the flow passage 436 using hydraulic pressurization techniques.
  • Figure 7 shows a cross-sectional view downstream along the first direction X of yet another embodiment of a tube assembly 512.
  • Features of embodiments described above may also be present in this tube assembly 512 and will not all be discussed here again.
  • Like features are designated with similar reference numerals preceded by 500.
  • the upper and lower medial wall regions 580, 581 of the upper and lower further tube wall portions 542, 543 are displaced away from the nominal axis A and along the third direction Z, to define a local widening of the flow passage 536 relative to the lateral wall portions 540, 541 and a local narrowing of the second fluid channel 524.
  • the tube deformation is asymmetric relative to the nominal tube axis A and along second direction Y.
  • the maximum deflection of the medial wall regions 580, 581 of each tube 530 is located on a lateral side of the nominal axis A that is closer to the lateral wall portion 541 facing the incoming second fluid flow 528.
  • the outer wall surfaces 544, 545 of adjacent tube rows 532 on opposite sides of the second fluid channel 524 define a periodic sequence of Venturi-shaped profiles.
  • the outer wall surfaces 544, 545 in an individual Venturi-profile first converges and then diverges in the third direction Z as function of position along the second direction Y.
  • the incoming second fluid flow 528 first traverses a bell mouth shaped narrowing of the second channel 524 to a locally reduced height DZ4, which causes the flow velocity in the second flow 528 to increase.
  • the second channel 524 widens again in an approximately linear fashion, to finish at an increased channel height DZ2 at the end of the individual Venturi profile.
  • the extent of narrowing and widening is drawn in an exaggerated manner in figure 7.
  • the ratio of DZ2 to DZ4 preferably is larger than zero but smaller than 1 .2.
  • the subsequent widening of the respective wall surface 544, 545 is preferably oriented at an (half) angle b in a range of -4° ⁇ b ⁇ +4° away from the second direction Y, to ensure that a pressure drop in the second fluid flow 528 remains minimal.
  • the channel heights DZ1 , DZ2 of the first and second fluid channels were described as approximately equal, merely for illustration purposes.
  • the protrusions 376, 377 on both sides of the structure were vertically aligned and the periodicities of the protrusions on plate structures in adjacent tube rows were essentially identical and in phase.
  • the periodicity of the protrusions in adjacent tube rows may be identical, but may be shifted in phase along the first direction X, for instance over half the spatial period.
  • Such half-phase offset between protrusions on both sides of a second fluid channel ensures that the crests in the first height profile on one vertical side of a second fluid channel will coincide with the troughs of the second height profile on the other side of the same second fluid channel, to create a second fluid channel with an effective height that stays essentially constant along the first direction X.
  • the resulting fluid flow and turbulence effects within the second channel may thus stay relatively uniform along X.
  • the shape of the protrusions may be similar or different, within the same height profile on one side of a single plate structure, and/or between the first and second height profiles on both sides of the same plate structure, and/or between adjacent plate structures on both sides of the same second fluid channel.
  • the technical features disclosed herein are not restricted to the exemplary cross-flow plate-type HE device and tube arrangements described above, but may also be applied to other heat exchanger types, for example based on concurrent flow or counter flow principles and/or having Z-type or U-type configurations.
  • the tubes in the above-described exemplary embodiments were substantially linear in shape, and extended predominantly along the first direction X.
  • the three directions X, Y, Z should be considered local spatial properties, which vary with position along the flow trajectory.
  • the tube rows may for instance have a Z-shape, U-type, or undulated shape.
  • the shapes of the second fluid channels may also be varied along the flow path of the second fluid, to form macroscopically curved configurations, for instance of the Z-type, or U-type.
  • the cross-sectional shape of the entire tube arrangement may deviate from a uniform rectangular shape, by varying widths of distinct tube rows as function along the third direction, and/or by using spacer members with outer lateral surfaces that interpolating ⁇ interconnect the mutually displaced tube edges of above- and below-situated tube rows.
  • the tubes may be formed of different materials than metal.
  • the tubes may for instance consist essentially of metal alloys, a ceramics, glass, glass coated metals, or glass coated metal alloys. Different materials may be selected for distinct tubes and/or for distinct tube rows, depending on the mechanical and thermal requirements of the resulting HE device.
  • the tubes may have other cross-sectional shapes, provided that the lateral tube wall portions have complementary outer surfaces that allow adjacent tubes to adjoin and interconnect to form a tube row.
  • the lateral tube wall portions are flat.
  • the tubes may for instance have quadrilateral cross-sectional shapes e.g. rectangular (e.g. square), rhomboidal (e.g. diamond), trapezoidal, or parallelogram shapes.
  • quadrilateral cross-sectional shapes e.g. rectangular (e.g. square), rhomboidal (e.g. diamond), trapezoidal, or parallelogram shapes.
  • the cross-sectional shapes of distinct tubes may be identical or different.
  • the flow passages of the tubes in each tube row jointly formed one first fluid channel to provide passage to the same first fluid with initial physical properties (e.g. composition, pressure, temperature, velocity, etc.).
  • the adjacent flow passages of tubes in one tube row may provide passage to distinct fluids with different composition, pressure, temperature, and/or velocity characteristics.
  • a first selection of the tubes in this row may provide passage to the first fluid
  • a further (i.e. distinct) selection of the tubes in this row may provide passage to a further fluid with different composition, pressure, temperature, and/or velocity characteristics.
  • the HE device may be provided with fluid supply and/or discharge manifolds that are configured to convey the distinct fluid flows towards and/or away from their corresponding flow passages through the tube assembly.
  • tube-type HE devices of a unitary kind, i.e. a single tube assembly mounted in a single frame with connections for incoming and outgoing fluid streams.
  • HE units - of similar or diverse configurations as described herein and/or in combination with known HE unit types e.g. shell-and-tube-type HE units, plate-type HE units, etc.
  • known HE unit types e.g. shell-and-tube-type HE units, plate-type HE units, etc.
  • spacer e.g. plate spacer
  • X first direction e.g. longitudinal direction
  • Y second direction (e.g. transversal direction)
  • Z third direction e.g. vertical direction

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  • 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

Ensemble tube (312) pour un dispositif échangeur de chaleur de type à tube, et comprenant une pluralité de tubes (330a2, 330a3, 330b2). Chaque tube est formé par une paroi de délimitation qui entoure un passage d'écoulement le long d'un axe nominal dans une première direction (X). La paroi comporte deux parties de paroi latérales et deux autres parties de paroi (342a2, 342b2, 343a3). Les tubes sont disposés de manière adjacente en rangées de tubes (332a, 332b) qui coopèrent le long de la première direction pour délimiter des premiers canaux de fluide. Les rangées de tubes sont espacées le long d'une troisième direction (Z) pour définir des deuxièmes canaux de fluide (324a) entre des paires adjacentes de rangées de tubes. Au moins une rangée de tubes (332a, 332b) est formée de tubes (330a2, 330a3) qui sont disposés consécutivement le long d'une deuxième direction (Y), de telle sorte que les parties de paroi de tube latérales adjacentes et les passages d'écoulement desdits tubes forment conjointement un premier canal de fluide, et que les autres parties de paroi de tube (342a2, 343a3) délimitent conjointement des surfaces extérieures (344a2, 344a2) qui bordent des deuxièmes canaux de fluide (324a) respectifs.
EP19745318.6A 2018-06-08 2019-06-07 Ensemble tube pour un dispositif échangeur de chaleur de type à tube Active EP3814713B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NL2021088A NL2021088B1 (en) 2018-06-08 2018-06-08 Tube Assembly for a Tube-type Heat Exchanger Device
PCT/NL2019/050348 WO2019235934A1 (fr) 2018-06-08 2019-06-07 Ensemble tube pour un dispositif échangeur de chaleur de type à tube

Publications (2)

Publication Number Publication Date
EP3814713A1 true EP3814713A1 (fr) 2021-05-05
EP3814713B1 EP3814713B1 (fr) 2023-01-25

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EP19745318.6A Active EP3814713B1 (fr) 2018-06-08 2019-06-07 Ensemble tube pour un dispositif échangeur de chaleur de type à tube

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EP (1) EP3814713B1 (fr)
NL (1) NL2021088B1 (fr)
WO (1) WO2019235934A1 (fr)

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Publication number Priority date Publication date Assignee Title
US11391522B2 (en) * 2020-04-20 2022-07-19 Mikutay Corporation Tube and chamber type heat exchange apparatus having an enhanced medium directing assembly
CN115727691B (zh) * 2022-11-18 2023-11-21 大连理工大学 基于Sigmoid函数杂化方法的极小曲面与Kagome桁架结构的多孔介质换热器

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Publication number Priority date Publication date Assignee Title
CA2030577C (fr) 1990-11-23 1994-10-11 Mircea Dinulescu Echangeur thermique a plaques
DE102007015146B4 (de) * 2007-03-29 2009-12-10 Benteler Automobiltechnik Gmbh Aluminium System Kühler
NL2003983C2 (en) * 2009-12-18 2011-06-21 Mircea Dinulescu Plate type heat exchanger and method of manufacturing heat exchanger plate.
DE102012220435A1 (de) * 2012-11-09 2014-05-15 Mahle International Gmbh Kühlplatte
CN104101235A (zh) * 2014-07-31 2014-10-15 洛阳明远石化技术有限公司 管板式换热器

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EP3814713B1 (fr) 2023-01-25
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