Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F1/00—Tubular elements; Assemblies of tubular elements
  • F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
  • F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
  • F28F1/24—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
  • F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F28—HEAT EXCHANGE IN GENERAL
  • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
  • F28F2215/00—Fins
  • F28F2215/10—Secondary fins, e.g. projections or recesses on main fins

Definitions

• Heat exchanger comprising grooved finned tubes
• the invention relates to a tube heat exchanger comprising finned tubes, in which the tubes extend in a certain axial direction and are provided with heat exchange fins, each fin having a heat exchange surface. surrounding a tube which extends in a certain radial direction relative to the tube and which is structured in relief to form grooves spaced relative to each other in the radial direction.
• the invention applies more particularly to a tube heat exchanger using air as a secondary exchange fluid such as aero-refrigerant, aero-condenser, aero-heater or aero-evaporator type equipment, used respectively for cooling, condensing, reheating and evaporation of a fluid, in particular in refining processes, gas treatment and compression plants, gas liquefaction units, coal synthesis units and gas, power generation facilities, regasification units, or any other fluid treatment facility.
• a secondary exchange fluid such as aero-refrigerant, aero-condenser, aero-heater or aero-evaporator type equipment, used respectively for cooling, condensing, reheating and evaporation of a fluid, in particular in refining processes, gas treatment and compression plants, gas liquefaction units, coal synthesis units and gas, power generation facilities, regasification units, or any other fluid treatment facility.
• such equipment comprises a main heat exchanger provided with a bundle of tubes with external fins in which circulates the fluid to be cooled, condensed, heated or evaporated, as well as distribution and distribution manifolds. fluid between the tubes.
• the fluid is cooled in the outer finned tubes by heat exchange with a second fluid circulating around the external tubes and fins, including ambient air.
• a circulation or forced ventilation of ambient air is provided by fans positioned either below (what is called a forced draft) or above (so-called induced draft) tubes exchanger .
• the ambient air is drawn through the finned tube bundle at a relatively low frontal speed of between 1.5 and 4 meters per second (m / s).
• the flow regime of the ambient air is generally laminar with some local turbulence.
• the areas of the heat exchanger where heat exchange is most important are the leading edges of the fins and tubes in the direction of the flow of air.
• recirculation zones of the exchanger are characterized by recirculation of the air which generates losses of charge and which do not allow good cooling of the fin.
• Patent document US-2008023180 discloses a fin for aero-refrigerant tube which has on the surface a relief with cavities or grooves formed by mechanical deformation of the fins. Such cavities or grooves make it possible to increase the heat exchange between the air and the fin thanks to creating turbulence while increasing pressure losses.
• concentric grooves 42 of semi-cylindrical section are formed on each fin.
• a fin for a heat exchanger tube equipped with airflow deflectors in the form of projecting surfaces which modify the structure of the air flow in order to improve the air flow. heat exchanges between the air and the fin. These surfaces are in the form of rectangular or triangular cutouts in the fin.
• the cuts made in the fin can be sources of fouling due to dust, insects, etc .. which obstruct the cuts.
• the object of the invention is to provide a grooved fin structure for a heat exchanger tube which makes it possible to obtain an increase in the heat exchange between the air and the fluid circulating in the tube, without deteriorating the loss of heat. charge.
• the subject of the invention is a tube heat exchanger comprising finned tubes, in which the tubes extend in a certain axial direction and are provided with heat exchange fins, each fin having a heat exchange surface surrounding a tube which extends in a certain radial direction relative to the tube and which is structured in relief to form grooves spaced from each other in the radial direction, and wherein the grooves of a fin have dimensions different that decrease as one moves away from the tube in the radial direction so as to provide a guide for a fluid around the tube.
• the main advantage of such a staggered conformation of the relief of the fins is that it makes it possible to better guide the flow of air at the rear of the tubes in the radial direction of the tubes (according to the direction of the flow which arrives on the tubes ).
• tubes with external fins according to the invention it is thus possible to greatly reduce an air recirculation zone at the rear of the tubes in the direction of the flow of air, which is normally important when uses flat-profiled (flat-profile) finned tubes.
• the raised relief floor surface guiding the air at the rear of the tubes makes it possible to reduce the recirculation zones where the heat exchange is bad and thus to take better advantage of the surface of the fins. In this way with a fin according to the invention, the gain obtained in terms of thermal performance can be very important.
• the grooves of a fin may have different depths and widths which decrease as one moves away from the tube in said radial direction.
• Each fin may have a thickness which decreases as one moves away from the tube in said radial direction.
• the grooves of a fin may be spaced from each other in a concentric shape pattern or in an elliptical shape pattern.
• the grooves of a fin may be very close to one another, that is to say joined.
• the grooves may be disposed on both sides of the fin.
• Each fin can be rolled up helically around the tube or where the fins may be in the form of disc.
• Figure 1 shows schematically in section a heat exchanger heat
• Figure 2 is a plan view of a fin according to the invention
• Figure 3 is a radial partial sectional view along the axis III-III of Figure 2 of a tube with two fins according to the invention
• Figure 4 is a radial partial sectional view along the axis III-III of Figure 2 of a tube with two fins according to the invention in another embodiment
• Figure 5 is a plan view of a fin according to the invention in yet another embodiment
• Figure 6 is a radial sectional view along the axis III-III of Figure 2 of a tube provided with several fins according to the invention
• Figure 7 is a radial sectional view of a set of tubes with flat profile fins showing current lines in a plane between two fins obtained by numerical simulation
• Figure 8 is a radial sectional view of a set of tubes with
• FIG. 9 schematically represents a representative graph of the pressure drop as a function of the frontal velocity of the air arriving on a fin according to the invention and on a flat-profile fin;
• FIG. 10 schematically represents a representative graph of the power exchanged as a function of the frontal speed of the air arriving on a fin according to the invention and on a flat profile fin.
• FIG. 1 shows a heat exchanger 1 comprising a bundle of tubes 2 of circular section with fins arranged in several substantially parallel superimposed rows extending in an axial direction A in which circulates a fluid to be cooled between an inlet B and an outlet C of the fluid, and around which circulates a flow of ambient air drawn from the bottom upwards in the direction indicated by the arrows D, transversely to the tubes 2, by fans 3 positioned above the heat exchanger 1.
• the circulation of the fluid is here divided into three passage sections or passes 2a, 2b, 2c successive diagrammatically shown in Figure 1 to improve the cooling of the fluid.
• a heat exchanger 1 thus generally comprises between three and eight rows of superposed tubes 2 arranged staggered or aligned with respect to the direction of flow of the fluid in the tubes 2 as indicated by the arrows F.
• the tubes 2 are provided with fins 4 radial outer annular substantially perpendicular to the tube 2 and substantially parallel to each other promoting the heat exchange between the ambient air and the fluid, and the guiding of the air flow towards the rear of the tubes 2 in the axial direction, as this will be described below.
• the outer fins 4 make it possible to increase the external heat exchange area by a factor of between 15 and 25 with respect to the surface of a similar tube 2 without fins. Such a surface increase makes it possible to increase the heat exchange, but also generates losses which are in particular compensated by the use of efficient fans.
• FIG. 1 shows a few fins 4 spaced from each other on a tube 2, it being obvious that fins 4 are preferably arranged all along all the tubes 2 of the exchanger 1. Moreover, the shape and the dimension of the outer fins 4 may vary from one tube to another of the bundle of tubes 2. The configurations of tubes 2 with external fins 4 are not necessarily homogeneous within a bundle of tubes 2, in particular the diameters of the tubes 2 may vary.
• FIG. 2 shows, around a tube 2, a fin 4 according to the invention with a radial surface structured in relief 5 to form grooves 5a, 5b, 5c spaced from each other in a certain radial direction E by a portion of annular fin 8 substantially flat.
• the grooves 5a, 5b, 5c of the fin 4 have different dimensions which decrease as one moves away from the tube 2 in such a way as to guide the flow of ambient air around the tube 2 in the axial direction A. More precisely, the grooves 5a, 5b, 5c of a fin 4 have respective respective depths p1, p2, p3 in the axial direction A and respective widths 11, 12, 13 in the radial direction E, respectively.
• the innermost groove 5a is the uppermost and widest of the grooves
• the outermost groove 5c is the smallest and the smallest
• the middle groove 5b is of intermediate height and width.
• the number of grooves 5a, 5b, 5c on a fin 4 is between two and four, but other grooves may be added depending on the application.
• the raised surface 5 consists of three circular grooves 5a, 5b, 5c arranged in a concentric shape and centered around the tube 2.
• Adjacent fins 4 may have concentric grooves 5a, 5b, 5c which are respectively in axial alignment (the fins 4 have the same raised surface 5 and thus a groove 5a, 5b, 5c of a fin 4 is in axial alignment with the corresponding groove of the other fins 4 on the tube 2).
• FIG. 3 the raised surface 5 consists of three circular grooves 5a, 5b, 5c arranged in a concentric shape and centered around the tube 2.
• Adjacent fins 4 may have concentric grooves 5a, 5b, 5c which are respectively in axial alignment (the fins 4 have the same raised surface 5 and thus a groove 5a, 5b, 5c of a fin 4 is in axial alignment with
• the concentric adjacent grooves 5a, 5b, 5c of a fin 4 are separated (disjoint) radially from one another by flat annular planar portions 8.
• These annular portions 8 may have in the radial direction E the same width d1, d2 or different widths d1, d2 according to a variable diagram, d1, d2 being for example between 1 and 5 mm.
• the portion widths decreases going from the tube 2 to the outer peripheral edge 4A or vice versa.
• the width of the separation portions 8 is very small (less than 1 mm).
• a tube 2 has fins 4 of the same configuration over its entire length.
• tubes 2 with different configurations of fins 4.
• the grooves 5a, 5b, 5c are formed on one and the same face 4c of the fin 4, that is, oriented in the same direction with respect to the fin 4.
• FIG. 4 shows another embodiment of a fin 4 according to the invention in which grooves 5d, 5e, 5f are oriented on either side of the fin 4, that is to say that they are arranged alternately on two faces 4c, 4d of the fin 4 opposite, which can confer a better mechanical strength with respect to the grooves 5a, 5b, 5c.
• FIG. 5 shows another embodiment of a fin 4 according to the invention in which the concentric grooves 5a, 5b, 5c have been replaced by grooves 6a, 6b, 6c arranged according to an elliptical shape diagram 4
• Such elliptical grooves 6a, 6b, 6c make it possible to take better advantage of the phenomenon of guiding the air through the grooves while limiting the increase in the associated pressure drop.
• the advantage of this solution is an increase in performance gain for similar conditions of use, ie iso speed and even pressure drop.
• the outer fins 4 can be made from an aluminum strip 7 or even another heat-conducting material wound helically in the axial direction A around each tube 2, as shown schematically in FIG. Note that the fins 4 are here very slightly inclined relative to the tube 2 and the direction A, as indicated by the arrow 4e, this inclination being small because the fins 4 are very close to each other, so that we can consider that the fins 4 are almost perpendicular to the tube 2. It is also possible to make a tube 2 with fins 4 more inclined relative to the axial direction A of the tube 2. Another embodiment of an outer fin 4 is formed by means of a series of rotating disks.
• the attachment between the fin 4 and the tube 2 may be made by embedding the fin 4, for example in a groove previously made on the periphery of the tube 2 (not shown), or by winding the fin 4 to the base of which a folding is achieved and crimping on the tube 2 for example knurled.
• the fin 4 can also be obtained by forming or deformation of an aluminum tube attached to the tube 2.
• the fin 4 can also be made using stacked disks.
• the fin 4 has a thickness which decreases as one moves away from the tube from the inner edge 4b the fin 4 towards its outer edge 4a.
• the thickness e1 of the fin 4 at its outer edge 4a may be between about 0.15 and 0.4 millimeters (mm) and the thickness e2 of the fin 4 at its inner edge 4b can be between about 0.4 and 1 mm.
• the grooves 5a, 5b, 5c have respective depths p1, p2, p3 between about 0.4 and 1.5 mm, and respective widths 11, 12, 13 at the base of the groove between about 1 and 4 mm, the grooves 5a, 5b, 5c having different heights and widths so as to obtain the decreasing stage relief away from the tube 2 such that p1> p2> p3 and 11> I2> I3.
• the fin 4 according to the invention has a length H of between approximately 10 and
• the pitch P between two consecutive fins along the tube 2 is between about 2.2 and 3.5 mm and preferably between about 2.5 and 3.2 mm, or generally less than the conventional spacing between two blades profiled consecutive dish.
• a heat exchanger 1 comprises a bundle of tubes
• the tubes 2 may be composed of steel, for example stainless steel or carbon steel or a high-alloy steel, such as incoloy, the choice of the material of the tubes 2 being a function of the transported fluid which may be aggressive. , and operating conditions.
• the outer fins 4 are generally made of aluminum, but may also be stainless steel, or any other heat conducting material.
• FIGS. 7 and 8 show current lines (obtained by numerical simulation) of the ambient air flowing in the direction D around several tubes 2 of the heat exchanger 1 in a plane M substantially perpendicular to the tubes 2 and located at the center between two consecutive fins 4 as shown in Figure 1 and in Figure 3.
• Figure 7 shows the case of a flat-profile fin and Figure 8 shows the case of a fin 4 according to the invention having concentric grooves 5a, 5b, 5c.
• a fluid recirculation zone Z1 is located behind the tubes 2 in the direction of the flow D of the air in which the heat exchange is bad.
• FIG. 8 there is a very large decrease in the recirculation of the fluid in a zone Z2 located at the rear of the tubes 2 in the direction of the flow D of the air.
• the pressure drop is represented as a function of the frontal air speed on the tubes 2 for tubes 2 with flat profile fins (curve 9A) and for tubes 2 with fins 4 according to FIG. invention with concentric grooves 5a, 5b, 5c (curve 9B).
• curve 9A flat profile fins
• curve 9B concentric grooves 5a, 5b, 5c
• This increase in the pressure drop can be compensated by spacing the fins 4 each other along the tube 2.
• the pitch P between two consecutive fins is different according to whether the surface of the fins is raised or not: 2.54 mm in the case of the flat profile vane and 3 mm for the fin 4 according to the invention with grooves 5a, 5b, 5c concentric. In this way, as can be seen in FIG. 9, the increase in the pressure drop caused by the raised surface 5 remains very small.
• FIG. 10 shows the power exchanged as a function of the frontal speed of the air on the tubes 2 for flat-profile tubes 2 (curve 10A) and for tubes 2 with fins 4 according to the invention. grooves 5a, 5b, 5c concentric (curve 10B) and for pitch P between fins as defined above.
• the exchanged power of the heat exchanger 1 that is to say the gain obtained, increases by about 10 to 25% depending on the frontal air speed, which corresponds to an increase in performance per unit of heat. exchanger length of between 2 and 10%.
• the spacing of the fins 4 along the tube 2 reduces the amount of material used to make the fins, which compensates for the increase in material caused by the realization of the raised surface 5 on the fin 4 by modifying the surface of the fin, and decreases the amount of material used to achieve a saving of the order of 3 to 6% per meter.

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

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Publications (2)

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• 2008
  • 2008-12-19 FR FR0858864A patent/FR2940422B1/fr active Active
• 2009
  • 2009-05-05 CN CN2009800002273A patent/CN101861506B/zh active Active
  • 2009-05-05 ES ES09716192T patent/ES2399504T3/es active Active
  • 2009-05-05 EP EP09716192A patent/EP2379977B1/de active Active
  • 2009-05-05 CA CA2747353A patent/CA2747353C/fr active Active
  • 2009-05-05 PL PL09716192T patent/PL2379977T3/pl unknown
  • 2009-05-05 KR KR1020097020333A patent/KR101177726B1/ko active Active
  • 2009-05-05 BR BRPI0906068-5 patent/BRPI0906068B1/pt active IP Right Grant
  • 2009-05-05 RU RU2011129831/06A patent/RU2494330C2/ru active
  • 2009-05-05 WO PCT/FR2009/050832 patent/WO2010070216A1/fr not_active Ceased
  • 2009-05-11 US US12/463,861 patent/US8376033B2/en active Active

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