[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP2053334B1 - Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur - Google Patents

Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur Download PDF

Info

Publication number
EP2053334B1
EP2053334B1 EP20070119401 EP07119401A EP2053334B1 EP 2053334 B1 EP2053334 B1 EP 2053334B1 EP 20070119401 EP20070119401 EP 20070119401 EP 07119401 A EP07119401 A EP 07119401A EP 2053334 B1 EP2053334 B1 EP 2053334B1
Authority
EP
European Patent Office
Prior art keywords
heat transfer
micro
particles
turbulating
binding medium
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.)
Not-in-force
Application number
EP20070119401
Other languages
German (de)
English (en)
Other versions
EP2053334A1 (fr
Inventor
Ronald Scott Bunker
Wayne Charles Hasz
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to EP20070119401 priority Critical patent/EP2053334B1/fr
Priority to ES07119401T priority patent/ES2436767T3/es
Publication of EP2053334A1 publication Critical patent/EP2053334A1/fr
Application granted granted Critical
Publication of EP2053334B1 publication Critical patent/EP2053334B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/18Arrangements for modifying heat-transfer, e.g. increasing, decreasing by applying coatings, e.g. radiation-absorbing, radiation-reflecting; by surface treatment, e.g. polishing
    • F28F13/185Heat-exchange surfaces provided with microstructures or with porous coatings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0061Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for phase-change applications
    • F28D2021/0064Vaporizers, e.g. evaporators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/18Arrangements for modifying heat-transfer, e.g. increasing, decreasing by applying coatings, e.g. radiation-absorbing, radiation-reflecting; by surface treatment, e.g. polishing
    • F28F13/185Heat-exchange surfaces provided with microstructures or with porous coatings
    • F28F13/187Heat-exchange surfaces provided with microstructures or with porous coatings especially adapted for evaporator surfaces or condenser surfaces, e.g. with nucleation sites

Definitions

  • the invention relates generally to an open rack vaporizer and a method for manufacturing such a manufacturing such an open rack vaporizer.
  • a heat transfer device such as a heat exchanger
  • a heat exchanger is a device that transmits thermal energy between a hot fluid and a cold fluid. Heat flows from the hot fluid to the cold fluid in the heat transfer device via a plurality of heat transfer surfaces such as tubes or panels. Heat exchangers may be classified into different types such as parallel flow type, counter flow type, cross flow type, single pass type, or multiple pass type. Heat exchangers used in fluid processing plants, for example liquid natural gas vaporizers or natural gas liquefiers, rely on several conventional heat transfer techniques to enhance thermal effectiveness or to enhance other heat transfer characteristics between a process fluid (e.g. liquid natural gas) side and a heat source or a heat sink side of the heat exchanger.
  • a process fluid e.g. liquid natural gas
  • One conventional technique to improve thermal effectiveness involves increasing the surface area of the heat transfer surfaces.
  • An increase in the surface area may be achieved by providing a plurality of fins, protrusions, or recesses for example, to the heat transfer surfaces, leading to an increase in the total heat flux per unit area (base surface area) of the heat transfer device resulting in a decrease in size and cost of the heat transfer device or an increase in total capacity of the device.
  • Another conventional technique to improve thermal effectiveness is to increase the heat transfer coefficient by providing flow turbulators or baffles to the heat transfer surfaces.
  • provision of flow turbulators or baffles results in increased pressure losses in the heat transfer device.
  • embodiments of the present invention provide a heat transfer device having a plurality of heat transfer walls configured to separate a first fluid and a second fluid.
  • An exemplary heat transfer enhancing system in accordance with the exemplary embodiments of the present invention is provided to one or more heat transfer walls.
  • the heat transfer enhancing system includes a plurality of micro turbulating particles bonded to one or more heat transfer walls using a binding medium.
  • the micro turbulating particles may include spherical shaped particles, or particles of different shapes depending on the requirement.
  • Exemplary techniques in accordance with the embodiments of the present invention are used to bond the micro turbulating particles randomly or in a predetermined pattern to the heat transfer surfaces.
  • the heat transfer enhancing system utilizes micro turbulating particles to enhance thermal effectiveness of heat transfer surfaces, such as for example, a plurality of tubes or panels in a liquid natural gas heat exchanger. Particle size, distribution density, spacing and pattern may be varied to achieve desired thermal enhancement.
  • the "micro turbulating particle distribution density" may be referred to as average increase in wetted surface area due to the micro turbulating particles. In one example, an average increase is 50%.
  • the micro turbulating particles act to enhance heat transfer between the first fluid and the second fluid via the heat transfer walls. Additional pressure loss in the heat transfer device is minimal. Specific embodiments of the present invention are discussed below referring generally to FIGS. 1-12 .
  • an exemplary system 10 for example, a liquid natural gas (LNG) system
  • the system 10 is an open rack vaporizer system.
  • the illustrated system 10 includes an LNG pump 12 coupled to an LNG tank 14.
  • the LNG pump 12 is also coupled via a pipe 16 to a panel (heat exchanger) 18.
  • the panel 18 includes a plurality of heat transfer tubes 20 arranged proximate to each other.
  • the LNG pump 12 is configured to supply a first fluid or a process liquid 19 (i.e. liquid natural gas) from the LNG tank 14 to the panel 18 via the pipe 16.
  • a valve 22 is provided to the pipe 16 and configured to control the amount of liquid natural gas flowing through the pipe 16.
  • the system 10 further includes another pump 24 coupled to an intake tank 26.
  • the pump 24 is also coupled to a header 28 via a pipe 30.
  • the pump 24 is configured to supply a second liquid (i.e. sea water) 32 from the intake tank 26 to the header 28 via the pipe 30.
  • the header 28 is provided to spray sea water 32 on the plurality of tubes 20 of the panel 18. Warm sea water flows along external surfaces of the tubes 20, while liquid natural gas flows through the tubes 20 and is evaporated.
  • the panel 18 includes an inlet side 34 configured to intake liquid natural gas 19 and an outlet side 36 configured to discharge natural gas via a supply pipe 38.
  • the inlet side 34 includes a vaporizing zone 40 and the outlet side 36 includes a heating zone 42.
  • the exemplary system 10 uses sea water 32 at atmospheric pressure as the heating source for vaporizing or heating low-temperature fluids (liquid natural gas) into gases at atmospheric temperatures.
  • the liquid natural gas is vaporized using sea water in the vaporizing zone 40 of the panel 18.
  • the vaporized natural gas is then further heated to a higher temperature in the heating zone 42 before discharging through the supply pipe 38.
  • an aluminum-zinc alloy is thermal-sprayed on the panel 18 to protect the panel 18 against corrosion by seawater 32.
  • a heat transfer enhancing system 44 in accordance with the exemplary embodiments of the present invention is provided to a plurality of heat transfer walls 46 of the plurality of tubes 20 of the panel 18.
  • the heat transfer enhancing system 44 includes a plurality of micro turbulating metallic particles bonded to the one or more heat transfer walls 46 of the tubes 20 using a binding medium.
  • a "micro turbulating particle" may be referred to as a single micro turbulating particle or an agglomeration of one or more single particles into one complex micro turbulating particle that does not allow liquid flow to penetrate inside the agglomeration.
  • micro turbulating particle size may be referred to as average height or diameter of a single or agglomerated micro turbulating particle.
  • particle spacing may be referred to as the local or regional average distance from one particle center to that of the adjacent particle center, expressed as a ratio of the particle size.
  • the panel 18 may include a plurality of panels arranged in parallel arrays. Warm sea water flows along external surfaces of the panels, while liquid natural gas flows through the panels and is evaporated.
  • the LNG vaporizer is illustrated, in certain other exemplary embodiments, the heat transfer enhancing system 44 may also be applicable to liquefiers, intercoolers, electrical and electronic thermal management devices, or the like where enhanced heat transfer rates are required.
  • the system 44 may be applicable to various types of heat exchangers such as parallel flow type, counter flow type, crossed flow type, and combined flow type heat exchangers.
  • Turbulation in accordance with the exemplary embodiments of the present invention may be utilized to treat a variety of components including combustor liners, combustor domes, vanes or blades, or shrouds of gas turbines.
  • the exemplary turbulation techniques may also be used to treat shroud clearance control areas including flanges, casings, and rings.
  • micro turbulating particles increase the surface area and the heat transfer coefficient of the heat transfer walls 46 that results in increased heat transfer rates and reduced relative pressure losses compared to other augmentation methods. Processing of the heat transfer walls may be customized depending on the requirement and differing levels of desired thermal enhancement. Specific embodiments of the present invention are discussed below referring generally to FIGS. 1-12 .
  • the heat transfer tube 20 in accordance with the aspects of FIG. 1 is illustrated.
  • the heat transfer enhancing system 44 is provided to an exterior surface 41 and an interior surface 43 of the heat transfer wall 46 of the tube 20.
  • the system 44 includes a plurality of micro turbulating particles bonded to the surfaces 41, 43 of the tube 20 using a binding medium.
  • the plurality of micro turbulating particles may include nickel, cobalt, aluminum, silicon, or iron, or alloys thereof, or a combination including any of the foregoing.
  • the binding medium may include epoxy, or metal foil, or solder, or braze material, or weld material, or a combination thereof.
  • micro turbulating particles and binding medium are not exhaustive and other metallic material or metallic alloys suitable for enhancing heat transfer characteristics are also envisaged.
  • the amount and type of binder generally ensures sufficient adhesive strength of the micro turbulating particles to the heat transfer wall in system 44.
  • the micro turbulating particles are applied randomly to the surfaces 41, 43 of the tube 20.
  • the micro turbulating particles may be randomly or partially provided to the heat transfer walls of the vaporizing zone and the heating zone of the panel.
  • the micro turbulating particles are uniformly bonded to one or more heat transfer walls of the tubes 20.
  • the micro turbulating particles are bonded in a predetermined pattern to one or more heat transfer walls of the tubes 20. The provision of the micro turbulating particles may be varied in different zones of the heat exchanger depending on the thermal potential of the zones.
  • the increase in heat transfer is largely due to increased micro turbulated surface area of the tube.
  • the micro turbulating particles may also increase heat transfer by modifying fluid flow characteristics such as from laminar flow to turbulent flow along the heat transfer surfaces. It should noted that the fluid flow along the heat transfer surface having enhanced heat transfer characteristics may include channel type fluid flow and impinging type fluid flow.
  • the system 44 includes a plurality of protuberances 48 provided in a predetermined pattern to a heat transfer wall 46 of the heat transfer tube.
  • the plurality of protuberances together defines "turbulation", which appears as a roughened surface that is effective to increase heat transfer through the heat transfer wall 46.
  • the protuberances are shown approximately spherical shaped, other shapes may also be envisaged to meet the desired roughness and surface area characteristics and thus obtain a desired heat transfer enhancement.
  • the protuberances 48 are provided along three rows 50, 52, 54 and four columns 56, 58, 60, and 62 to the heat transfer wall 46.
  • each protuberance 48 is 9 mils (0.009 inches). It should be noted that value of height "h” should not be construed as a limiting value and may vary depending on the heat transfer requirement.
  • Each protuberance 48 includes one or more of micro turbulating particles packed closely together. The protuberances 48 are bonded to the heat transfer surface 46 using the binding medium. It should again be noted that the illustrated example is merely an exemplary embodiment and that particle size, distribution density, spacing and pattern may be varied to achieve desired thermal enhancement. Size of the particles is determined based on the desired degree of surface roughness and surface area that will be provided by the protuberances. The micro turbulating particles facilitate enhanced heat transfer between the first fluid and the second fluid via the heat transfer wall 46. Additional pressure loss in the heat transfer device is minimal relative to that without the system 44.
  • the pattern may include predetermined limits on the relative size / spacing of the micro turbulating particles applied to the heat transfer wall 46.
  • the average height of the micro turbulating particle is characterized as "H”
  • the average micro turbulating particle diameter is characterized as "D”
  • the spacing between mutually adjacent micro turbulating particles may be in the range of 2 to 8 times the average diameter (D).
  • the micro turbulating particle height (H) may be in the range of 1 to 6 times the average diameter (D) of the micro turbulating particle.
  • the heat transfer tube 64 is an extruded tube having a plurality of fins 66 provided on an exterior surface 68 of a heat transfer wall 70.
  • the fins 66 may include plain type fins, or perforate type fins, or herringbone type fins, or serrated type fins, or a combination thereof.
  • An exemplary heat transfer enhancing system 44 in accordance with certain embodiments of the present invention is provided to the plurality of fins 66 provided on the exterior surface 68 of the heat transfer wall 70.
  • the heat transfer enhancing system 44 includes a plurality of micro turbulating particles bonded to the plurality of fins 66 using the binding medium.
  • the micro turbulating particles and the binding medium are applied to the fins 66 using techniques such as spraying, or slurry painting.
  • the binder may be thermally matured to realize bond strength (e.g. solder, braze).
  • the micro turbulating particles increase the micro turbulated surface area and heat transfer coefficient of the heat transfer wall 70 that results in enhanced heat transfer rates and reduced relative pressure losses.
  • FIG. 5 is a perspective view of a heat transfer device 76 (heat exchanger) in accordance with other aspects of the present invention.
  • the heat transfer device 76 includes a corrugated panel 78 in which the process fluid and heating/cooling fluid flows in alternate channels 80, 82 respectively.
  • the exemplary heat transfer enhancing system 44 in accordance with aspects of the present invention is provided and includes a plurality of micro turbulating particles 79 bonded to one side or both sides of the corrugated panel 78 using the binding medium.
  • the micro turbulating particles 79 and the binding medium are applied to the corrugated panel 78 using techniques such as spraying, or slurry, or roll coating, or a combination thereof and then heat treated to perform curing.
  • micro turbulating particles 79 increase the micro turbulated surface area and heat transfer coefficient of the corrugated panel 78 that results in enhanced heat transfer rates and reduced relative pressure losses.
  • particle size, spacing and pattern may be varied to achieve desired thermal enhancement.
  • the heat transfer enhancing system 44 in accordance with an exemplary embodiment of the present invention is illustrated.
  • the direction of flow of the process fluid and/or the heating/cooling fluid is indicated by the arrow 81 with respect to a flat heat transfer plate 83.
  • the heat transfer plate 83 includes an inlet region 85, a middle region 89, and an exit region 93.
  • the system 44 includes the plurality of micro turbulating particles 79 bonded to one side or both sides of the heat transfer plate 83 using the binding medium.
  • the micro turbulating particle distribution is concentrated in the inlet region 85 and the middle region 89.
  • the exit region 93 of the plate 83 is maintained smooth.
  • the micro turbulating particles 79 are closely packed together in the inlet region 85 whereas spacing between the micro turbulating particles is greater in the middle region 89.
  • the micro turbulating particles 79 increase the micro turbulated surface area and heat transfer coefficient of the heat transfer plate 83 that results in enhanced heat transfer rates and reduced relative pressure losses.
  • the heat transfer enhancing system 44 in accordance with an exemplary embodiment of the present invention is illustrated.
  • the heat transfer plate 83 includes the inlet region 85, the middle region 89, and the exit region 93.
  • the system 44 includes the plurality of micro turbulating particles 79 bonded to one side or both sides of the heat transfer plate 83 using the binding medium.
  • the micro turbulating particle distribution is concentrated in the inlet region 85 and the middle region 89.
  • the exit region 93 of the plate 83 is maintained smooth.
  • the size of micro turbulating particles 79 in the inlet region 85 is greater than the size of particles in the middle region 89.
  • the heat transfer enhancing system 44 in accordance with an exemplary embodiment of the present invention is illustrated.
  • the heat transfer plate 83 includes the inlet region 85, the middle region 89, and the exit region 93.
  • the system 44 includes the plurality of micro turbulating particles 79 bonded to one side or both sides of the heat transfer plate 83 using the binding medium.
  • the micro turbulating particle distribution is concentrated in the inlet region 85 and the exit region 93.
  • the middle region 87 is maintained smooth.
  • the size of micro turbulating particles 79 in the inlet region 85 is greater than the size of particles in the exit region 93.
  • the particle distribution density in the exit region 93 is greater than the distribution density in the inlet region 85 (i.e. the micro turbulating particles 79 are closely packed in the exit region 93 whereas spacing between the micro turbulating particles in the inlet region 85 is greater).
  • the particle distribution density is also characterized by the particle shaping, or agglomeration sizes, or size, or a combination thereof and creation of wetted surface area/flow turbulation.
  • the heat transfer enhancing system 44 in accordance with an exemplary embodiment of the present invention is illustrated.
  • the heat transfer plate 83 includes a top region 95, an intermediate region 97, and a lower region 99.
  • the system 44 includes the plurality of micro turbulating particles 79 bonded to one side or both sides of the heat transfer plate 83 using the binding medium.
  • the micro turbulating particle distribution is concentrated in the top region 85 and the lower region 99.
  • the intermediate region 97 is maintained smooth.
  • the size of micro turbulating particles 79 in the inlet region 85 is greater than the size of particles in the exit region 93.
  • FIG. 10 a graph representing variation of fluid jet Reynolds number (x-axis) versus heat transfer enhancement (y-axis) for impinging type fluid flow in accordance with an exemplary embodiment of the present invention is illustrated.
  • the Reynolds number is the ratio of inertial forces to viscous forces and is used for determining whether a flow will be laminar or turbulent.
  • Heat transfer enhancement is the ratio of heat transfer coefficient for a micro turbulated surface to the heat transfer coefficient for a smooth surface.
  • the illustrated graph shows variation of jet Reynolds number versus heat transfer enhancement for two heat transfer walls having different surface roughnesses.
  • Curve 84 represents variation of jet Reynolds number versus heat transfer enhancement for a heat transfer wall having an average surface roughness (Ra) equal to 0.35 mils (i.e.0.00035 inches).
  • Curve 86 represents variation of jet Reynolds number versus heat transfer enhancement for a heat transfer wall having an average surface roughness (Ra) equal to 1.14 mils (0.00114 inches). It may be observed that heat transfer rates across the heat transfer walls increases with increase in average surface roughness.
  • the illustrated graph is merely an exemplary embodiment and the variation of jet Reynolds number versus heat transfer enhancement may vary depending on the particle size, spacing and pattern applied to achieve desired thermal enhancement. In certain exemplary embodiments, the average surface roughness values are typically 7 to 12 times less than the actual particle size for random surfaces, and depend on particle spacing for non-random surfaces.
  • an exemplary technique used to provide a heat transfer enhancing system to a heat transfer device for example a heat exchanger, in accordance with an exemplary embodiment of the present invention.
  • the illustrated exemplary technique involves spraying a binding medium to a heat transfer tube 88 of a heat exchanger.
  • the binding medium may include epoxy, or metal foil, or solder, or braze material, or weld material, or a combination thereof.
  • the micro turbulating particles 87 are dusted over the binding medium applied to the heat transfer tube 88. It should be noted that other exemplary techniques for applying micro turbulating particles over the binding medium applied to the heat transfer tube 88 are also envisaged.
  • the micro turbulating particles 87 are bonded randomly or in a predetermined pattern to the heat transfer surface of the heat transfer tube 88.
  • the plurality of micro turbulating particles may include nickel, or cobalt, or aluminum, or silicon, or iron, or copper, or a combination thereof.
  • the particle size, spacing and pattern may also be varied to achieve desired thermal enhancement.
  • the heat transfer tube 88 may be rotated for applying micro turbulating particles 87 over the binding medium applied to the heat transfer tube 88.
  • the micro turbulating particles 87 may be applied from different angles over the binding medium applied to the heat transfer tube 88.
  • the heat transfer tube 88 is then passed through an oven 90 for thermal heat treatment to cure the micro turbulating particles 87.
  • FIG. 12 illustrates an exemplary technique used to provide a heat transfer enhancing system to a heat transfer device 94, for example an intercooler, in accordance with an exemplary embodiment of the present invention.
  • the exemplary technique involves spraying or applying a binding medium 91 such as a film of high conductivity epoxy to a heat transfer surface 92 of an intercooler 94.
  • a binding medium 91 such as a film of high conductivity epoxy
  • a plurality of micro turbulating particles 96 are sprayed randomly or in predetermined pattern over the binding medium applied to the heat transfer surface 92 of the intercooler 94.
  • the micro turbulating particles 96 may be then heat treated for curing.
  • a binding medium such as aluminum foil or solder foil are applied to the heat transfer surface 92 of the intercooler.
  • the plurality of micro turbulating particles 96 are sprayed randomly or in predetermined pattern over the aluminum foil or solder foil applied to the heat transfer surface 92.
  • the foil and the particles are then heat treated to bond the particles to the heat transfer surface 92.
  • a binding medium such as a braze alloy may be dip coated to the heat transfer surface 92 of the intercooler 94.
  • the plurality of micro turbulating particles 96 are sprayed randomly or in predetermined pattern over the braze alloy applied to the heat transfer surface 92.
  • the braze alloy and the particles are then heat treated to bond the particles to the heat transfer surface 92.
  • the binding medium and the micro turbulating particles are applied simultaneously to the heat transfer surface 92 and then heat treated to bond the binding medium and the particles to the heat transfer surface.
  • the application of binding medium and the micro turbulating particles may be done by techniques such as spraying, or roll coating, or a combination thereof.
  • the patterning of the binding medium on the heat transfer surface may be performed through patterned masking, or screen printing, or roll printing, or a combination thereof.
  • the micro turbulating particles are patterned to the heat transfer surface 92 through a screen by a screen printing technique. Alternately or additionally, the binding medium is applied through the screen to the heat transfer surface. Removal of the screen results in the predetermined pattern formed on the heat transfer surface.
  • a pattern in accordance with aspects of the present invention may be defined as plurality of "clusters" of particles (one or more particles), wherein the clusters are generally spaced apart from each other by a pitch corresponding to the spacing of openings in the screen. The excess particles are removed resulting in the desired pattern of the particles.
  • the binding medium may be applied using sprayers, or brushes, or squeegee, or trowel, or as sheets, or a combination thereof.
  • the micro turbulating particles may also be patterned to the heat transfer surface by screen printing.
  • the binding medium and the particles may be cured by thermal heat treatment, or ultra violet rays, or spray activator, or a combination thereof.
  • a pre-turbulated sheet having micro turbulating particles and binding medium may be bonded to the heat transfer surface.

Landscapes

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

Claims (9)

  1. Vaporisateur à casier ouvert, comprenant un dispositif de transfert de chaleur, le dispositif de transfert de chaleur (18) comportant :
    au moins une paroi de transfert de chaleur (46) configurée pour séparer du gaz naturel liquide (19) et l'eau de mer (32);
    un système améliorant le transfert de chaleur (44) prévu sur la paroi de transfert de chaleur (46), au nombre d'au moins une, et comprenant une pluralité de particules génératrices de microturbulences (48) appliquées sur la paroi de transfert, au nombre d'au moins une, ou des parties de celle-ci, en utilisant un agent liant,
    dans lequel au moins quelques-unes des particules génératrices de microturbulences (48) forment une ou plus d'une agglomérations de particules génératrices de microturbulences (48), l'agglomération ou chacune des agglomérations de particules génératrices de microturbulences (48) ne permettant pas à un flux de fluide de pénétrer à l'intérieur de l'agglomération;
    dans lequel le système améliorant le transfert de chaleur (44) comprend une variation sélectionnée de la taille des particules ou de la densité de distribution des particules ou de l'espacement des régions de particules ou une combinaison de ceux-ci.
  2. Vaporisateur à casier ouvert selon la revendication 1, dans lequel la pluralité de particules génératrices de microturbulences (48) est constituée de nickel, de cobalt, d'aluminium, de silicium ou de fer ou de cuivre ou d'alliages de ceux-ci, ou d'une combinaison comportant l'une quelconque des matières précitées.
  3. Vaporisateur à casier ouvert selon la revendication 1, dans lequel l'agent liant est constitué d'époxy ou d'une feuille métallique ou de brasure tendre ou de brasure forte ou d'un matériau de soudage ou d'une combinaison de ceux-ci.
  4. Vaporisateur à casier ouvert selon la revendication 1, dans lequel la pluralité de particules génératrices de microturbulences (48) sont fixées de manière aléatoire ou uniforme à la paroi de transfert de chaleur (46), au nombre d'au moins une, en utilisant l'agent liant.
  5. Vaporisateur à casier ouvert selon la revendication 1, dans lequel la pluralité de particules génératrices de microturbulences (48) sont fixées selon un motif prédéterminé à la paroi de transfert de chaleur (46), au nombre d'au moins une, ou à des parties de celle-ci, en utilisant l'agent liant.
  6. Vaporisateur à casier ouvert (18) selon la revendication 1, dans lequel la pluralité de particules génératrices de microturbulences (48) sont fixées à une pluralité d'ailettes ou de saillies (66) sur la paroi de transfert de chaleur (46), au nombre d'au moins une, en utilisant l'agent liant.
  7. Procédé de fabrication d'un vaporisateur à casier ouvert selon la revendication 1, comprenant un dispositif de transfert de chaleur (18), le procédé consistant en :
    la mise en place d'au moins une paroi de transfert de chaleur (46) configurée pour séparer le gaz naturel liquide (19) et l'eau de mer (32);
    la mise en place d'un système améliorant le transfert de chaleur (44) sur la paroi de transfert de chaleur (46), au nombre d'au moins une, et consistant en la fixation d'une pluralité de particules génératrices de microturbulences (48) à la paroi de transfert de chaleur (46), au nombre d'au moins une, ou des parties de celle-ci, en utilisant un agent liant, au moins quelques-unes des particules génératrices de microturbulences (48) formant une ou plus d'une agglomérations de particules génératrices de microturbulences (48), l'agglomération ou chacune des agglomérations de particules génératrices de microturbulences (48) ne permettant pas à un flux de fluide de pénétrer à l'intérieur de l'agglomération.
  8. Procédé selon la revendication 7, consistant en la fixation de la pluralité de particules génératrices de microturbulences (48), selon un motif prédéterminé, à la paroi de transfert de chaleur (46), au nombre d'au moins une, ou à des parties de celle-ci, en utilisant l'agent liant.
  9. Procédé selon la revendication 7, consistant en la fixation partielle de la pluralité de particules génératrices de microturbulences (48) à la paroi de transfert de chaleur (46), au nombre d'au moins une, en utilisant l'agent liant.
EP20070119401 2007-10-26 2007-10-26 Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur Not-in-force EP2053334B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP20070119401 EP2053334B1 (fr) 2007-10-26 2007-10-26 Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur
ES07119401T ES2436767T3 (es) 2007-10-26 2007-10-26 Sistema de mejora de la transferencia de calor y procedimiento de fabricación de un dispositivo de transferencia de calor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20070119401 EP2053334B1 (fr) 2007-10-26 2007-10-26 Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur

Publications (2)

Publication Number Publication Date
EP2053334A1 EP2053334A1 (fr) 2009-04-29
EP2053334B1 true EP2053334B1 (fr) 2013-08-28

Family

ID=39126637

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20070119401 Not-in-force EP2053334B1 (fr) 2007-10-26 2007-10-26 Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur

Country Status (2)

Country Link
EP (1) EP2053334B1 (fr)
ES (1) ES2436767T3 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6894729B2 (ja) * 2017-03-16 2021-06-30 住友精密工業株式会社 オープンラック式気化装置
FR3075341B1 (fr) * 2017-12-19 2021-01-08 Air Liquide Echangeur de chaleur avec elements intercalaires a texturation de surface

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6468669B1 (en) 1999-05-03 2002-10-22 General Electric Company Article having turbulation and method of providing turbulation on an article
DE10248548A1 (de) 2002-10-18 2004-04-29 Alstom (Switzerland) Ltd. Kühlbares Bauteil
EP1557627A1 (fr) 2003-12-01 2005-07-27 SPX Cooling Technologies GmbH Canal d'écoulement

Also Published As

Publication number Publication date
ES2436767T3 (es) 2014-01-07
EP2053334A1 (fr) 2009-04-29

Similar Documents

Publication Publication Date Title
US8356658B2 (en) Heat transfer enhancing system and method for fabricating heat transfer device
Sadeghianjahromi et al. Heat transfer enhancement in fin-and-tube heat exchangers–A review on different mechanisms
Awais et al. Heat and mass transfer for compact heat exchanger (CHXs) design: A state-of-the-art review
Huang et al. Review of nature-inspired heat exchanger technology
EP3803252B1 (fr) Structures fabriquées de manière additive pour une conductivité thermique à gradient
Riofrío et al. State of the art of efficient pumped two-phase flow cooling technologies
US20200080796A1 (en) Additive manufactured heat exchanger
US10422588B2 (en) Heat exchanger coil with offset fins
US12018894B2 (en) On-demand sweating-boosted air cooled heat-pipe condensers
WO1987002762A1 (fr) Echangeur thermique
EP2053334B1 (fr) Système pour l'amélioration du transfert de chaleur et procédé pour la fabrication d'un dispositif de transfert de chaleur
Kumar et al. A comprehensive review on thermal performance enhancement of plate heat exchanger
Abolfathi et al. Experimental study on flow around a tube in mixed tube bundles comprising cam-shaped and circular cylinders in in-line arrangement
JP2009109037A (ja) 熱伝達増進システムと熱伝達装置の製作方法
CA2607688C (fr) Systeme de facilitation du transfert thermique et methode de fabrication du dispositif en question
US3396782A (en) Heating unit
RU2447386C2 (ru) Устройство повышения теплопередачи и способ изготовления устройства теплопередачи
CN101424495A (zh) 用于制造传热设备的传热强化系统和方法
Chaturvedi et al. Heat transfer enhancement using delta and circular winglets on a double pipe heat exchanger
KR101433377B1 (ko) 열전달 증대 시스템 및 열전달 장치 제조 방법
KR20140036541A (ko) 튜브와 와이어로 조립된 트러스 구조체를 이용한 라디에이터
US11525618B2 (en) Enhanced heat exchanger performance under frosting conditions
RU2825805C2 (ru) Теплообменник
TWI839736B (zh) 三維最小曲面結構熱交換器設計
Kamath et al. An expermental study on enhancement of convective heat transfer over dimpled surface

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

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

17P Request for examination filed

Effective date: 20091029

17Q First examination report despatched

Effective date: 20091124

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20130402

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 629588

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130915

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602007032509

Country of ref document: DE

Effective date: 20131024

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2436767

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20140107

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 629588

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130828

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20130828

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

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131228

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131230

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130731

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20130828

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

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20131129

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

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

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

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

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

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

Ref country code: DE

Ref legal event code: R097

Ref document number: 602007032509

Country of ref document: DE

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

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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: 20131031

Ref country code: CH

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

Effective date: 20131031

26N No opposition filed

Effective date: 20140530

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602007032509

Country of ref document: DE

Effective date: 20140530

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

Ref country code: IE

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

Effective date: 20131026

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

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

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

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

Ref country code: LU

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

Effective date: 20131026

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20071026

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

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130828

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

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

Ref country code: FR

Payment date: 20200917

Year of fee payment: 14

Ref country code: GB

Payment date: 20200921

Year of fee payment: 14

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

Ref country code: DE

Payment date: 20200917

Year of fee payment: 14

Ref country code: IT

Payment date: 20200917

Year of fee payment: 14

Ref country code: ES

Payment date: 20201102

Year of fee payment: 14

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602007032509

Country of ref document: DE

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

Effective date: 20211026

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: 20211026

Ref country code: DE

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

Effective date: 20220503

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

Ref country code: FR

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

Effective date: 20211031

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: 20211026

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20230210

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 NON-PAYMENT OF DUE FEES

Effective date: 20211027