EP4090901B1 - Energieaustasuchapparat zwischen medien mit verbesserter struktur und leistung - Google Patents

Energieaustasuchapparat zwischen medien mit verbesserter struktur und leistung Download PDF

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Publication number
EP4090901B1
EP4090901B1 EP21702712.7A EP21702712A EP4090901B1 EP 4090901 B1 EP4090901 B1 EP 4090901B1 EP 21702712 A EP21702712 A EP 21702712A EP 4090901 B1 EP4090901 B1 EP 4090901B1
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EP
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Prior art keywords
coil
coils
heat exchanger
fluid
structural
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English (en)
French (fr)
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EP4090901A1 (de
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Aleksandar Stamenic
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Stamenic Aleksandar
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Individual
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    • 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
    • F28D7/04—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 being spirally coiled
    • 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
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/0243—Header boxes having a circular cross-section
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/026—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • F28F9/0265—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits by using guiding means or impingement means inside the header box
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2225/00—Reinforcing means
    • F28F2225/04—Reinforcing means for conduits

Definitions

  • the invention generally belongs to the field of heat exchangers. According to the International Patent Classification (IPC Intel.), the present invention is classified and designated F28, a broader classification, which refers to heat exchange in general.
  • IPC Intel. International Patent Classification
  • F28 a broader classification, which refers to heat exchange in general.
  • the invention is characterized by its structure, it can also be designated F28F - structural elements of devices for heat exchange and transfer for general application.
  • the inventors aimed to improve the thermal performances of the heat exchanger core, primarily in a way that the essential parameters of the working fluids can be easily controlled.
  • the inventors have designed a heat exchanger that is easy to manufacture, use and maintain, suitable for use in a variety of commercial and residential premises, and in a variety of industries. Also, the inventors aimed to design a heat exchanger that has a smaller mass in relation to the existing heat exchangers of the same power and the same material.
  • heat exchangers that include a structure that has helical tubes, a stepwise distance between the tubes, and a crossflow of fluids such as EP0351247 (A2 ) or US20100096115A1 - Multiple concentric cylindrical co-coiled heat exchanger or US3403727A - Crossflow countercurrent heat exchanger with inner and outer-tube sections made up of closely packed coaxially nested layers of helicoidally wound tubes.
  • a device according to the preamble of claim 1 is disclosed in WO 2009/024854 A2 .
  • the invention is defined in claim 1.
  • the present invention is a design solution of a counterflow and crossflow heat exchanger, made by winding helical tubes (coils) successively through structural reinforcements, which are an integral part of the heat exchanger core, and which enable stepwise/zigzag arrangement of coils, and arrangement of tubes of each coil exactly in the middle position and at the same distance between the tubes of adjacent coils in the entire heat exchanger core, and together they make the heat exchanger surface.
  • Structural reinforcements are made so that their inner and outer edge correspond to the required coil pitch and that the inner edge additionally follows the angle of the coil on which they are placed and that the outer edge follows the angle of the next coil.
  • this device may include a central router with conical extensions and structural reinforcement support, wherein a basic structural reinforcement on which the first helical coil is wound is placed on the central router having conical extensions on both sides, and wherein the central router is to direct the flow of the first fluid towards the coils and prevent the passage of the first fluid through the central part of the heat exchanger core, and wherein the conical extensions direct the flow of the first fluid as close as possible to the outer walls of the coils through which the second fluid moves.
  • All odd- numbered coils are parallel to each other in both transverse and longitudinal planes of the heat exchange core, while also all even- numbered coils (the second, the fourth, the sixth,...) are parallel to each other in both transverse and longitudinal planes of the heat exchange core.
  • the diameters of the d pipes from which all the coils are made are the same.
  • Each coil in the heat exchanger core has a different diameter, wherein all coils have the same coil pitch, and each coil has a different thread angle.
  • the structural reinforcements have a sinusoidal or wavy or wavy-zigzag shape, whereby the shape of the structural reinforcements represents bearings on which the coils move when wound into the heat exchanger core.
  • Structural reinforcements comprise an inner edge and an outer edge, wherein they correspond to the required coil pitch, and wherein the inner edge additionally follows the thread angle of the coil on which they are placed, and the outer edge follows the angle of the next coil, wherein the first coil has the diameter, the pitch and the thread angle of the first coil.
  • the first structural reinforcement which is placed on the first coil and follows the pitch, additionally follows the angle of the first coil with the inner edge, and with the outer edge, it follows the angle of the next second coil and so on till the last wound coil.
  • At least two structural reinforcements are placed on each coil in turn, and most preferably three or more, arranged at equal distances along the diameters of the coils with structural reinforcements placed on each subsequent coil so that they are not in the same plane with the structural reinforcements of the previous coil.
  • the basic structural reinforcements are connected by welding to the central router and each subsequent structural reinforcement to the next wound coil in turn in the heat exchanger core, where the structural reinforcements also enable stepwise or zigzag arrangement of coils, and the arrangement of tubes of each coil exactly in the middle position and at the same distance between the tubes of adjacent coils in the entire heat exchanger core, transverse to the second fluid.
  • This energy exchange device may further comprise structural reinforcement supports, on which holes are drilled so that one end of the structural reinforcement is inserted into each hole, wherein each of the structural reinforcement supports has as many holes drilled both vertically and horizontally as necessary to place at least two structural reinforcements on each coil.
  • the advantage of the present invention is reflected in simple manufacture, improved thermal performances, simple control of essential parameters of the working fluids, easy modularity for application in commercial, residential premises, and in various industries, and easy modularity for smaller/higher powers.
  • the energy exchange device between media with improved structure and performances in one embodiment contains the following parts: sheath 104, shield 106, commutator (collector) 107, coils or helical tubes 201, 2012, 203, 204, 205, 206, 207, 208, 289, 290, tubes with expansions 110, central router 101 with conical extensions 102, structural reinforcements 300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390 and structural reinforcement support 105.
  • central router 101 Usually, basic structural reinforcements 300 are placed on both sides of the central router 101 with conical extensions on which the first helical tube (coil) 201 will be wound.
  • the task of the central router 101 ist to direct the flow of the first fluid 400 towards the coils 201, 202, 203, 204, 205, 206, 207, 208, 289, 290 and to prevent the passage of the first fluid 400 through the central part of the heat exchanger core 200.
  • Conical extensions 102 direct the flow of the first fluid 400 as close as possible to the outer walls of the coils 201, 202, 203, 204, 205, 206, 207, 208, 289, 290 through which the second fluid moves 402.
  • Central router 101 is made of pipes of a defined diameter to which conical extensions 102 are welded on both sides.
  • Coils of the heat exchanger core 200 are formed on the tools.
  • a tool can be a cylinder of a defined diameter and length, made of plastic or metal with channels that correspond to the required coil and its characteristics, whereby helical tubes (coils) of given parameters are produced by turning the tool. All coils with an odd number e.g. 201, 203 to 289 are parallel in both transverse and longitudinal planes of the heat exchanger core 200. The same applies to even- numbered coils 202, 204, etc.
  • the diameters of d pipes 295, from which all coils are made, are all the same.
  • Each coil 201 to 289, 290 has a different diameter, and so is the diameter of the first coil 501, the diameter of the penultimate coil 589, and the diameter of the last coil 590 defined. All coils have the same coil pitch, but a different thread angle, so the first coil has a thread angle 601, the thread angle of the penultimate coil is 689, while the angle of the last coil is 690, therefore the tool is different for each coil. Coils can also be made on modified tools for pipe bending, e.g., three-cylinder, drum-like tools, and other tools known from the prior art.
  • the pipes from which the coils are made can be made of copper, aluminum, stainless steel, dual metals, etc.
  • the heat exchanger core 200 can be connected to the heating or cooling systems vertically or horizontally.
  • Structural reinforcements 300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390 enable coil winding into the heat exchanger core 200.
  • Structural reinforcements 300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390 have a sinusoidal/wavy/wavy-zigzag shape. This form of structural reinforcements enables bearings on which the coils 201, 202, 203, 204, 205, 206, 207, 208, 289, 290 move when wound into the heat exchanger core 200. They are placed parallel to the longitudinal axis 112, and the inner edge 291 and the outer edge 292 are designed to fit the required coil pitch 600.
  • the thread angle of coils 601, 689, 690 for each coil 201, 202, 203, 204, 205, 206, 207, 208, 289, 290 is different, all structural reinforcements are different, made so that the inner edge 291 additionally follows the thread angle of the coil on which they are placed, and the outer edge 292 follows the angle of the next coil.
  • the first coil 201 has a diameter 501, a thread pitch 600, a diameter of d pipe of which the coil 201 is made, a thread angle 601 and the first structural reinforcement 301, and so on for each subsequent coil successively.
  • the first structural reinforcement 301 placed on the coil 201 that follows the pitch 600 additionally follows the angle of the coil 601 for the first coil 201 with the inner edge 291 and with the outer edge 292 it follows the angle 602 of the next second coil 202 and so on to the last wound coil.
  • At least two structural reinforcements 300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390 and most preferably three or more, arranged at equal distances along the diameters of the coils 201, 289,290 are placed on each coil in turn.
  • the structural reinforcements are placed so that they are not in the same plane as the reinforcements of the previous coil.
  • the basic structural reinforcement 300 is connected by welding to the central router 101, and each subsequent structural reinforcement 301, 302, 303, 304, 305, 306, 307, 308, 389, 390 to the next wound coil in turn into the heat exchanger core 200.
  • Structural reinforcements also enable a stepwise/zigzag arrangement of the coils and the arrangement of the tubes of each coil exactly in the middle position and at the same distance between the tubes 320 (transverse to the second fluid 402) of adjacent coils in the entire heat exchanger core 200. After placing the structural reinforcements on the last wound coil 289 or 290, a cylindrical sheath 104 of the heat exchanger is placed on them.
  • the basic structural reinforcements 300 and the last structural reinforcements 390 can also be flat, without zigzag waves, and other aforementioned characteristics, and can be flush with the structural reinforcement of the next coil, which applies to the basic structural reinforcements 300, or with the structural reinforcement of the previous coil, which applies to the last structural reinforcements 390.
  • the coils 201,289,290 with their pair of structural reinforcements 301, 389, 390 in turn, can be welded, before being wound into the heat exchanger core 200, and then individually wound into the heat exchanger core successively.
  • Structural reinforcements ensure the stability of the entire heat exchanger core 200, reduction of vibrations, and a uniform distance between the coil tubes 320. They additionally increase the heat exchange surface and together with the coils they form the total exchange surface. Other modifications are also possible in the way of bonding structural reinforcements besides welding e.g. soldering, gluing, etc.
  • Structural reinforcements are most preferably made of the same type of material as the coils.
  • Structural reinforcements are made of full section materials, strips, wires, etc., or capillary tubes (microchannel tubes). They are made in their molds or are being cut, for example by laser cutting, to obtain a specific shape that ensures that the coils are easily wound, successively, into the heat exchanger core.
  • the thickness 310 of the material from which the structural reinforcements are made is one of the reasons that affect the size (interspace-gap) of the distance 320.
  • Each structural reinforcement has the same thickness 310 of the material from which it is made.
  • the size of the distance 320 decreases or increases, but always ensures a stepwise/zigzag arrangement of coils, and the arrangement of tubes of each coil exactly in the middle position and at the same distance 320 between the tubes of adjacent coils in the entire heat exchanger core 200.
  • FIGS 9 to 15 show examples of the heat exchanger core 200 with supports 105 with eight coils 201 to 208. All structural reinforcements that are inserted into the supports 105 are made according to the previously described principle. Each of the supports 105 is, most preferably, made of two identical pipes or round bars with a full section, which are welded at their centers at right angles. Structural reinforcements are inserted between the supports 105 in the holes 1050 drilled therein. In the above example, the last structural reinforcement is the eighth structural reinforcement 308.
  • the supports 105 are made of the same type of material as the central router 101, with a diameter not larger than the diameter of the d coil pipe 295.
  • Each of the supports 105 has as many holes drilled both vertically and horizontally as necessary to place at least two structural reinforcements on each coil.
  • the supports 105 can be welded to the central router 101 before welding its conical extensions 102. After inserting all structural reinforcements into the supports 105, Figures 9 to 11 show, coils 201 to 208 being rotated in turn, forming the heat exchanger core 200. Also, structural reinforcements can be inserted into the supports 105 individually in turn, after winding each coil.
  • the length 120 and the diameter 130 of the heat exchanger core are determined, the diameter of d pipe 295 for making coils, wall thickness 311 of pipes from which coils are made, the diameter of the first coil 501 to the diameter of the last coil 590 in turn, the number of coils and the required distance 320 are defined.
  • the distance 320 is easily regulated, which enables simple control of the desired fluid pressure drop 400.
  • the length of each coil depends on the diameter of each coil, as well as the length 120 of the core itself.
  • Example 2 Example of an optimized heat exchanger according to the present invention for a required power of 1850W air-water: Basic parameters for manufacturing a heat exchanger core First fluid 400: air 0.0934 [kg/s] mass flow of the first fluid 400 32.0000 [C] inlet temperature of the first fluid 400 Second fluid 402: water 4.8300 [lt/min] second fluid flow 402 8.0000 [C] inlet temperature of the second fluid 402
  • the required pressure drop of the first fluid is 80 Pa and of the second fluid 6 kPa
  • each is cut at its beginning and end in such a way that all coils of the heat exchanger core reach the same normal plane on axis 112.
  • tubes 110 with expansions of the same length are then placed on each coil individually. Holes 103 for the passage of tubes 110 with expansions that further enter straight into the commutator (collector) 107 are drilled on sheath 104. Tubes with expansions 110 can be welded, glued, etc., to coils.
  • Shield 106 is placed between the core sheath 104 and the tubes with expansions 110 to prevent the first fluid 400 flow outside the heat exchanger core 200.
  • Tubes with expansions 110 are most preferably made of the same material and diameter of d pipe 295 as the coils and are widened at one end where they will be drawn on the coils with standard pipe expansion tools.
  • the commutator (collector) 107 additionally has openings 108 for venting the heat exchanger core 200.
  • the first fluid 400 moves around the coils and the second fluid 402 through the coils.
  • the inlet 410 of the first fluid 400 concerning the inlet 420 of the second fluid 402 is located on the opposite side of the heat exchanger core, whereby the fluids move in opposite directions.
  • the first fluid 400 further moves approximately perpendicularly (crosswise/ normally) concerning the axis of the coil tube. In this arrangement coils greatly interfere with the flow of the first fluid 400, so there is continuous turbulence of the first fluid 400 around the coils. This enhances the heat exchange but also increases the pressure drop of the first fluid 400.
  • the tubes of each coil are exactly in the middle position and at the same distance 320 (transverse to the second fluid 402) between the tubes of adjacent coils, the first fluid 400 is forced to move near the walls of the coil tubes.
  • the tube of, e.g., the fifth coil 205, as shown in Figure 16 is located exactly in the middle position between the adjacent tubes of the fourth coil 204 and the sixth coil 206.
  • the flow of the first fluid 400, which passes between the fourth coil 204 and the sixth coil 206 directly strikes the tube of the fifth coil 205.
  • the flow of the first fluid 400, which passes between the fourth coil 204 and the sixth coil 206 does not release or receive sufficient heat because it is located in the middle of the passage between the fourth coil 204 and the sixth coil 206, at the first point 430. But it further passes near the pipe wall of the fifth coil 205 at the second point 431, where a lot of heat is released or received.
  • the heat transfer can be improved by reducing the distance from the pipe walls to the first fluid 400, i.e., by reducing the distance 320. If the distance 320 is very small, the flow of the first fluid 400 is forced to pass very closely to the pipe walls, therefore is the heat transfer higher. Basically, the thermal resistance of the flow of the first fluid 400 is proportional to the distance 320, so the heat transfer rate is proportional to the inverse length of the distance 320 between the coil tubes: Q ⁇ ⁇ Lg -1
  • the first fluid 400 is forced to pass through narrow passages, so more mechanical work is necessary to overcome the resistance, i.e., there is an increase in pressure drop of the first fluid 400 through the heat exchanger core 200. This is an undesirable effect because part of the pressure is lost.
  • the pressure drop of the first fluid 400 increases proportionally to the inverse cubic of the distance 320, i.e., ⁇ P fluidsS ⁇ L g -3 .
  • the above-mentioned method of the present invention manufacture achieves the maximum heat exchange for the default pressure drop of the first fluid 400.
  • This design enables the manufacture of an axial helical countercurrent (of opposite direction) and crossflow heat exchanger core 200, and a stepwise arrangement of coils, which is simply made by winding helical tubes (coils) successively over structural reinforcements, thus achieving high heat performances and simple control of the most important parameters.
  • An additional advantage of the present heat exchanger core 200 is the mechanism of "self-cleaning" of the interior of the coils. Scale, other sediments, and contaminants inside the coils cause a localized increase in the speed of the second fluid 402, which increases the “pushing" of the impurity by friction between the second fluid 402 and the impurity, in such a way the inner surface of the coil cleans "itself".
  • the diameters 412 of the inlet of the first fluid 410 and the outlet of the first fluid 411, as well as the diameter 422 of the inlet of the second fluid 420 and the outlet of the second fluid 421 of the heat exchanger core, as shown in Figure 17 , can be reduced or increased for connection to standard connectors.
  • the increase of the required power of the present invention can also be accomplished by binding lower powers of the heat exchanger core 200 made according to the same principle.
  • Figure 12 shows an example of binding multiple heat exchanger cores 200 of lower powers made according to the present invention to provide a single higher power heat exchanger.
  • Figure 9 shows an embodiment of the heat exchanger core 200 in section with 8 coils 201, 202, 203, 204, 205, 206, 207, 208 so that it can be seen that first comes the basic structural reinforcement 300, then the first coil 201, then the first structural reinforcement 301 on it, and then the second coil 202, which is placed in the recesses 294, and on the bulges 293 of the first structural reinforcement 301 comes the third coil 203 on which comes the third structural reinforcement 303 on which comes the fourth coil 204, which is placed in the recess 294 of the third structural reinforcement 303, and on the bulges 293 of the third structural reinforcement 303 comes the fifth coil 205 on which comes the fifth structural reinforcement 305, and on it the sixth coil 206, which is placed in the recesses 294, and on the bulges 293 of the fifth structural reinforcement 305 comes the seventh coil
  • Figure 11 illustrates one of the applications of the invention in the automotive industry on a complete heat exchanger for cooling (intercooler) highly compressed hot air, where its purpose is to lower the air temperature with as little pressure loss as possible.

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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)

Claims (10)

  1. Gegenstrom- und Querstrom-Energieaustauschvorrichtung zwischen Medien mit verbesserter Struktur und Leistung, dadurch gekennzeichnet, dass sie Spulen (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) enthält, die aus Rohren und strukturellen Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) hergestellt sind, wobei die Spulen (201, 202, 203, 203, 204, 205, 206, 207, 208, 289, 290) und strukturelle Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) bilden den Wärmetauscherkern (200), wobei die Spulen (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) nacheinander über strukturelle Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) gewickelt sind, wobei die Spulen eine stufenweise/zickzackförmige Anordnung (201, 202, 203, 204, 205, 206, 207, 208, 289, 290), und wobei die Anordnung der Rohre jeder Spule genau in der mittleren Position und im gleichen Abstand zwischen den Rohren benachbarter Spulen in dem gesamten Wärmetauscherkern (200) liegt, wobei das erste Fluid (400) und das zweite Fluid (402) durch die Energieaustauschvorrichtung strömen können, ferner umfassend einen zentralen Fräser (101) mit konischen Verlängerungen (102), einer strukturellen Verstärkung (105) und einer grundlegenden strukturellen Verstärkung (300), wobei eine grundlegende strukturelle Verstärkung (300) auf beiden Seiten des zentralen Routers (101) mit konischen Verlängerungen (102) platziert ist, an die die erste spiralförmige Spule (201) gewickelt ist, und wobei der zentrale Router (101) die Strömung des ersten Fluids (400) in Richtung der Spulen (201) lenkt, 202, 203, 204, 205, 206, 207, 208, 289, 290) und verhindert den Durchgang des ersten Fluids (400) durch den zentralen Teil des Wärmetauscherkerns (200), und wobei die konischen Verlängerungen (102) den Durchfluss des ersten Fluids (400) zu den Außenwänden der Spulen (201, 202, 203, 204, 205, 206, 207) leiten, 208, 289, 290), durch die sich das zweite Fluid (402) bewegt.
  2. Energieaustauschvorrichtung, wie im früheren Patentanspruch beansprucht, dadurch gekennzeichnet, dass alle ungeraden Spulen (201, 203, 205, 207, 289) sowohl in der Querals auch in der Längsebene des Wärmetauscherkerns (200) parallel zueinander sind und alle geradzahligen Spulen (202, 204, 206, 208, 290) ebenfalls sowohl in der Quer- als auch in der Längsebene des Wärmetauscherkerns (200) zueinander parallel sind.
  3. Energieaustauschvorrichtung, wie in einem der früheren Patentansprüche beansprucht, dadurch gekennzeichnet, dass die Durchmesser der d-Rohre (295), aus denen alle Spulen hergestellt sind, gleich sind.
  4. Energieaustauschvorrichtung, wie in einem der früheren Patentansprüche beansprucht, dadurch gekennzeichnet, dass jede Spule (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) im Wärmetauscherkern (200) einen unterschiedlichen Durchmesser (501, 589, 590) aufweist, wobei alle Spulen die gleiche Spulenteilung (600) aufweisen und wobei jede Spule (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) hat einen anderen Fadenwinkel (601, 689, 690).
  5. Energieaustauschvorrichtung, wie in einem der früheren Patentansprüche beansprucht, dadurch gekennzeichnet, dass die strukturellen Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) eine sinusförmige oder wellenförmige oder wellenförmige oder wellenförmige Zickzackform aufweisen, wobei die Form der strukturellen Verstärkungen die Lager bildet, auf denen sich die Spulen bewegen (201, 202, 203, 204, 205, 206, 207, 208, 289, 290), wenn sie in den Wärmetauscherkern (200) eingewickelt sind.
  6. Energieaustauschvorrichtung nach Anspruch 5, dadurch gekennzeichnet, dass die strukturellen Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) eine Innenkante (291) und eine Außenkante (292) umfassen, die der erforderlichen Spulensteigung (600) entsprechen, und wobei die Innenkante (291) zusätzlich dem Gewindewinkel der Spule (201, 202, 203, 204, 205, 206, 207, 208, 289, 290), auf denen sie platziert sind, und die Außenkante (292) dem Winkel der nächsten Windung folgt, wobei die erste Windung (201) einen Durchmesser der ersten Windung (501), eine Windungssteigung (600) und einen Gewindewinkel der ersten Windung (601) aufweist.
  7. Energieaustauschvorrichtung nach Anspruch 6, dadurch gekennzeichnet, dass die erste strukturelle Verstärkung (301), die auf die erste Spule (201) aufgesetzt ist und der Steigung (600) folgt, zusätzlich dem Winkel der ersten Spule (601) mit der Innenkante (291) folgt und mit der Außenkante (292) dem Winkel der nächsten zweiten Spule (602) folgt, und so weiter bis zur letzten gewickelten Spule.
  8. Energieaustauschvorrichtung, wie in einem der früheren Patentansprüche beansprucht, dadurch gekennzeichnet, dass mindestens zwei strukturelle Verstärkungen (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) oder drei strukturelle Verstärkungen oder mehr nacheinander auf jeder Spule (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) angebracht sind, in gleichen Abständen entlang der Durchmesser der Windungen (201, 202, 203, 204, 205, 206, 207, 208, 289, 290) angeordnet sind, wobei strukturelle Verstärkungen auf jeder nachfolgenden Windung so platziert sind, dass sie sich nicht in derselben Ebene mit den strukturellen Verstärkungen der vorherigen Windung befinden.
  9. Energieaustauschvorrichtung, wie in einem der früheren Patentansprüche beansprucht, dadurch gekennzeichnet, dass die grundlegenden strukturellen Verstärkungen (300) durch Schweißen mit dem zentralen Router (101) verbunden sind und jede nachfolgende strukturelle Verstärkung (300, 301, 302, 303, 304, 305, 306, 307, 308, 389, 390) wiederum mit der nächsten gewickelten Spule in den Wärmetauscherkern (200) verbunden ist, wobei eine stufenweise oder zickzackförmige Anordnung der Spulen vorliegt und die Anordnung der Rohre jeder Spule genau in der mittleren Position und im gleichen Abstand zwischen den Rohren (320) der benachbarten Spulen im gesamten Wärmetauscherkern (200) quer zur zweiten Flüssigkeit (402) liegt.
  10. Energieaustauschvorrichtung, wie sie in einem der früheren Patentansprüche beansprucht wird, dadurch gekennzeichnet, dass sie strukturelle Verstärkungsstützen (105) umfasst, auf denen Löcher (1050) gebohrt sind, so dass ein Ende der strukturellen Verstärkung in ein einzelnes Loch (1050) eingeführt wird, wobei jede der strukturellen Verstärkungsstützen (105) sowohl vertikal als auch horizontal so viele perforierte Löcher aufweist, wie erforderlich sind, um mindestens zwei strukturelle Verstärkungen auf jeder Spule zu platzieren.
EP21702712.7A 2020-01-13 2021-01-11 Energieaustasuchapparat zwischen medien mit verbesserter struktur und leistung Active EP4090901B1 (de)

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RS20200036A RS20200036A1 (sr) 2020-01-13 2020-01-13 Uređaj za razmenu energije između medijuma sa poboljšanom strukturom i performansama
PCT/IB2021/050174 WO2021144682A1 (en) 2020-01-13 2021-01-11 Energy exchange device between media with improved structure and performances

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GB685848A (en) 1950-01-24 1953-01-14 Vickers Electrical Co Ltd Improvements relating to the construction of tubular heat exchangers
US3212571A (en) * 1962-12-31 1965-10-19 Combustion Eng Tube bundle for shell and tube type heat exchanger formed of spirally wound coil segments
DE1501519B2 (de) 1965-04-30 1971-02-25 Linde Ag, 6200 Wiesbaden Kreuzgegenstromer
WO1988001362A1 (en) 1986-08-21 1988-02-25 Emil Bader Countercurrent heat-exchanger with helical bank of tubes
EP0351247A3 (de) 1988-07-15 1990-04-25 Roberts, E. Dawson Wärmerückgewinnung aus Abgasen
ITMI20071685A1 (it) * 2007-08-22 2009-02-23 Luciano Cinotti Reattore nucleare, in particolare reattore nucleare raffreddato a metallo liquido, con scambiatore di calore primario compatto
GB2463482B (en) * 2008-09-12 2012-05-02 Tanjung Citech Uk Ltd A heat exchange unit
US20100096115A1 (en) 2008-10-07 2010-04-22 Donald Charles Erickson Multiple concentric cylindrical co-coiled heat exchanger
US11162424B2 (en) * 2013-10-11 2021-11-02 Reaction Engines Ltd Heat exchangers
GB2521114B (en) * 2013-10-11 2017-05-24 Reaction Engines Ltd Heat exchangers
GB201319284D0 (en) * 2013-10-31 2013-12-18 Heat Recovery Solutions Ltd Heat exchange array

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