EP0015915B1 - Wärmeübertragersystem und verfahren zu seiner herstellung - Google Patents
Wärmeübertragersystem und verfahren zu seiner herstellung Download PDFInfo
- Publication number
- EP0015915B1 EP0015915B1 EP79900267A EP79900267A EP0015915B1 EP 0015915 B1 EP0015915 B1 EP 0015915B1 EP 79900267 A EP79900267 A EP 79900267A EP 79900267 A EP79900267 A EP 79900267A EP 0015915 B1 EP0015915 B1 EP 0015915B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- heat
- exchanger
- tube
- projections
- heat exchanger
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 229910052751 metal Inorganic materials 0.000 claims abstract description 8
- 239000002184 metal Substances 0.000 claims abstract description 8
- 238000005266 casting Methods 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 5
- 238000004873 anchoring Methods 0.000 claims description 2
- 230000003247 decreasing effect Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims description 2
- 238000005058 metal casting Methods 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 7
- 239000007788 liquid Substances 0.000 abstract description 3
- 238000004804 winding Methods 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
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
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/081—Heat exchange elements made from metals or metal alloys
- F28F21/084—Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
-
- 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
-
- 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
- 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
- F28D7/08—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 otherwise bent, e.g. in a serpentine or zig-zag
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F7/00—Elements not covered by group F28F1/00, F28F3/00 or F28F5/00
- F28F7/02—Blocks traversed by passages for heat-exchange media
-
- 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
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0054—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for nuclear applications
-
- 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
- the invention relates to a heat exchanger system with at least two heat exchanger elements, each of which has at least one tube bent in one plane or in a cylinder surface for a first medium involved in the heat transfer, with adjacent sections of the tube or the tubes in each case forming a sealed heat exchanger element heat transfer wall are connected.
- the invention is based on the object, starting from the heat exchanger system according to DE-A-22 37 430, to provide a heat exchanger system which can be operated at moderate temperatures in the range from 0 to 200.degree. C. and which enables a compact construction which is on the side of the second medium has a very large heat transfer surface and thus ensures a large heat transfer and which is inexpensive to produce.
- the wall is formed by a metallic cast body that tightly envelops the sections of the tube or tubes, the heat-conducting projections, the surface of which is a multiple of the tube inner surface that they account for, preferably ribs that run approximately parallel to one another , and that at least two heat exchanger elements are arranged relative to one another in such a way that at least one closed channel, into which the projections protrude, is formed for a second medium involved in the heat transfer.
- This design results in a smaller, more compact heat exchanger system, which has the additional advantage that, in the case of corrosive properties of the second medium, the pipe material is protected from corrosion attacks by the cast body. This also ensures that the two media always remain separate.
- FR-A-1 031 374 describes a heat exchanger intended for a hot gas piston engine, in which a plurality of pipes through which liquid flows and each bent into a loop are distributed in a circular ring, each pipe loop lying in a radial plane of the ring. All pipes are enclosed in a uniform cast body that has slit-shaped channels that run parallel to the pipe loops and are open on the inside of the circular ring without projections. The channels are closed by a special sleeve that lies against the inner circumference of the circular ring.
- This known heat exchanger takes up a lot of space and is expensive to manufacture.
- the heat exchanger system is to have the shape of a cuboid, this is best achieved by the tube or tubes of each heat exchanger element running in a serpentine or meandering manner in a single plane. If the supply and discharge lines have circular or annular connection cross sections, the heat exchanger elements are expediently designed in such a way that the pipe or the pipes run along helical lines on a single, fictitious pipe cylinder. Such a design also has particular advantages if the second medium has a pressure which differs greatly from the atmospheric pressure, because then each heat exchanger element forms a load-bearing wall with its cast body because of the coiled tube.
- the projections are advantageously designed as radially projecting ribs, essentially extending along helical lines.
- the protrusions can preferably be formed as turns in the case of pipes wound according to helical lines, which rise in the opposite sense to the turns of the pipes.
- a significant improvement in the heat transfer on the side of the second medium can be achieved in that the projections have a tree-like branched cross section, the passage area for the heat flow decreasing with increasing distance from the base of the projection.
- the heat exchangers can be produced in a particularly simple manner by a method according to the invention in that the tube of each heat exchanger element is bent and placed in a casting mold, the mold is poured out with a metal and the projections are machined out of the cast body, and that at least two heat exchanger elements are added be connected to a heat exchanger system.
- the tube of each heat exchanger element is bent and placed in a casting mold, that the mold is poured out with a metal and the casting body is machined in such a way that recesses for anchoring the rib-like parts forming the projections Parts are created which are caulked, soldered or welded into these recesses and that at least two heat exchanger elements are connected to form a heat exchanger system.
- Figure 1 shows a longitudinal section through a box-shaped heat exchanger system with several flat heat exchanger elements.
- Figure 2 shows a cross section 11-11 through the heat exchanger system of FIG. 1.
- Figure 3 is a cross section through a heat exchanger system with two concentrically arranged, circular cylindrical heat exchanger elements.
- FIG. 4 shows, on an enlarged scale, a longitudinal section IV-IV of the heat transfer system according to FIG. 3.
- FIG. 5 is, analogously to FIG. 3, a cross section through a modified heat exchanger system with two concentrically arranged heat exchanger elements.
- FIG. 6 shows a longitudinal section of a variant of FIG. 5.
- FIG. 7 shows a longitudinal section through a heat exchanger system with a plurality of heat exchanger elements, in each of which a tube is arranged after a spiral.
- FIG. 8 is a horizontal section through a heat transfer element in the levels VIII 1, VII 2 and Vii1 3 of FIG. 7.
- Figure 9 illustrates the cross section through two ribs with branches.
- Figure 10 shows a cross section of another embodiment of branched ribs and their mutual arrangement.
- Figures 11 and 12 each represent a cross section through further branched ribs.
- FIG. 13 shows a cross section through part of a circular cylindrical heat exchanger element with simple ribs which run along helical lines.
- Figure 14 shows the development of a cylinder with helical, interrupted ribs.
- each of the heat exchanger elements consists of a tube 3 which is bent back and forth in a vertical plane.
- the adjacent sections of each tube 3 are each cast with an aluminum body 4, the two side faces of which have cast-in projections 5 in the form of ribs and are parallel to the bending plane.
- the outermost ribs 5 'of each element 1 are somewhat longer than the other ribs and are each connected by a weld 6 to an abutting rib 5' of an adjacent heat exchanger element, as a result of which the aforementioned box shape and channels closed between these elements are created.
- an end plate 8 is welded on the free side, which extends over the entire outer ribbed surface of the respective heat exchanger element.
- a discharge line for the second medium is connected to the funnel thus formed, which is not apparent from the drawing.
- An identical funnel with a feed line for the second medium is located at the lower end of the heat exchanger system 2.
- the tubes 3 emerge laterally from the top and bottom of the heat transfer system 2 and end Flanges 13.
- the flanges 13 are connected to flanges of pipe sockets 14, the upper of which open into a distributor 15 and the lower, not shown in the drawing, into a collector.
- the distributor 15 and the collector are divided by bellows 17 because of the thermal expansion differences between them on the one hand and the cast aluminum body 4 on the other.
- the channels between the two end plates 8 and their adjacent heat exchanger elements 1 and the channels between adjacent heat exchanger elements 1 are flowed through from bottom to top by the second, heat-emitting, gaseous medium.
- the large heat transfer surface formed by the fins 5 compensates for the relatively poor heat transfer coefficient of the gas, so that the temperature difference between the heat-emitting gas and the heat-absorbing surface of the fins 5 remains relatively small.
- the fins 5 are wedge-shaped, so that the increased heat flow in the region of the fin nozzle can flow to the pipe 3 with a relatively low temperature drop. Since the water flowing in the pipe 3 ensures good heat transfer, there are also no high temperature differences on the water side.
- tubes 3a and 3b are wound according to helical lines.
- Each tube coil formed in this way is encased by an aluminum body 4a or 4b and forms a circular cylindrical heat exchanger element 1a or 1b.
- the heat exchanger element 1 a has radial longitudinal ribs 5 on its inside, while its outside is smooth.
- the heat exchanger element 1b has a greatly widened fin 23, in which a pipe section 24 connected to the upper end of the coiled tubing runs downwards in an axially parallel manner. Below the heat exchanger system, the pipe section 24 leads outwards, piercing a funnel wall (not shown).
- a gas flows through the highly jagged ring channel delimited by the surfaces of the ribs 5 between the two heat exchanger elements 1a and 1b, while a liquid flows through the two tubes 3a and 3b, which are preferably connected in parallel.
- ribs 5 are also arranged on the inside of the heat exchanger element 1b.
- the flow channel for the gas is delimited on the inside by a circular-cylindrical displacer 25.
- the heat exchanger element 1 a could also be provided with ribs on the outside and surrounded by a circular cylindrical jacket.
- the exemplary embodiment according to FIG. 6 differs from that according to FIG.
- the inner heat exchanger element 1b has two coils 3c and 3d, both of which open at their upper end into a common collecting tube 26, which is surrounded by an aluminum cast body 27, through the wall of a funnel 28 leads and finally ends outdoors with a flange 29.
- the upper end of the tube coil 3a leaves the heat exchanger element 1a outside the funnel 28 and is provided with a flange 29 '.
- five heat exchanger elements are designed as circular, cast disks 4f to 4k and are arranged coaxially one above the other, within which tubes 3f ... 3k which are bent according to spirals run.
- the fins 5 are each perpendicular to the plane of the tubes and are bent according to involutes.
- the heat exchanger elements are surrounded on the outside by a cylindrical jacket 130, which is tightly connected to the cast bodies 4f, 4h and 4k by flat ring plates 31, 32 and 33.
- shut-off disks 35 and 36 are arranged in the bore of the cast bodies 4g and 4i.
- the involute-shaped ribs 5 On the second uppermost cast body 4g (FIG. 8), the involute-shaped ribs 5, if they are followed in the counter-clockwise direction, on the top of the element (section VIII 1 ) from the outside inwards and on the underside from the inside out (section VIII 3 ).
- the uppermost cast body 4f has ribs only on its underside, which run like those on the top of the adjacent pane 4g.
- the cast body 4i is designed in the same way as 4g, while the intermediate cast body 4h has ribs that run in reverse: on the top, always referring to the counterclockwise direction, they lead from the inside to the outside and on the bottom from the outside to the inside.
- the lowermost cast body 4k only carries ribs on its upper side, which run from the inside to the outside.
- This rib arrangement ensures that the gaseous medium, which enters the stack of heat exchanger elements centrally from below through the inlet 50 of the heat exchanger system, flows outward in the channel between the mutually facing ribs 5 of the cast bodies 4i and 4k, through the lower one Annulus 42 between the cast body 4i and the jacket 30, rotating further in the counterclockwise direction, rises and flows inward in the counterclockwise direction through the channel between the cast bodies 4h and 4i. Continuously rotating in the same direction, it flows outwards into the upper annular space 42 'in the channel between the cast bodies 4g and 4h and finally, flowing inward via the channel between the cast bodies 4f and 4g, reaches the outlet opening 51 of the heat transfer system.
- each of the pipes 3g to 3i initially extends radially from the outside to the associated one Cast body, wherein the radial portion 38 located within the shell 30 is cast with aluminum.
- each tube 3g to 3i extends as a spiral 40, preferably as an involute with a small radial part, wound up against the inner edge of the cast body.
- each of the tubes 3g to 3i in each case passes into the level of the fins 5 on the underside of the heat exchanger element in question, where it is cast in as an involute tube 41 in a thickened fin 23 'which, like the neighboring fins, runs in an involute manner.
- each involute tube 41 merges into a radial tube section 43 which penetrates the jacket 30 and is cast with aluminum within the jacket.
- the tubes 3f and 3k also each have a radial tube section 39, which is, however, located outside the annular spaces 42 and 42 '.
- the spiral tubes 3f and 3k are led up and down out of the cast body and set continues as tube 44 or 45.
- the changes in direction of the tube are chosen to be as small as possible by the water circling in the same way within a heat exchanger element in the spiral tube 40 as well as in the involute tube 41.
- the spiral tube 40 in the cast bodies 4g and 4i is wound from the outside inwards in the counterclockwise direction, while that of the cast bodies 4h and 4k runs clockwise from the outside inwards.
- the pipes 3f ... 3k are expediently connected in series, according to the countercurrent principle, which cannot be implemented consistently here.
- the pipe section 39 of the cast body 4f is therefore connected to the involute pipe 41 of the cast body 4g, the involute pipe 44 forming the water inlet.
- the pipe section 38 of the cast body 4g is connected to the section 38 of the cast body 4h, the involute tube of which is connected to the section of the cast body 4i and finally the involute pipe of the cast body 4i to the section 39 of the lowermost cast body 4k.
- Practical considerations as well as thermodynamic calculations can also lead to a different circuit.
- FIGS. 9 to 12 While simple ribs are always provided in the exemplary embodiments described so far, it may also be expedient to ramify the ribs, as shown in FIGS. 9 to 12.
- flat grooves 56 are screwed into the cast body 55, which tightly surrounds the tube 3, into each of which a rib 57 is soldered.
- the ribs 57 have a stem-shaped central rib 58, from each of which four branch ribs 59 branch off.
- the trunk rib 38 thickens in accordance with the increasing heat flow against the rib foot 54, and the astra ribs 59 are inclined so that the heat flow reaches the rib foot 54 in a shorter way.
- the astocks 59 are also arranged such that the spaces for the medium flowing around the fins have a hydraulic radius that changes as little as possible.
- Ribs according to Fig. 10 are easy to cast, while the extrusion presents difficulties due to the uneven cross-sectional distribution.
- the cross-sectional shapes according to FIGS. 11 and 12, which are assembled by soldering simple angle profiles 60, are more favorable. These can be formed by folding sheet metal or by extrusion.
- the profiles 60 are preferably joined together with a first, high-melting solder to form a branched rib, which is then soldered into the grooves 56 of the cast body 55 with a second, less high-melting solder.
- a plurality of ribs 61 extend radially inward from a circular cylindrical heat exchanger element 60, the ribs running along helical lines.
- one (70) of the trailing edges 70, 71 is rounded off with a large radius.
- the consequence of this is that the Coanda effect causes a thin layer of the medium flowing between the ribs to pass through the gap between two successive ribs into the adjacent flow path. This phenomenon can further improve the heat transfer.
- the ribs which are inclined in FIG. 14 can also run in the axial direction, in which case the interruptions between the ribs can follow a helical line.
Landscapes
- 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH2800/78 | 1978-03-15 | ||
CH280078A CH625611A5 (enrdf_load_stackoverflow) | 1978-03-15 | 1978-03-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0015915A1 EP0015915A1 (de) | 1980-10-01 |
EP0015915B1 true EP0015915B1 (de) | 1982-09-22 |
Family
ID=4241865
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP79900267A Expired EP0015915B1 (de) | 1978-03-15 | 1979-10-12 | Wärmeübertragersystem und verfahren zu seiner herstellung |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0015915B1 (enrdf_load_stackoverflow) |
JP (1) | JPS55500151A (enrdf_load_stackoverflow) |
AU (1) | AU526929B2 (enrdf_load_stackoverflow) |
CH (1) | CH625611A5 (enrdf_load_stackoverflow) |
DE (1) | DE2963708D1 (enrdf_load_stackoverflow) |
WO (1) | WO1979000766A1 (enrdf_load_stackoverflow) |
ZA (1) | ZA791190B (enrdf_load_stackoverflow) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29604521U1 (de) * | 1996-03-11 | 1996-06-20 | SGL Technik GmbH, 86405 Meitingen | Aus Platten aufgebauter Wärmeaustauscherkörper |
EP3855104A4 (en) * | 2018-09-21 | 2021-11-10 | Sumitomo Precision Products Co., Ltd. | HEAT EXCHANGER |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3563119D1 (en) * | 1984-01-10 | 1988-07-07 | Kloeckner Humboldt Deutz Ag | Heat exchanger for two fluids, especially an air intake cooler for a combustion engine |
EP0627065B1 (en) * | 1992-02-28 | 1999-05-26 | Melanesia International Trust Company Limited | Heat exchanger assembly |
DE4302479A1 (de) * | 1993-01-29 | 1994-08-04 | Hans Dr Viesmann | Heizkessel für die Verbrennung flüssiger oder gasförmiger Brennstoffe |
WO1994023257A1 (en) * | 1993-03-29 | 1994-10-13 | Melanesia International Trust Company Limited | Heat exchanger assembly |
AUPP502698A0 (en) * | 1998-08-04 | 1998-08-27 | Andale Repetition Engineering Pty. Limited | Beverage chiller |
EP2202475B1 (en) * | 2008-12-23 | 2012-05-02 | Ching-Sung Kuo | Wing-spanning thermal-dissipating device |
CN103753161B (zh) * | 2013-12-30 | 2016-05-18 | 上海华谊集团装备工程有限公司 | 一种用于大型设备上的冷却加热盘管的加工工艺 |
WO2016057471A1 (en) * | 2014-10-07 | 2016-04-14 | Unison Industries, Llc | Spiral wound cross-flow heat exchanger |
US20170089643A1 (en) * | 2015-09-25 | 2017-03-30 | Westinghouse Electric Company, Llc. | Heat Exchanger |
CN111721150B (zh) * | 2020-07-27 | 2024-10-22 | 西安热工研究院有限公司 | 一种紧凑型多级串联pche换热器及换热方法 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR741113A (enrdf_load_stackoverflow) * | 1933-02-04 | |||
FR550944A (fr) * | 1922-05-03 | 1923-03-23 | Leblanc Vickers Maurice Sa | échangeur de chaleur |
US1571068A (en) * | 1922-08-07 | 1926-01-26 | Stancliffe Engineering Corp | Heat interchanger |
GB426114A (en) * | 1934-08-11 | 1935-03-27 | Charles Adolphe Hubert | A process for converting gilled tubes into heat exchanger elements having continuous ducts of uniform cross-sectional area for a heat exchanging medium |
US2707096A (en) * | 1950-01-26 | 1955-04-26 | Hartford Nat Bank & Trust Co | Heat exchanger |
CH287676A (fr) * | 1950-12-07 | 1952-12-15 | Somo Societe Pour Les Metaux O | Echangeur thermique. |
FR1032286A (fr) * | 1951-02-09 | 1953-06-30 | Brandt Soc Nouv Ets | élément échangeur thermique pour réfrigérateurs et radiateurs |
GB864946A (en) * | 1958-01-30 | 1961-04-12 | Green & Son Ltd | Improvements in or relating to gilled tubes |
FR1230106A (fr) * | 1959-03-03 | 1960-09-13 | Griscom Russell Co | Fabrication de tubes munis d'ailettes |
FR1354623A (fr) * | 1962-04-23 | 1964-03-06 | Nihon Genshiryoku Kenkyujo | Perfectionnements aux tubes échangeurs de chaleur à ailettes |
FR1405807A (fr) * | 1963-03-21 | 1965-07-16 | Commissariat Energie Atomique | Procédé d'usinage d'éléments tubulaires à ailettes pour échangeurs de chaleur |
GB987739A (en) * | 1963-05-01 | 1965-03-31 | Senior Economisers Ltd | Improvements in and relating to heat exchanger elements |
DE1926187A1 (de) * | 1969-05-22 | 1970-11-26 | Schoell Dr Ing Guenter | Waermeaustauschelement aus Werkstoffen mit geringer Waermeleitfaehigkeit und Festigkeit |
GB1424532A (en) * | 1972-03-20 | 1976-02-11 | Brown Sons Ltd James | Components using cast-in cooling tubes |
DE2256439A1 (de) * | 1972-11-17 | 1974-05-22 | Fritz Fischer | Rippenheizkoerper aus aluminiumguss |
JPS607183B2 (ja) * | 1977-08-12 | 1985-02-22 | 株式会社日立製作所 | 熱交換器 |
JPS5496438A (en) * | 1978-01-17 | 1979-07-30 | Asahi Glass Co Ltd | Ultrasonic one-side hot dipping equipment |
-
1978
- 1978-03-15 CH CH280078A patent/CH625611A5/de not_active IP Right Cessation
-
1979
- 1979-03-14 DE DE7979900267T patent/DE2963708D1/de not_active Expired
- 1979-03-14 JP JP50050079A patent/JPS55500151A/ja active Pending
- 1979-03-14 WO PCT/CH1979/000040 patent/WO1979000766A1/de unknown
- 1979-03-14 ZA ZA791190A patent/ZA791190B/xx unknown
- 1979-03-14 AU AU45112/79A patent/AU526929B2/en not_active Ceased
- 1979-10-12 EP EP79900267A patent/EP0015915B1/de not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29604521U1 (de) * | 1996-03-11 | 1996-06-20 | SGL Technik GmbH, 86405 Meitingen | Aus Platten aufgebauter Wärmeaustauscherkörper |
EP3855104A4 (en) * | 2018-09-21 | 2021-11-10 | Sumitomo Precision Products Co., Ltd. | HEAT EXCHANGER |
US11802742B2 (en) | 2018-09-21 | 2023-10-31 | Sumitomo Precision Products Co., Ltd. | Heat exchanger |
Also Published As
Publication number | Publication date |
---|---|
WO1979000766A1 (en) | 1979-10-04 |
ZA791190B (en) | 1980-03-26 |
DE2963708D1 (en) | 1982-11-04 |
AU526929B2 (en) | 1983-02-10 |
EP0015915A1 (de) | 1980-10-01 |
CH625611A5 (enrdf_load_stackoverflow) | 1981-09-30 |
AU4511279A (en) | 1979-09-20 |
JPS55500151A (enrdf_load_stackoverflow) | 1980-03-21 |
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