EP1398592A1 - Flachrohr-Wärmeübertrager - Google Patents
Flachrohr-Wärmeübertrager Download PDFInfo
- Publication number
- EP1398592A1 EP1398592A1 EP20030020179 EP03020179A EP1398592A1 EP 1398592 A1 EP1398592 A1 EP 1398592A1 EP 20030020179 EP20030020179 EP 20030020179 EP 03020179 A EP03020179 A EP 03020179A EP 1398592 A1 EP1398592 A1 EP 1398592A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- heat exchanger
- exchanger according
- rib
- medium
- ribs
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000463 material Substances 0.000 claims abstract description 8
- 210000002816 gill Anatomy 0.000 claims description 14
- 230000002452 interceptive effect Effects 0.000 claims description 8
- 239000003570 air Substances 0.000 description 29
- 239000002826 coolant Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 238000004049 embossing Methods 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 238000004378 air conditioning Methods 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000005499 meniscus Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 208000008918 voyeurism Diseases 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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/126—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 consisting of zig-zag shaped fins
- F28F1/128—Fins with openings, e.g. louvered fins
Definitions
- the invention relates to a heat exchanger with pipes and ribs the preamble of claim 1.
- the corrugated fins are approximately zigzag-shaped, d. H. they form with the walls of the flat tubes about triangular Flow channels, which in each case two rib surfaces to each other are arranged inclined (V-type).
- the newly formed ribbed surfaces are occupied with so-called gills, d. H. with slits through which the Air is deflected from one flow channel into the adjacent one.
- This Rib configuration serves on the one hand to increase the heat transfer surface on the air side and on the other hand the improvement of the heat transfer by increasing the turbulence.
- boundary layers are formed by the gills each be broken up again.
- a modified ribbed form the so-called parallel rib or U-type, was known from US-A 5,271,478, also for a soldered one Flat-tube heat exchanger.
- Rib are the rib surfaces arranged here parallel to each other, d. H.
- the rib surfaces and the tube walls form approximately rectangular Flow channels for the air.
- the rib areas are with gills occupied, with the gill angle another way to influence the boundary layers and the turbulence offers.
- the solution to this problem arises from the features of claim 1.
- the invention is based on the recognition that the air flow or the heat transfer in the areas of the pipe rib contact point can still be improved - therefore, there are additional according to the invention there Disturbing elements in a different geometric configuration provided, which act essentially as a vortex generator and thus a Turbulence of the flow result.
- Disturbing elements in a different geometric configuration provided, which act essentially as a vortex generator and thus a Turbulence of the flow result.
- erfindungsgemä ⁇ e Measure are also in the pipe wall near the rib the Boundary layers broken up or disturbed. It thus comes to an improved Heat transfer without the rib configuration significantly would have to be changed, d. H. without appreciable cost increase.
- the Interference elements according to the invention can basically be found in the above-mentioned Rib forms, d. H.
- the curved rib section has a flat central portion. This will be the rib base slightly widened and the necessary space for the arrangement of the interfering elements created.
- interfering elements themselves can be the most diverse embodiments have, with an expression of the ribbed sheet in the form of a round or elongated knob or in the form of a truncated cone or a Cone tip advantageous formations are relatively simple in the conventional embossing of the rib.
- a further advantageous embodiment is partial from the ribbed plate cut-out or punched-out and bent-out surface elements, z. B. in the form of a ramp which forms a trailing edge for the air flow and thus causes a turbulence.
- lobes from the ribbed plate bent out and placed in parallel or obliquely in the air flow become.
- the angle of attack of the lobes or flags results also a turbulence.
- the disturbing elements unfold their maximum effect, if they are within given dimensions lie, which also result from the dependent claims.
- the upper limit for the height of the interfering elements is that they do not protrude into the area of the gill flow and also the pressure loss the air flow may not increase significantly.
- similar interference elements arranged in or on the pipe wall between two wave crests be, for. B. by impressing the pipe wall inwards, d. H. to Liquid side. Also an expression of the pipe wall to the air side is possible, for. In the form of so-called winglets, d. H. V-shaped Forms.
- Fig. 1 shows a corrugated fin 1 only partially shown in cross section, arranged between two flat tubes 2, 3, which are only partially shown as pipe wall pieces.
- the corrugated fin 1 and the flat tubes 2, 3 are parts of a heat exchanger network, not shown, which is part of a heat exchanger in a known type.
- heat exchangers can be, for example, coolant radiators for cooling an internal combustion engine of a motor vehicle or else refrigerant condensers as part of an automotive air conditioning system.
- Both heat exchangers have in common that a liquid and / or vapor medium flows through the tubes, while the outside of the tubes, whose surface is enlarged by the corrugated fins, is exposed to ambient air. The air is thereby promoted by back pressure or by a blower.
- the corrugated fin 1 has two mutually inclined, d. H. a point Angle with each other forming rib surfaces 4, 5, which has a curved piece 6, the so-called wave crest are interconnected.
- the wave crest 6 is soldered to the pipe wall 2.
- the ribbed surfaces 4, 5 have so-called gills 7, 8, each up to the beginning of the elbow 6, d. H. up to a distance a to the pipe wall 2, 3.
- the Rib surfaces 4, 5 form with the pipe wall 3 is an approximately triangular Flow channel 9.
- the average distance of the rib surfaces 4, 5 is in a Center plane measured m and is denoted by t.
- the corrugated fin 1 extends to the right and left in analogue training and with the same division t.
- a recess 11 formed in the pipe wall 3 is an additional option to the rib side interfering element 10 thought.
- Fig. 2 shows another rib shape, namely a so-called parallel rib 12 with parallel to each other or U-shaped rib surfaces 13, 14, which are interconnected via a bend piece 15.
- the two rib surfaces 14, 15 also have known gills 16, 17, which have a length l and thus do not extend over the entire channel cross-section, but in each case have a distance a from the pipe walls 18.
- the elbow 15 is composed of three sections, namely two outer approximately circularly curved portions 15a, 15b and a middle relatively flat portion 15c together.
- the rib surfaces 13, 14 in conjunction with the elbow 15 and the tube wall 19 thus form an approximately rectangular flow channel 20 with a constant rib spacing or a rib pitch t.
- a knob-shaped interference element 21 is arranged, which is formed from the rib material in the direction of the flow channel 20.
- the contour of this knob-shaped interference element 21 shows a view in the direction A: the shape 21 has an approximately oval contour with a longitudinal extent K and a width B.
- These interference elements 21 are - as also apparent from the following representations - aligned in the air flow direction one behind the other, so that the boundary layer is disturbed and turbulence is generated in these areas.
- a turbulent flow is generated.
- Fig. 3 shows a parallel rib 22 of the same configuration as the parallel rib 12 in Fig. 2 with the difference that instead of the knob-like expression 21 here a metal strip in the form of a flag 23 is provided as a disruptive element.
- This flag 23 extends with a height H, which corresponds approximately to the distance a, in the air flow channel, ie until the beginning of the gills.
- Fig. 4 shows a longitudinal section through a rib or air flow channel with a view of a rib surface 30 with gills 31.
- the rib 30 is soldered with its upper crest 30 a with a tube wall 32 of a flat tube not fully illustrated, and a lower crest 30 b is with a Tube wall 33 of an adjacent flat tube soldered.
- interference elements 34 are arranged, which have approximately the shape of a conical tip and are embossed from the material of the rib 30.
- the air flow the direction of which is indicated by an arrow L, is thus disturbed in the lower region 30b of the rib 30 by the interference elements 34, which are arranged one behind the other and project with their tips into the air flow.
- There are formed behind each interfering element 34 vortex which improve the heat transfer in this area.
- the interference elements 34 thus act as a vortex generator.
- a partial section in the plane IV-IV shows the profile of the gills 31, the - in Direction of employment - have a Kiementiefe T.
- Fig. 5 shows the same view as in Fig. 4, but with another embodiment of interference elements 35, which are round or oval and also embossed from the fin material.
- Fig. 6 shows a similar representation as Figs. 4 and 5, but with another embodiment of interference elements 36 which are formed in a ramp shape and are shown as a detail X in Fig. 8 .
- the interference elements 36 are formed as a ramp 37, which are cut out of a rib 38 and bent into the air flow L.
- the ramp 37 is characterized by a height H and a length K.
- the rib 38 is soldered in this area with a tube wall 39.
- the ramp 37 has a tear-off edge 40, at which air turbulence form.
- FIG. 7 shows a further embodiment of interference elements 41, which are formed like lobes and shown as a detail Y in FIG. 9 .
- the interference element 41 is formed as a rectangular flap 42, which is cut out of a ribbed bottom 43 and bent into the air flow L.
- the tab 42 which has a height H and a length K, is in this embodiment with its surfaces parallel to the air flow L and thus acts with its leading edge 43 as a "boundary layer breaker".
- FIG. 10 shows an enlarged sectional view of the knob-shaped expression 21 in FIG. 2.
- the rib 15 is soldered to the tube wall 18 via solder meniscuses 45.
- the central region 15c has a knob-like expression 21, which protrudes with a height H in the air flow channel. The production of this expression 21 is possible without great effort when rolling the ribs by appropriate embossing nubs are provided on the rollers.
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
Description
- Fig. 1
- eine Wellrippe mit V-förmiger Anordnung (V-Typ),
- Fig. 2
- eine Wellrippe in U-förmiger Anordnung (U-Typ) mit ausgeprägtem Störelement,
- Fig. 3
- eine Wellrippe (U-Typ) mit ausgeschnittenem Störelement,
- Fig. 4
- einen Längsschnitt durch einen Rippenkanal mit spitzen Störelementen,
- Fig. 5
- einen Längsschnitt durch einen Rippenkanal mit noppenförmigen Störelementen,
- Fig. 6
- einen Längsschnitt durch einen Rippenkanal mit rampenförmigen Störelementen,
- Fig. 7
- einen Längsschnitt durch einen Rippenkanal mit lappenförmigen Störelementen,
- Fig. 8
- eine Einzelheit X aus Fig. 6,
- Fig. 9
- eine Einzelheit Y aus Fig. 7 und
- Fig. 10
- eine Teilschnittdarstellung der noppenartigen Ausprägung gemäß Fig. 2.
Claims (19)
- Wärmeübertrager mit Rohren und Rippen, wobei die Rohre von einem ersten Medium durchströmbar und die Rippen von einem zweiten Medium umströmbar sind, dadurch gekennzeichnet, dass im Bereich einer Rohrrippenkontaktstelle zumindest ein Störelement für die Strömung des zweiten Mediums vorgesehen ist.
- Wärmeübertrager nach Anspruch 1, dadurch gekennzeichnet, dass die Rohre und die Rippen miteinander verlötet sind.
- Wärmeübertrager nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Rohre als Flachrohre und die Rippen als Wellrippen ausgebildet sind, wobei die Flachrohre von Wellenkämmen der Wellrippen berührt werden.
- Wärmeübertrager nach Anspruch 3, dadurch gekennzeichnet, dass die Wellrippen mit Kiemen besetzte Rippenflächen aufweisen.
- Wärmeübertrager nach Anspruch 3 oder 4, dadurch gekennzeichnet, dass die Wellrippen gegeneinander geneigte Rippenflächen aufweisen.
- Wärmeübertrager nach Anspruch 3 oder 4, dadurch gekennzeichnet, dass die Wellrippen zueinander parallele Rippenflächen aufweisen.
- Wärmeübertrager nach Anspruch 6, dadurch gekennzeichnet, dass die Wellenkämme jeweils drei Abschnitte aufweisen, nämlich zwei äußere Abschnitte mit relativ großer Krümmung und einen mittleren Abschnitt mit kleinerer oder ohne Krümmung.
- Wärmeübertrager nach einem der Ansprüche 3 bis 7, dadurch gekennzeichnet, dass im Bereich eines Wellenkammes mehrere Störelemente für die Strömung des zweiten Mediums vorgesehen sind.
- Wärmeübertrager nach Anspruch 8, dadurch gekennzeichnet, dass mehrere Störelemente eines Wellenkammes in Hauptströmungsrichtung des zweiten Mediums fluchtend angeordnet sind.
- Wärmeübertrager nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass zumindest ein Störelement als noppenartige Ausprägung aus dem Rippenmaterial ausgebildet ist.
- Wärmeübertrager nach einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, dass zumindest ein Störelement als Lappen ausgebildet ist, wobei der Lappen insbesondere aus dem Rippenmaterial gestanzt ist.
- Wärmeübertrager nach Anspruch 11, dadurch gekennzeichnet, dass der Lappen gegenüber einer Hauptströmungsrichtung des zweiten Mediums angestellt ist.
- Wärmeübertrager nach Anspruch 11 oder 12, dadurch gekennzeichnet, dass der Lappen als Rampe ausgebildet ist.
- Wärmeübertrager nach Anspruch 11 oder 12, dadurch gekennzeichnet, dass der Lappen als Fahne ausgebildet ist.
- Wärmeübertrager nach einem der Ansprüche 4 bis 14, dadurch gekennzeichnet, dass zumindest ein Störelement eine Höhe H senkrecht zu einer Hauptströmungsrichtung des zweiten Mediums und die Kiemen einen Abstand a von der Rohrrippenkontaktstelle aufweisen, wobei folgende Beziehung gilt: 0,1 a ≤ H ≤ 1,0 a.
- Wärmeübertrager nach einem der Ansprüche 4 bis 15, dadurch gekennzeichnet, dass zumindest ein Störelement eine Länge K und die Kiemen eine Tiefe T aufweisen, wobei folgende Beziehung gilt: 0,5 T ≤ K ≤ 2,0 T.
- Wärmeübertrager nach einem der Ansprüche 1 bis 16, dadurch gekennzeichnet, dass zumindest ein Störelement eine Breite B und die zugehörige Rohrrippenkontaktstelle einen Abstand t zu einer benachbarten Rohrrippenkontaktstelle aufweist, wobei folgende Beziehung gilt: 0,1 t ≤ B ≤ 0,5 t.
- Wärmeübertrager nach einem der Ansprüche 3 bis 17, dadurch gekennzeichnet, dass ein Flachrohr zwischen zwei Wellenkämmen einer Wellrippe zumindest ein zweites Störelement für die Strömung des zweiten Mediums aufweist.
- Wärmeübertrager nach Anspruch 18, dadurch gekennzeichnet, dass zumindest ein zweites Störelement als Ausprägung aus einer Rohrwand ausgebildet ist.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2002142188 DE10242188A1 (de) | 2002-09-10 | 2002-09-10 | Flachrohr-Wärmeübertrager |
| DE10242188 | 2002-09-10 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1398592A1 true EP1398592A1 (de) | 2004-03-17 |
| EP1398592B1 EP1398592B1 (de) | 2015-07-22 |
Family
ID=31724654
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03020179.2A Expired - Lifetime EP1398592B1 (de) | 2002-09-10 | 2003-09-05 | Flachrohr-Wärmeübertrager |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP1398592B1 (de) |
| DE (1) | DE10242188A1 (de) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006000634A1 (de) * | 2006-01-03 | 2007-07-05 | Modine Manufacturing Co., Racine | Wellrippen für Wärmetauscher |
| DE102006031676B4 (de) | 2006-07-08 | 2025-11-13 | Mahle International Gmbh | Turbulenzblech, Verfahren zur Herstellung eines Turbulenzbleches und Verwendung eines Turbulenzbleches |
| DE102008007608A1 (de) | 2008-02-04 | 2009-08-06 | Behr Gmbh & Co. Kg | Wärmeübertrager mit Rohren |
| DE102008045845A1 (de) | 2008-09-05 | 2010-03-11 | Behr Gmbh & Co. Kg | Strömungsleitelement und Wärmetauscher |
| DE102016213197A1 (de) | 2016-07-19 | 2018-01-25 | Mahle International Gmbh | Wellrippe eines Wärmeübertragers und Wärmeübertrager |
| DE102019218266A1 (de) * | 2019-11-26 | 2021-05-27 | Mahle International Gmbh | Wellrippenstruktur |
| DE102020100105A1 (de) | 2020-01-06 | 2021-07-08 | Volkswagen Aktiengesellschaft | Wärmeübertrager |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3250325A (en) * | 1963-02-19 | 1966-05-10 | Ford Motor Co | Heat exchange device |
| US4311193A (en) * | 1980-07-14 | 1982-01-19 | Modine Manufacturing Company | Serpentine fin heat exchanger |
| JPH08271169A (ja) * | 1995-02-03 | 1996-10-18 | Nippondenso Co Ltd | 熱交換器 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2949963B2 (ja) * | 1991-10-18 | 1999-09-20 | 株式会社デンソー | コルゲートルーバフィン型熱交換器 |
| AU4359000A (en) * | 1999-04-19 | 2000-11-02 | Peerless Of America, Inc. | An improved fin array for heat transfer assemblies and method of making same |
| US6598669B2 (en) * | 1999-04-19 | 2003-07-29 | Peerless Of America | Fin array for heat transfer assemblies and method of making same |
-
2002
- 2002-09-10 DE DE2002142188 patent/DE10242188A1/de not_active Withdrawn
-
2003
- 2003-09-05 EP EP03020179.2A patent/EP1398592B1/de not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3250325A (en) * | 1963-02-19 | 1966-05-10 | Ford Motor Co | Heat exchange device |
| US4311193A (en) * | 1980-07-14 | 1982-01-19 | Modine Manufacturing Company | Serpentine fin heat exchanger |
| JPH08271169A (ja) * | 1995-02-03 | 1996-10-18 | Nippondenso Co Ltd | 熱交換器 |
Non-Patent Citations (1)
| Title |
|---|
| PATENT ABSTRACTS OF JAPAN vol. 1997, no. 02 28 February 1997 (1997-02-28) * |
Also Published As
| Publication number | Publication date |
|---|---|
| DE10242188A1 (de) | 2004-03-18 |
| EP1398592B1 (de) | 2015-07-22 |
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