CA2462074A1 - Aluminium alloy for making fin stock material - Google Patents

Aluminium alloy for making fin stock material Download PDF

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Publication number
CA2462074A1
CA2462074A1 CA002462074A CA2462074A CA2462074A1 CA 2462074 A1 CA2462074 A1 CA 2462074A1 CA 002462074 A CA002462074 A CA 002462074A CA 2462074 A CA2462074 A CA 2462074A CA 2462074 A1 CA2462074 A1 CA 2462074A1
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CA
Canada
Prior art keywords
aluminium alloy
stock material
fin stock
alloy according
range
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.)
Abandoned
Application number
CA002462074A
Other languages
French (fr)
Inventor
Scott W. Haller
Job Anthonius Van Der Hoeven
Adrianus Jacobus Wittebrood
Achim Buerger
Klaus Vieregge
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.)
Aleris Aluminum Canada LP
Novelis Koblenz GmbH
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Individual
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
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Publication of CA2462074A1 publication Critical patent/CA2462074A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081Heat exchange elements made from metals or metal alloys
    • F28F21/084Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/003Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/10Alloys based on aluminium with zinc as the next major constituent

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Conductive Materials (AREA)
  • Laminated Bodies (AREA)

Abstract

An aluminium alloy for making fin stock material, having the composition in weight percent: Si <= 1.2 Mn <= 0.05 Mg <= 0.05 Fe <= 2.0 0.5 &l t;= Ni <= 1.5 0.05 <=: Cu <=: 1.0 0.5 <= Zn <= 4.0 and/or 0.1 <= Sn <= 2 .0 and/or 0.01 <=: In <= 0.5 V <= 0.40 and/or Ti <0.01 and/or Cr <0.01 and/or Zr &l t;0.01 other elements up to 0.05 each, up to 0.15 in total Al balance.

Description

ALUMINIUM ALLOY FOR MAKING FIN STOCK MATERIAL
FIELD OF THE INVENTION
The invention relates to an aluminium alloy for making fin stock material. Fin stock material is used in heat exchanger devices. The fin stock material is used for making for instance corrugated fins, by which the heat from the heat exchanger must be removed. Furthermore, the invention relates to fin stock material made from the aluminium alloy according to the invention, and to a brazed heat exchanger having to fins made of this alloy. Moreover, the invention relates to a method of producing the fin stock alloy and the brazed heat exchanger.
DESCRIPTION OF THE RELATED ART
In the prior art, aluminium alloys are used for fins in heat exchanger applications because of their desirable combination of strength, weight, thermal conductivity, brazeability, corrosion resistance and formability.
Heat exchangers from aluminium can be fabricated by stacking aluminium alloy sheets, which have been formed to a desired configuration, to form fluid passageways or tubes, and by securing aluminium alloy fins between the fluid 2o passageways by brazing. The aluminium alloy sheets used to make the fluid passageways and/or the aluminium alloy used for the fins are provided with a low melting clad layer. The bonding between the alloy clad sheets and the fins is achieved by melting the cladding or filler material of the sheets and/or fin material.
As a brazing method, typically vacuum brazing or controlled atmosphere brazing is used. To improve the corrosion resistance of the fluid passageways, fin materials are used which are electrochemically anodic (less noble) relative to the fluid passageways material, so that this fin material has a sacrificial anode effect.
An example of an aluminium alloy for making fin material is given in International patent application no. WO OI/36697. This alloy has the following 3o composition, in weight percent:
Si 0.7 - I.2 Mn 0.7 - 1.2 Mg up to 0.35 Fe up to 0.8 Zn up to 3.0 Ni up to 1.5 Cu up to 0.5 Ti up to 0.20 In up to 0.20 Zr up to 0.25 V up to 0.25 Cr up to 0.25 others up to 0.05 each, and up to 0.15 in total.
Al balance.
This disclosed alloy is said to have an improved post-braze 0.2%-yield strength (also referred to as 0.2%-offset proof stress or 0.2% PS) over conventional alloys for the same application.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide an aluminium alloy for making fin stock material which can be used for heat exchangers, and which has an improved thermal conductivity.
2o It is another object of the invention to provide such an aluminium alloy, which has a strength which is at least as good as the strength of conventional aluminium alloys for making fin stock material.
It is still another object of the invention to provide such an aluminium alloy, which has a corrosion potential which is at least as negative as the corrosion potential of conventional aluminium alloys for making fin stock material.
In one aspect of the invention one or more of these objects are reached with an aluminium alloy for malting fin stock material, having the composition in weight percent:
Si <_ 1.2 Mn <_ 0.05 Mg <_ 0.05 Fe _< 2.0 0.5 _< Ni <_ 1.5 0.05 <_ Cu 51.0 0.5 <_ Zn <_ 4.0 and/or 0.1 <_ Sn _< 2.0 and/or 0.01 <_ In <_ 0.5 V <_ 0.40 and/or Ti <0.01 and/or Cr <0.01 andlor Zr <0.01 other elements up to 0.05 each, up to 0.15 in total Al balance.
This aluminium alloy has a very good thermal conductivity, thereby improving the heat exchange properties of the fins made from this aluminium alloy .
Moreover, this aluminium alloy has satisfactory mechanical properties in the post-brazed l0 condition, such as tensile strength and corrosion potential.
Although this aluminium alloy is primarily intended as fin stock material for heat exchangers, it may be used for other parts of heat exchange units, such as tube plate, or other uses.
The heat exchanger market, particularly in the automotive industry, requires a balance of properties for fin stock alloys, which includes strength, conductivity, formability, brazeability and corrosion potential. If one of these properties should be improved where the other properties must remain as good as they are, often many of the alloying elements in the composition must be changed in relation to each other.
In the present case, it is the merit of the invention that has been seen that the conductivity of the alloy could be improved by decreasing the solid solution in the alloy through carefully selecting the content of certain alloying elements.
This has resulted in the following limitations of the alloying elements in the aluminium alloy according to the present invention. All percentages are by weight.
Si is an important alloying element in the alloy according to the invention;
it is expected that Si improves the strength of the alloy by solid solution hardening and precipitation hardening. Because the solid solution in the alloy should be as low as possible for the required conductivity, the amount of Si should not be higher than 1.2 %. When the amount of Si is higher, too much Si will remain in solid solution, resulting in a lower conductivity. A more preferred range for Si is 0.4 to 0.8 %.
3o Within this range the required combination of strength and conductivity is reached best.
Mn is an important alloying element in conventional alloys for making fin stock material. Mn is normally added for strength. In the alloy according to this invention, the Mn content is kept very low so as to reduce the amount of solid solution in the alloy. Preferably Mn <_ 0.03 %, and more preferably Mn 5 0.01 %, thereby improving the conductivity as much as possible. Mn may also be absent.
Mg increases the strength of the alloy significantly, but has a detrimental effect on controlled atmosphere brazeability because it tends to interact with the flux material. For this reason the Mg content has a maximum of 0.05 %, and preferably Mg <_ 0.03 %, and more preferably Mg S 0.01 %, to keep the Mg content as low as possible. Mg may also be absent.
Fe is an alloying element that is present in all known aluminium alloys. Fe is added for post-braze strength. It is supposed to form precipitates with Al, Ni and Si.
The solid solubility of Fe in A1 is extremely low; therefore, Fe can be used to improve the strength without compromising the conductivity. Preferably Fe is in the range of 0.3 % to 1.6 %, and more preferably in the range of 0.7 % to 1.3 %, so as to reach a preferred strength without compromising the formability.
Ni is also present to improve the post-braze strength of the alloy. Like Fe, the solid solubility of Ni in A1 is extremely low; therefore, Ni can be used to improve the strength without compromising the conductivity. However, when the Ni content is >
2 %, the formability becomes too low. Ni is preferably present in the range of of 0.~
to 1.2 % because in this range the best combination of strength and formability is found.
Cu is present in the alloy according to the invention to improve the post-braze strength of the alloy. The amount of Cu is preferably restricted to the range of 0.1 %
to 0. ~ %, and more preferably to the range of 0.1 % to 0.6 %, so as to reach the required strength. However, Cu is believed to increase the corrosion potential of the alloy, whereas the corrosion potential should be low to allow the fin material to act as a sacrificial anode. For this reason, at least one of the elements Zn, Sn or In should be present.
Zn, Sn or In, or a combination of these three elements, are present to counteract the effect of Cu on the corrosion potential of the alloy. The amount of these elements must therefore be higher than zero, taking into account the stronger effect of Sn and especially In as compared to Zn. The amounts of Zn, Sn and In should not be higher than necessary and therefore preferably Zn is in the range of 1.0 % to 3.0 %
and/or Sn is in the range of 0.1 % to 1.0 % and/or In is in the range of 0.01 % to 0.05 %.
Preferably, only Zn is present, but Zn can be (partly) replaced by Sn and/or In.
Ti, V, Cr and Zr are to be avoided as much as possible, because they have a negative effect on the conductivity of the alloy. Preferably, these elements are below 0.01 % each.
It is expected that all elements present in the aluminium are detrimental to the conductivity of the alloy. Both impurities and intentionally added elements should therefore be as low as possible, the intentionally added elements being added in so far as they are needed to reach the desired properties.
In a second aspect of the invention there is provided fin stock material made from the aluminium alloy as specified above, wherein the fin stock material has a post-braze conductivity of at least 26 MSIm (45 % IACS), and preferably at least 29 MSIm (50 % IACS). A conductivity of more than 45 % IACS is good and a conductivity of more than 50 % IACS is very good in comparison to conventional fin stock material for heat exchangers.
Preferably, the fin stock material has a corrosion potential between -750 mV
and -950 mV versus SCE (ASTM G69), more preferably between -750 mV and -850 mV
2o according to SCE (ASTM G69). The indication SCE means that the voltage in mV
has been measured in relation to a saturated calomel electrode. These values for the corrosion potential give a good sacrificial anode effect when this fin stock material is used in heat exchangers.
According to a preferred embodiment the fin stock material has a post braze UTS (Ultimate Tensile Strength) between 135 and 155 MPa, andlor a 0.2% PS > 50 MPa. This strength is sufficiently high for normal use of fin stock material.
According to a third aspect of the invention, there is provided a brazed heat exchanger having fins made of an aluminium alloy according the first aspect of the invention, or having fins made of fin stock material according to the second aspect of the invention.
EXAMPLES
The aluminium alloy and fin stock material in accordance with the invention will now be illustrated by non-limitative and comparative examples.
On a laboratory scale nine alloys have been cast with solidification rates in a range comparable to solidification rates in industrial scale DC-casting. These alloys are manufactured on a laboratory scale, but the aluminium alloy in accordance with this invention can be manufactured on an industrial scale using various standard industrial scale DC-casting and continuous aluminium casting methods, followed by i0 hot andlor cold rolling.
The chemical compositions of the nine alloy examples are given in table l, some relevant properties after brazing simulation are given in table 2.
Table 1. Chemical composition, in wt%, of the aluminium alloys tested, the balance is aluminium and impurities.
alloySi Mn Mg Fe Ni Cu Zn Ti Zr V

1 0.70 <0.010.01 1.05 0.94 0.15 1.52 <0.01<0.01 <0.01 2 0.70 <0.01<0.01 0.87 0.99 0.30 1.99 <0.01<0.01 <0.01 3 0.48 <0.01<0.01 0.92 1.05 0.50 2.50 <0.01<0.01 <0.01 4 0.49 0.16 0.01 0.90 1.02 0.31 1.99 <0.01<0.01 <0.01 5 0.78 0.26 <0.01 0.76 0.66 0.51 0.51 0.03 <0.01 <0.01 6 0.78 0.96 <0.01 0.76 0.73 0.25 1.01 0.03 0.106 <0.01 7 0.76 0.97 0.11 0.29 0.71 0.25 0.20 0.13 <0.01 <0.01 8 0.79 0.99 <0.01 0.31 0.71 0.25 1.49 0.03 <0.01 0.15 9 1.07 ~ 0.21 ~ ~ ~ ~ ~ ~ <0.01~
0.92 0.31 0.49 0.25 0.20 0.02 <0.01 _7_ Table2. Properties after simulated brazing cycle.
alloy conductivitycorrosion potentialUTS 0.2% PS
[%IACS] [mV SCE] [MPa] [MPa]

1 49.3 -783 137 53 2 51.4 -779 143 59 3 46.0 -786 149 57 4 43.2 -778 134 54 42.8 -732 142 56 6 42.3 -770 156 70 7 40.5 -748 166 76 8 36.6 -805 154 67 9 43.3 -747 161 69 The nine different chemistries as specified in table 1 were cast and sawn to pieces with a thickness of 80 xnm, and thereafter preheated to a temperature below 5 540°C, the alloys were not homogenised. Subsequently hot rolled at a temperature below 540°C and cold rolled to a thickness of 0.15 mm. After inter annealing, the pieces were cold rolled to a thickness of 0.1 mm.
In the alloys 1 to 4 of table l, no Ti, V, Cr or Zr is present. The Zn present in the alloys can be (partly) replaced by Sn and/or In, as is known in the art.
1o As can be seen, the alloys 4 to 9 are comparative examples that do not fit in the alloy ranges according to the invention. The amount of Mn is too high. In alloys 6.7 and 8 additions of Zr, Ti and V, respectively, are also present. Despite the fact that the Mn level of alloys 4 and 5 is increased as compared to alloys 1, 2 and 3, the strength is not significantly increased. This is attributed to the decrease in Ni. Alloys 6, 7 and 8 show that with the Ni level of alloys 4 and 5 high strength can be reached when Zr, Ti or V additions are present. However, due to the additions of Mn, Zr, Ti or V in the alloys 4 to 9, the conductivity of these alloys is comparatively low.
The three alloys 1, 2 and 3 having a composition according to the invention clearly have a high conductivity, a sufficiently high strength and a corrosion potential 2o within the required range to get the sacrificial anode effect.

Claims (18)

1. An aluminium alloy for making fin stock material, having the composition in weight percent:
Si <= 1.2 Mn <= 0.05 Mg <= 0.05 Fe <= 2.0 0.5 <= Ni <= 1.5 0.05 <= Cu <= 1.0 1.0 <= Zn <= 3.0 and/or 0.1 <= Sn <= 1.0 and/or 0.01 <= In <= 0.05 V <= 0.40 and/or Ti < 0.01 and/or Cr < 0.01 and/or Zr < 0.01 other elements up to 0.05 each, up to 0.15 in total Al balance.
2. An aluminium alloy according to claim 1, wherein Si is in the range of 0.4 % to 0.8 %.
3. An aluminium alloy according to claim 1 or 2, wherein Mn <= 0.03 %.
4. An aluminium alloy according to claim 3, wherein Mn <= 0.01 %.
5. An aluminium alloy according to any of the claims 1 to 4, wherein Mg <= 0.03 %.
6. An aluminium alloy according to claim 5, wherein Mg <= 0.01 %.
7. An aluminium alloy according to any of the preceding claims, wherein Fe is in the range of 0.3 % to 1.6 %, and preferably in the range of 0.7 % to 1.3 %.
8. An aluminium alloy according to any of the preceding claims, wherein Ni is in the range of 0.8 % to 1.2 %.
9. An aluminium alloy according to any of the preceding claims, wherein Cu is in the range of 0.1 % to 0.8 %, and preferably in the range of 0.1 % to 0.6 %.
10. An aluminium alloy according to any of the preceding claims, wherein no In and no Sn is present.
11. An aluminium alloy according to any of the preceding claims, wherein V <
0.01 %.
12. Fin stock material made from the aluminium alloy according to any of the preceding claims, wherein the fin stock material has a post-braze conductivity of at least 26 MS/m (46 %
IACS), and preferably at least 29 MS/m (50 % IACS).
13. Fin stock material according to claim 12, wherein the fin stock material has a corrosion potential between -750 mV and -950 mV versus SCE (ASTM G69), preferably between -750 mV
and -850 mV versus SCE (ASTM G69).
14. Fin stock material according to claim 12 or 13, wherein the fin stock material has a post braze Ultimate Tensile Strength between 135 and 155 MPa.
15. Fin stock material according to claim 12, 13 or 14, wherein the fin stock material has a 0.2%-offset proof stress > 50 MPa.
16. Fin stock material according to one of claims 12 - 15, wherein the fin stock material has been clad on at least one side with a clad layer having a lower melting point than the fin stock material.
17. A brazed heat exchanger having fins made of an aluminium alloy according to any one of claims 1 -11.
18. A brazed heat exchanger having fins made of fin stock material according to any one of claims 12 -
CA002462074A 2001-10-05 2002-10-02 Aluminium alloy for making fin stock material Abandoned CA2462074A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP01203759A EP1300480A1 (en) 2001-10-05 2001-10-05 Aluminium alloy for making fin stock material
EP01203759.4 2001-10-05
PCT/EP2002/011191 WO2003031667A1 (en) 2001-10-05 2002-10-02 Aluminium alloy for making fin stock material

Publications (1)

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CA2462074A1 true CA2462074A1 (en) 2003-04-17

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CA002462074A Abandoned CA2462074A1 (en) 2001-10-05 2002-10-02 Aluminium alloy for making fin stock material

Country Status (8)

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US (1) US20050019204A1 (en)
EP (2) EP1300480A1 (en)
JP (1) JP2005504890A (en)
KR (1) KR20040045477A (en)
CN (1) CN1578844A (en)
CA (1) CA2462074A1 (en)
MX (1) MXPA04003133A (en)
WO (1) WO2003031667A1 (en)

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JP2008006480A (en) * 2006-06-30 2008-01-17 Sumitomo Light Metal Ind Ltd Brazing fin material for heat exchanger, heat exchanger, and method for manufacturing the same
KR100840385B1 (en) * 2006-07-20 2008-06-23 성훈엔지니어링(주) Heat resisting aluminum alloy
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JP5789401B2 (en) * 2011-04-15 2015-10-07 株式会社神戸製鋼所 Aluminum fin material for heat exchanger
CN102296217A (en) * 2011-08-24 2011-12-28 吴江市精工铝字制造厂 High-strength heat-resistant aluminum alloy
MX359572B (en) 2011-12-16 2018-10-01 Novelis Inc Aluminium fin alloy and method of making the same.
CN102534325B (en) * 2011-12-31 2013-10-16 江苏常铝铝业股份有限公司 Horizontal-flow porous pipe for heat exchanger and manufacturing method of the horizontal-flow porous pipe
JP6472378B2 (en) * 2012-05-23 2019-02-20 グランジェス・スウェーデン・アーべー Ultra-flexible and melt-resistant fin material with very high strength
KR101468957B1 (en) * 2012-05-30 2014-12-05 한국기계연구원 Aluminum alloy for casting
CN102703783A (en) * 2012-05-30 2012-10-03 江门市长利光电科技有限公司 High-heat conduction aluminum alloy for casting
JP5954099B2 (en) 2012-10-12 2016-07-20 日本軽金属株式会社 Aluminum alloy sheet for battery cases with excellent formability, heat dissipation and weldability
CN102994813A (en) * 2012-11-19 2013-03-27 宁波福士汽车部件有限公司 Aluminum alloy material for air conditioner pipe
CN103572123A (en) * 2013-10-21 2014-02-12 姚富云 Manufacturing method of heat exchanger aluminum alloy radiating fin suitable for hard brazing
CN103572078A (en) * 2013-10-21 2014-02-12 姚富云 Refining method of aluminum alloy for heat exchangers
CN103572101A (en) * 2013-10-21 2014-02-12 姚富云 Heat exchanger aluminum alloy radiating fin material suitable for hard brazing
JP6206322B2 (en) * 2014-05-14 2017-10-04 日本軽金属株式会社 Aluminum alloy fin material for heat exchanger excellent in brazing and sag resistance and method for producing the same
CN106574326B (en) 2014-08-06 2019-05-21 诺维尔里斯公司 Aluminium alloy for heat-exchanger fin
CN104233007A (en) * 2014-08-27 2014-12-24 邹平齐星工业铝材有限公司 High-thermal-conductivity heat transfer fin and manufacturing method thereof
CN104532084A (en) * 2014-11-25 2015-04-22 安徽天祥空调科技有限公司 High strength anti-cracking air conditioning radiator aluminum alloy sheet and preparation method thereof
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CN105296813A (en) * 2015-11-03 2016-02-03 任静儿 Aluminum alloy for liquid crystal display device wire harness
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Also Published As

Publication number Publication date
EP1300480A1 (en) 2003-04-09
CN1578844A (en) 2005-02-09
EP1436438A1 (en) 2004-07-14
US20050019204A1 (en) 2005-01-27
JP2005504890A (en) 2005-02-17
WO2003031667A1 (en) 2003-04-17
MXPA04003133A (en) 2004-07-08
KR20040045477A (en) 2004-06-01

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