EP1059362B1 - Aluminium-Strangpresslegierung - Google Patents

Aluminium-Strangpresslegierung Download PDF

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Publication number
EP1059362B1
EP1059362B1 EP20000202018 EP00202018A EP1059362B1 EP 1059362 B1 EP1059362 B1 EP 1059362B1 EP 20000202018 EP20000202018 EP 20000202018 EP 00202018 A EP00202018 A EP 00202018A EP 1059362 B1 EP1059362 B1 EP 1059362B1
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EP
European Patent Office
Prior art keywords
alloy
max
range
aluminium
extrusion
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.)
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EP20000202018
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English (en)
French (fr)
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EP1059362A1 (de
Inventor
Timothy John Hurd
Klaus Vieregge
Louis Walter Marie Paul Tack
Arne Mulkers
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.)
Alvance Aluminium Duffel BV
Novelis Koblenz GmbH
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Aleris Aluminum Duffell BVBA
Aleris Aluminum Koblenz GmbH
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Application filed by Aleris Aluminum Duffell BVBA, Aleris Aluminum Koblenz GmbH filed Critical Aleris Aluminum Duffell BVBA
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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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2255/00—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
    • F28F2255/16—Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes extruded

Definitions

  • the invention relates to an aluminium extrusion alloy and extruded sections thereof, containing Mn, Mg, Cu and Si, which aluminium extrusion alloy is particular suitable for application in brazed assemblies, and further to a method of its manufacture.
  • aluminium alloys are the alloys of choice for heat exchanger applications. These alloys are selected for their desirable combination of strength, low weight, good thermal and electrical conductivity, brazeability, corrosion resistance and formability.
  • Typical applications include automotive heater cores, radiators, evaporators, condensers, charge air coolers, and transmission/engine oil coolers.
  • brazed heat-exchanger devices such as for example automotive radiators
  • mechanical fasteners made of extruded Aluminium Association (AA)6063-series alloy, preferably in a T8-temper.
  • AA extruded Aluminium Association
  • a T8-temper involves solution heat treatment of the extruded product, cold working and then artificially ageing. This application requires excellent mechanical properties and a good machinability of the extruded product for putting in a mechanical thread. Additionally at least a reasonable corrosion resistance is required.
  • the chemical composition of standard AA6063 alloy is, in weight percent:-
  • EP-A-0676480 Northwest Aluminum discloses two very wide groups of high strength Al-Mg-Si extrusion alloys.
  • the first group of aluminium alloys consists of, in weight percent:-
  • WO-A-99/07906 discloses an aluminium alloy for welded structures and brazing application, having the following composition in weight percent:-
  • An object of the present invention as defined in the claims is to provide an aluminium extrusion alloy capable of obtaining post-brazing mechanical properties and corrosion resistance at least comparable to standard AA6063, and being capable of being processed in at least a Controlled Atmosphere Brazing (CAB) process.
  • CAB Controlled Atmosphere Brazing
  • a further object of the present invention is to provide an aluminium extrusion alloy having machinability characteristics at least equal to standard AA6063 extruded products, typically in a T8-temper.
  • Another object of the present invention is to provide a method of manufacturing extruded sections of the new aluminium alloy.
  • Another object of the present inventions is to provide a method of manufacturing an assembly of brazing components, wherein one of the components is made from the aluminium extrusion alloy of the invention.
  • an aluminium extrusion alloy having the following composition in weight percent:-
  • the aluminium extrusion alloy of the invention has similar post-braze mechanical strength as compared to AA6063 in the same temper and better than AA3003 material, a corrosion resistance as tested in a SWAAT test environment equivalent to AA6063 material in the same temper, and further the machinability characteristics of the present extrusion alloy are equal to or better than AA6063 material in the same temper and better than AA3003 material.
  • the aluminium extrusion alloy of the invention can be used to manufacture devices via a brazing process, and in particular in a Controlled Atmosphere Brazing process.
  • the aluminium alloy composition range is known from EP-A-0718072 , in which document it is mentioned that the alloy is used as a rolled product only as core alloy for brazing sheet having on at least one side thereof a brazing layer of an aluminium alloy containing silicon as main alloying element.
  • Mn is an important alloying element in the alloy according to the invention. And should be in the range of 1.0 to 1.4%. Below 1.0% there is not a sufficient effect, and above 1.4% it may result in the formation of detrimental large intermetallic particles. In this range the Mn present allows for a solid solution hardening effect because sufficient Mn is retained in solid solution for the desired increase in strength.
  • Cu is one of the main alloying elements in order to obtain the desired strength level, in particular by means of solution hardening. At least 0.2% is required for obtaining the desired strength and corrosion resistance, while a Cu content of over 2.0% does not produce any significant improvements in respect of strength, and may further result in the formation of detrimental low-melting eutectics. A more preferred lower limit for the Cu level is 0.5%. A more preferred Cu content is in a range of 0.65 to 1.5% in order to achieve an optimisation in the desired properties. A very suitable range for the Cu-content is 0.65 to 0.9% as a compromise in mechanical strength after extrusion, mechanical strength in the post-braze condition, post-braze corrosion resistance and extrudability.
  • Mg is another main alloying elements in combination with the Cu and Si present in order to obtain the desired properties.
  • the Mg can be present in the range of 0.1 to 0.6%.
  • a more suitable Mg-content is in the range of 0.1 to 0.35%.
  • a suitable Mg-content is in the range of 0.3 to 0.6%.
  • the proviso (Cu+Mg)>1.0 is met. Thereby a good corrosion resistance of a product manufactured via a brazing process is obtained.
  • Si is another important alloying element in the aluminium alloy according to this invention.
  • the main reason is to enable the formation of Mg 2 Si precipitation required to improve the strength by means of ageing before and after brazing. Further, the addition of Si results in an increased solution hardening of the alloy after brazing. Below 0.15% there is no effect of the Si, and above 1.0% it may result in the formation of detrimental low-melting eutectics and also in the formation of large intermetallic particles.
  • a more suitable minimum level of Si is 0.20%, more preferably of 0.30%, and most preferably of 0.40%.
  • a more suitable maximum level of Si is 0.70%, and more preferably 0.60% as a compromise in extrudability, tensile strength and corrosion resistance.
  • Fe is a known impurity element in this type of aluminium alloys. Its presence should be limited to a maximum of 0.8%, and preferably to a maximum of 0.4%, in order to optimise the mechanical properties and extrudability.
  • Zn is considered to be an impurity element also and can be tolerated up to 0.25%, but is preferably less than 0.15%, and more preferably less than 0.10%.
  • Ti is important as a grain refiner during solidification of cast extrusion billets or ingots.
  • the preferred range of Ti is not more than 0.15%, but preferably is less than 0.10%, and more preferably is less than 0.05%.
  • Cr improves the corrosion resistance of the alloy.
  • Cr limits the solubility of Mn and further reduces the extrudability of the aluminium alloy.
  • the Cr content must not be more than 0.35%, preferably not more than 0.2%, and more preferably less than 0.05%.
  • the optionally added Zr and/or V improves amongst other things the strength of the aluminium extrusion alloy.
  • a more preferred maximum for these elements alone or in combination is 0.25%.
  • a more suitable level of these elements alone or in combination is in the range of 0.05 to 0.25%.
  • each of Cr, Zr and V are at impurity level, meaning below 0.05%, in order to control the costs of the aluminium alloy and to increase its recycleability.
  • each impurity element is present at 0.05% maximum, and the total of impurities is 0.15% maximum.
  • the invention is further embodied in an extruded section having a composition of the aluminium alloy of this invention as set out above.
  • the extruded section can be provided at least in any one of a number of tempers selected from the following types T3, T4, T6, T8 and T9, or modifications thereof.
  • the invention also provides in a method of manufacturing an extruded section comprising the aluminium extrusion alloy set out above, which method comprises the following sequential steps:-
  • a method which allows for the production of extruded sections capable of obtaining similar post-braze mechanical strength as compared to AA6063 in the same temper and better than AA3003 material, a corrosion resistance as tested in a SWAAT test environment equivalent to AA6063 material in the same temper, and further to obtain machinability characteristics equal to or better than AA6063 material in the same temper and better than AA3003 material.
  • the aluminium extrusion alloy obtained by the method according to the invention can be used to manufacture devices via various brazing processes, and in particular in a Controlled Atmosphere Brazing process.
  • both continuous and semi-continuous casting processes can be used. Different configurations of castings can also be used to produce the desired extrusion shape.
  • the aluminium alloy may be homogenised.
  • the aim of the homogenising treatment is amongst other things, to homogenise the microstructure, to dissolve the relevant elements or components such as Mg 2 Si, to level off possible residual stresses resulting from the casting process, and to spheroidize sharp or needle shaped intermetallic compounds formed during solidification of the aluminium alloy.
  • a homogenisation treatment in the temperature range of 560 to 610 °C for a soaking time in the range of 5 to 24 hours results in the optimised properties.
  • a longer homogenisation time is not disadvantageous, but is not required and only serves to raise the costs of production.
  • the homogenisation treatment may be omitted. Omitting the homogenisation treatment still allows for very good extrusion characteristics, and resulting in a final extruded product having an improved post-braze mechanical properties while the corrosion resistance is somewhat reduced.
  • the cast billets are preheated at temperatures between 500 and 540°C.
  • the ingot or extrusion billet is processed into products via a hot extrusion process, wherein either direct or indirect extrusion techniques may be used.
  • the ingot temperature during extrusion is preferably in the range of 500 to 540°C.
  • the aluminium alloy in accordance with the invention can be processed in both solid and hollow extruded sections. In this temperature range it has been found that the alloy in accordance with the invention has a high extrudability, and very similar to AA6063 alloys.
  • aluminium extrusion alloy in accordance with the invention can be extruded in any configuration including channels, bars, seat rails, I-beams, angles, tubing, heat exchanger tubing, architectural shapes, rectangular hollows, rods, or other complex extruded shapes.
  • the alloy of the invention should be rapid cooled to below 150°C by means of water or water spray in order to prevent or minimise uncontrolled precipitation. This is also designated by the term "press-quenching". Following cooling to below 150°C, the extruded section is further cooled to about room temperature.
  • the extruded product is aged to the desired level of mechanical and physical properties.
  • the ageing may be natural ageing (at ambient temperature) and/or artificial ageing at an elevated temperature, preferably in the range of 100 to 250°C. A natural ageing period of 3 months is typical for this.
  • Artificial ageing can result in an 0.2% yield strength of 270 MPa or more.
  • the artificial ageing is executed for a time period in the range of 1 to 100 hours.
  • the artificial ageing is executed at about 160°C for a time period in the range of 3 to 100 hours, preferably for a time period in the range of 3 to 15 hours, or at an equivalent combination of time and temperature giving a similar ageing effect.
  • the extruded product is cold worked after extrusion.
  • the cold working may be performed prior to or after the ageing treatment, but there is a preference for cold working prior to the ageing treatment.
  • the product may be cold worked, for example, by drawing or stretching up in the range of 4 to 20% of its original length.
  • the cold reduction is in the range of 5 to 18% of its original length to optimise properties.
  • the extruded section can be provided in at least any one of the following tempers selected from the group of T3 (solution heat treated, cold worked, and naturally aged to a substantially stable condition), T4 (solution heat treated and naturally aged to a substantially stable condition), T6 (solution heat treated and then artificially aged), T8 (solution heat treated, cold worked, and then artificially aged), T9 (solution heat treated, artificially aged, and then cold worked), and modifications thereof.
  • T3 solution heat treated, cold worked, and naturally aged to a substantially stable condition
  • T4 solution heat treated and naturally aged to a substantially stable condition
  • T6 solution heat treated and then artificially aged
  • T8 solution heat treated, cold worked, and then artificially aged
  • T9 solution heat treated, artificially aged, and then cold worked
  • the extruded section is capable of obtaining an 0.2% yield strength of at least 270 MPa or more, and preferably of 280 MPa or more. Further, by artificial ageing treatment the extruded section is capable of obtaining an ultimate tensile strength of 290 MPa or more, preferably of 310 MPa or more, and in the best examples of 325 MPa or more.
  • the extruded and aged section may be worked into a more suitable shape, for example by means of machining.
  • the worked product may be added to an assembled device, for example an automotive radiator, which device is subsequently joined in a brazing process.
  • the brazed assembly together with the worked product is cooled to below 100°C and preferably to room temperature by a set cooling rate.
  • the brazed assembly is allowed to age to final desired mechanical properties.
  • the extrusion alloy of the invention is capable of obtaining a post-braze 0.2% yield strength of at least 100 MPa or more, preferably of 120 MPa or more, and in the best examples of 140 MPa or more, and a post-braze ultimate tensile strength of at least 200 MPa or more, and preferably of 220 MPa or more, by means of natural ageing at ambient temperatures. If desired the extrusion alloy in accordance with the invention is capable of reaching even higher mechanical properties when artificially aged.
  • An advantage of the application of the extrusion alloy in accordance with the present invention is that it provides high mechanical properties both before and after a brazing cycle.
  • the mechanical properties are at least similar to AA6063 material in the same temper, while the inventive alloy further allows for a favourable processing in a CAB brazing process.
  • the cooling rate after the brazing cycle plays a role in obtaining the desired strength level of the brazed assembly.
  • the cooling rate should not be below 30°C/min. More preferably the cooling rate after brazing is at least 50°C/min, and more preferably at least 60°C/min, and most preferably at least 70°C/min. Increasing the cooling rate after the brazing cycle can give rise to a further increase in the obtainable strength levels.
  • extruded sections having a composition in accordance with the invention as set out above and which have been homogenised during their manufacture from a cast ingot into extruded sections respond to the influence of the cooling rate after brazing.
  • extruded sections having a composition in accordance with the invention as set out above and which have not been homogenised during their manufacture from a cast ingot into extruded sections respond to a much lesser extend on the cooling rate after brazing and the subsequent ageing.
  • a controlled atmosphere (CAB) is being used whereby a suitable brazing flux material is used.
  • a brazed assembly comprising at least one member being an extruded section comprising the aluminium alloy of the invention, and having a post-braze 0.2% yield strength of at least 100 MPa or more, preferably of at least 120 MPa or more, and more preferably of at least 140 MPa or more.
  • extruded rods have been tested for their mechanical properties, 0.2% yield strength (0.2% YS), ultimate tensile strength (UTS) and elongation at fracture (A 50 ), see Table 2, and for their machinability characteristics.
  • Table 3 shows typical properties of AA6063-T8 and AA3003-H111 extruded material.
  • the machinability characteristics of the alloy of the invention is similar to or better than AA6063 material in the same T8-temper; both give about 1 cm long, spiral or curly chips.
  • the machinability is much better than AA3003 material, which gives unbroken chips being arranged around the cutting tools. Further it is believed that from a machinability point of view a T9-temper provides better results than T8-temper material, resulting in shorter chips and the cut surface is more shiny and more smooth.
  • the alloy of the invention is capable of obtaining similar or better mechanical properties than AA6063 material, both alloys being in a T8-temper. Further it can be seen that non-homogenised material has mechanical properties in the same range as homogenised material.
  • the alloy of the invention is capable of obtaining mechanical properties significantly better than AA3003-H111 material, which material would be the normal alternative for AA6063 when further processed in a CAB brazing process.
  • Table 1 Alloy composition in weight %.
  • the alloys as manufactured in Example 1 will usually be provided to customers in the aged condition for further application.
  • the material is preferably in a T8- or T9-temper.
  • the alloy of the invention When used in manufacturing a brazed assembly, the alloy of the invention will be subjected to a heat-treatment in accordance to the braze cycle, which affects its mechanical properties.
  • the alloy of the invention has significant higher post-braze mechanical properties than AA3003-material. Further it can be seen that that for homogenised material the mechanical properties tend to increase with increasing cooling rate after brazing. However, non-homogenised material (Alloy 3 material) shows almost no influence of the cooling rate after brazing on the post-braze mechanical properties. Further, the non-homogenised material has significantly higher strength and lower elongation directly after brazing and shows almost no influence of natural ageing time. The results with respect to the non-homogenised material were unexpected and can not readily be explained.
  • the alloy of the invention is capable of obtaining mechanical properties at least similar to AA6063 material.
  • the AA6063 material After 15 days in a SWAAT test, the AA6063 material showed a shiny bright surface with only slight pitting with a PA qualification. Alloy 2 material showed also a shiny bright surface with somewhat deeper pits with a PA qualification. The alloy 4 material showed uniform attack and was given a PB qualification. The alloy 3 materials showed a uniform attack, and was given a PB/C qualification. From these results it can be concluded that the alloy in accordance with the invention is capable of obtaining an equivalent corrosion resistance as AA6063 material. Table 4. Post-braze mechanical properties as function of alloy composition, days of natural ageing after brazing and cooling rate after the braze cycle. 5 days natural ageing 30 days natural ageing Material PS [MPa] UTS. [MPa] Elong.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
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  • Extrusion Of Metal (AREA)

Claims (16)

  1. Verfahren zur Herstellung eines stranggepressten bzw. extrudierten Teils einer Aluminiumextrusions- bzw. -strangpresslegierung, wobei das Verfahren die aufeinanderfolgenden Schritte umfasst:
    (a) Gießen der Legierung zu Barren, die eine Zusammensetzung, in Gew.-%, aufweisen von:
    Mn    1.0 - 1.4
    Cu    0.2 - 2.0
    Mg    0.1 - 0.6
    Si    0.15 - 1.0
    Fe     max. 0,8
    Zn    max. 0,25
    Ti     max. 0,15
    Cr     max. 0,35
    Zr und/oder V insgesamt    max. 0.25
    andere jeweils bis 0,05, insgesamt 0,15 Rest Aluminium,
    und mit der Maßgabe, dass (Cu+Mg) > 0,7 und bevorzugt
    (Cu+Mg) > 1,0 ist,
    (b) Vorwärmen des Gussbarrens,
    (c) Warmextrudieren des vorgewärmten Gussbarrens in ein extrudiertes Produkt,
    (d) rasches (Ab)Kühlen des extrudierten Produkts auf unter 150°C mithilfe von Wasser oder Wassersprühen,
    (e) Altern des extrudierten und gekühlten Produkts, um eine 0,2-Prozent-Dehnfestigkeit von wenigstens 270 MPa zu erzielen.
  2. Verfahren nach Anspruch 1, wobei das Verfahren ferner vor Schritt (b) den Schritt des Homogenisierens des Gussbarrens in einem Temperaturbereich von 560 bis 610°C für eine Durchwärmzeit im Bereich von 5 bis 24 Stunden umfasst.
  3. Verfahren nach Anspruch 1 oder 2, wobei das Warmextrudieren während Schritt (c) mit einem Extrusionsknüppel in einem Temperaturbereich von 500 bis 540°C durchgeführt wird.
  4. Verfahren nach einem der Ansprüche 1 bis 3, wobei die Legierung einen Cu-Gehalt im Bereich von 0,65 bis 2,0% und bevorzugt 0,65 bis 0,90% aufweist.
  5. Verfahren nach einem der Ansprüche 1 bis 4, wobei die Legierung einen Si-Gehalt im Bereich von 0,30 bis 1,0% und bevorzugt 0,4 bis 1,0% aufweist.
  6. Verfahren nach einem der Ansprüche 1 bis 5, wobei die Legierung einen Mg-Gehalt im Bereich von 0,1 bis 0,35% aufweist.
  7. Verfahren nach einem der Ansprüche 1 bis 6, wobei die Legierung einen Mg-Gehalt im Bereich von 0,3 bis 0,6% aufweist.
  8. Verfahren nach einem der Ansprüche 1 bis 7, wobei der extrudierte, aus der Aluminiumextrusionslegierung hergestellte Teil in einem T8 oder T9 Zustand bereitgestellt wird.
  9. Verfahren zur Herstellung einer Anordnung aus hartgelöteten Bauteilen, umfassend die Schritte:
    (a) Bilden der Bauteile, von denen wenigstens eines aus einer Aluminiumextrusionslegierung hergestellt ist, die eine Zusammensetzung, in Gew.-%, aufweist von: Mn 1,0 bis 1,4, Cu 0,2 bis 2,0, Mg 0,1 bis 0,6, Si 0,15 bis 1,0, Fe max. 0,8, Zn max. 0,25, Ti max. 0,15, Cr max. 0,35, Zr und/oder V insgesamt max. 0,25, andere jeweils bis zu 0,05, insgesamt 0,15, Rest Aluminium, und mit der Maßgabe, dass (Cu+Mg) > 0,7 und bevorzugt (Cu+Mg) > 1,0 ist, erzielt durch das Verfahren gemäß einem der Ansprüche 1 bis 8,
    (b) Zusammensetzen der Bauteile zu einer Anordnung,
    (c) Hartlöten der Anordnung bei erhöhter Temperatur für einen Zeitraum, der zum Schmelzen und Verteilen des Hartlots ausreicht,
    (d) (Ab)Kühlen der hartgelöteten Anordnung auf unter 100°C,
    (e) Altern der hartgelöteten und gekühlten Anordnung, um eine 0,2-Prozent-Dehnfestigkeit von wenigstens 100 MPa und bevorzugt wenigstens 120 MPa zu erzielen.
  10. Verfahren nach Anspruch 9, wobei der Hartlötschritt (c) ferner die Verwendung eines Hartlötflussmittels und einer Schutzatmosphäre bzw. kontrollierter Atmosphäre (CAB) umfasst.
  11. Verfahren nach Anspruch 9 oder 10, wobei während Schritt (d) die hartgelötete Anordnung unter 100°C mit einer Kühlgeschwindigkeit von wenigstens 50°C/min (ab)gekühlt wird.
  12. Verfahren nach einem der Ansprüche 9 bis 11, wobei die Aluminiumextrusionslegierung einen Cu-Gehalt im Bereich von 0,65 bis 2,0% und bevorzugt 0,65 bis 0,90% aufweist.
  13. Verfahren nach einem der Ansprüche 9 bis 12, wobei die Aluminiumextrusionslegierung einen Si-Gehalt im Bereich von 0,30 bis 1,0% und bevorzugt 0,4 bis 1,0% aufweist.
  14. Verfahren nach einem der Ansprüche 9 bis 13, wobei die Aluminiumextrusionslegierung einen Mg-Gehalt im Bereich von 0,1 bis 0,35% aufweist.
  15. Verfahren nach einem der Ansprüche 9 bis 14, wobei die Aluminiumextrusionslegierung einen Mg-Gehalt im Bereich von 0,3 bis 0,6% aufweist.
  16. Hartgelötete Anordnung, umfassend wenigstens ein Element mit einem extrudierten Teil, der die folgende Zusammensetzung, in Gew.-%, hat: Mn 1,0 bis 1,4, Cu 0,2 bis 2,0, Mg 0,1 bis 0,6, Si 0,15 bis 1,0, Fe max. 0,8, Zn max. 0,25, Ti max. 0,15, Cr max. 0,35, Zr und/oder V insgesamt max. 0,25, andere jeweils bis 0,05, insgesamt 0,15, Rest Aluminium, und mit der Maßgabe, dass (Cu+Mg) > 0,7 und bevorzugt (Cu+Mg) > 1,0 ist, und wobei dieses Element eine 0,2-Prozent-Dehnfestigkeit nach dem Hartlöten von wenigstens 100 MPa und bevorzugt von wenigstens 120 MPa aufweist.
EP20000202018 1999-06-11 2000-06-07 Aluminium-Strangpresslegierung Expired - Lifetime EP1059362B1 (de)

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EP99201855 1999-06-11
EP20000202018 EP1059362B1 (de) 1999-06-11 2000-06-07 Aluminium-Strangpresslegierung

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Publication number Priority date Publication date Assignee Title
FR2797454B1 (fr) * 1999-08-12 2001-08-31 Pechiney Rhenalu Bande ou tube en alliage d'aluminium pour la fabrication d'echangeurs de chaleur brases
CA2558108C (en) * 2004-03-31 2014-07-08 Hydro Aluminium Deutschland Gmbh Heat-resistant aluminium alloy for heat exchangers
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