EP2171111A1 - Aus einer al-mg-si-legierung hergestelltes extrudiertes produkt mit erhöhter korrosionsresistenz - Google Patents

Aus einer al-mg-si-legierung hergestelltes extrudiertes produkt mit erhöhter korrosionsresistenz

Info

Publication number
EP2171111A1
EP2171111A1 EP08835140A EP08835140A EP2171111A1 EP 2171111 A1 EP2171111 A1 EP 2171111A1 EP 08835140 A EP08835140 A EP 08835140A EP 08835140 A EP08835140 A EP 08835140A EP 2171111 A1 EP2171111 A1 EP 2171111A1
Authority
EP
European Patent Office
Prior art keywords
weight
product according
alloy
spun
mpa
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
Application number
EP08835140A
Other languages
English (en)
French (fr)
Other versions
EP2171111B1 (de
Inventor
Bruce Morere
Annabelle Bigot
Jérôme PIGNATEL
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.)
Constellium Issoire SAS
Original Assignee
Alcan Rhenalu SAS
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
Application filed by Alcan Rhenalu SAS filed Critical Alcan Rhenalu SAS
Publication of EP2171111A1 publication Critical patent/EP2171111A1/de
Application granted granted Critical
Publication of EP2171111B1 publication Critical patent/EP2171111B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • 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

Definitions

  • AI-Mg-Si aluminum alloy spun product with improved corrosion resistance AI-Mg-Si aluminum alloy spun product with improved corrosion resistance
  • the invention relates to spun aluminum alloy products Al-Mg-Si (series 6000 according to the nomenclature of Aluminumuminum Association) with improved corrosion resistance, in particular drawn tubes intended in particular for pipes or heat exchangers for car manufacturing.
  • HFCs HydroFluoroCarbures
  • CO2 even though it is a greenhouse gas, has a much lower impact than HFCs, which would reduce the harmfulness of emissions related to leaks.
  • a compressor compresses the CO2 at high pressure and it then goes into a gas cooler (traditionally called a condenser, but in which condensation does not occur when the refrigerant is CO2), then in an internal heat exchanger (which allows heat exchange with the low pressure zone).
  • the CO2 which is still gaseous, then passes into a regulator from which a liquid flows out which allows the cooling of the passenger compartment by passing through an evaporator.
  • the low pressure gas is then accumulated before circulating in the internal heat exchanger and back into the compressor for a new cycle.
  • the spun aluminum products can be used for the manufacture of heat exchangers (gas cooler, evaporator) and / or for the realization of the pipes allowing the refrigerant to circulate between the various elements of the cooling circuit.
  • the use of CO2 as a refrigerant is made difficult by the pressure at which it must be used.
  • the critical temperature of CO2 is lower than that of HFC-134a and its critical pressure is higher which forces the air conditioning system to operate at higher pressures and temperatures than those currently used, whether in the high pressure part or the low pressure part of the circuit.
  • the materials used in the air conditioning circuit must therefore be stronger than current materials while maintaining at least equivalent performance in terms of manufacturing, shaping, assembly and corrosion resistance.
  • the CO2 thus needs to be compressed at high pressures of the order of 100 to 200 bar. Therefore, to allow the use of CO2 as a refrigerant, the pipes must withstand an operating pressure of 200 bar for high temperatures of 130-170 0 C which is high compared to current conditions, the order of 5 bars at 60 ° C. Alloys have been proposed for the production of flat tubes for heat exchangers (gas cooler, evaporator) of air conditioning systems using CO2 as a refrigerant gas.
  • JP 2005-068557 discloses a composition alloy (wt%) Mn: 0.8 - 2, Cu: 0.22 - 0.6, Ti: 0.01 - 0.2, Fe: 0.01 - 0, 4, Zn ⁇ 0.2, Sn ⁇ 0.018, In ⁇ 0.02.
  • JP 2007-070699 discloses a composition alloy (% by weight)
  • Patent application WO 99/18250 also discloses an alloy of the 3XXX series of composition Cu ⁇ 0.03, Mn: 0.1 - 1.5, Ti 0.03 - 0.35, Mg ⁇ 1.0 , Ni ⁇ 0.01, Zn: 0.05 - 1.0, Zr ⁇ 0.3, Fe ⁇ 0.50, Si ⁇ 0.50 Cr ⁇ 0.20.
  • alloys AA6060, AA6061 and AA6063 are examples of alloys AA6060, AA6061 and AA6063.
  • AA6060 alloy has the composition:
  • AA6061 alloy has the composition: Mg: 0.8 - 1.2, Si: 0.40 - 0.8, Fe: ⁇ 0.7, Cu: 0.15-0.40, Mn ⁇ 0.15, Cr 0, 04-0.35, Zn ⁇ 0.25, Ti ⁇ 0.15, other ⁇ 0.05 each and ⁇ 0.15 total, remains aluminum.
  • AA6063 alloy has the composition:
  • Mg 0.40 - 0.8, Si: 0.30 - 0.6, Fe ⁇ 0.35, Cu ⁇ 0.25, Mn ⁇ 0.05 - 0.20, Cr ⁇ 0.20, Zn ⁇ 0.10, other ⁇ 0.05 each and ⁇ 0.15 total, remains aluminum is also known from the applicant for the production of drawn tubes.
  • the problem addressed by the present invention is to provide a 6XXX alloy spun product of improved corrosion resistance and mechanical properties to withstand high pressures, particularly for operating temperatures between 130 ° C and 170 ° C while having the same or better performance in terms of manufacturing, forming, assembly and corrosion resistance than current 3XXX, 5XXX and 6XXX series products .
  • the subject of the invention is a spun product, in particular a stretched tube, made of alloy of the 6XXX series of composition (% by weight): Mg: 0.4 - 0.7, Si: 0.4 - 0.7, Fe : 0.1 - 0.3, Zn: 0.16 - 0.3, Ti 0.12 - 0.3, Mn ⁇ 0.10, Cu ⁇ 0.05, Cr ⁇ 0.05, Ni ⁇ 0, 05 other ⁇ 0.05 each and ⁇ 0.15 total, remaining aluminum, in which the Si / Mg ratio is between 0.9 and 1.3.
  • the preferred contents are (% by weight): Mg: 0.5 - 0.6, Si: 0.5 - 0.6, Fe: 0.15 - 0.25, Zn: 0.16 - 0.25, , Ti 0.16 - 0.25, Mn ⁇ 0.05, Cr ⁇ 0.03, Cu ⁇ 0.03, Ni ⁇ 0.03 other ⁇ 0.05 each and ⁇ 0.15 total, remaining aluminum, in wherein the Si / Mg ratio is between 1.0 and 1.2.
  • Another object of the invention is the use of a spun product according to the invention in the manufacture of motor vehicles.
  • the static mechanical characteristics that is the breaking strength R m , the yield point R p o , 2 , and the elongation at break A, are determined by a tensile test according to the standards EN 10002-1 and EN 754-2.
  • the term "spun product” includes so-called “stretched” products, that is products that are made by spinning followed by stretching.
  • the alloy of the 6XXX series according to the invention comprises, with respect to alloys AA6060 and AA6063, an addition of zinc and titanium.
  • the zinc content must be between 0.16 and 0.3% by weight and preferably between 0.16 and 0.25% by weight.
  • the titanium content must be between 0.12 and 0.3% by weight, and preferably between 0.16 and 0.25% by weight.
  • the content of Cr, Cu and Ni must be maintained at an impurity level: less than 0.05% by weight and preferably less than 0.03% by weight.
  • the alloy according to the invention thus differs from the alloy AA6061 which contains 0.04 - 0.35% by weight of Cr and 0.15 - 0.40% by weight of Cu.
  • the combination of the addition of Zn and Ti makes it possible both to improve the mechanical properties and the resistance to corrosion.
  • the magnesium content is between 0.4 and 0.7% by weight and preferably between 0.5 and 0.6% by weight.
  • the silicon content is between 0.4 and 0.7% by weight and preferably between 0.5 and 0.6% by weight.
  • the addition of magnesium and silicon at a content of at least 0.4% by weight and preferably at least 0.5% by weight makes it possible to achieve the desired mechanical characteristics.
  • the magnesium content must however be limited to a maximum of 0.7% by weight and preferably 0.6% by weight to ensure satisfactory brazeability of the products, as well as a good performance in terms of extrusionability. .
  • the silicon content must also be limited to a maximum of 0.7% by weight and preferably 0.6% by weight.
  • the Si / Mg ratio is between 0.9 and 1.3 and preferably between 1.0 and 1.2.
  • the manganese content must be less than 0.10% by weight and preferably less than 0.05% by weight.
  • the iron content must be between 0.1 and 0.3% by weight and preferably between 0.15 and 0.25% by weight. Too high a content of iron contributes to the degradation of the corrosion resistance and a maximum content of 0.3% by weight is required, a maximum content of 0.25% by weight being preferred. For economic reasons of recycling, the iron content must be at least 0.1% by weight and preferably at least 0.15% by weight. The addition of other elements may have a detrimental effect on the alloy and they must therefore have a content of less than 0.05% by weight each and less than 0.15% by weight in total.
  • the process for producing the spun products according to the invention involves the casting of billets of the indicated alloy, the homogenization of the billets, their heating and their spinning in order to obtain a tube in straight length or in a crown, the solution and quenching and optionally one or more stretching passes to bring the product to the desired dimensions.
  • the tube may advantageously be annealed at a temperature between 400 ° C. and 550 ° C. to improve its ductility.
  • the spun products according to the invention are used in the T4 state, that is to say that the maturation is carried out at room temperature.
  • the products according to the invention can be obtained by quenching on a press.
  • the spun products according to the invention undergo a return which leads them to the T6 state, so as to maximize the mechanical strength.
  • the products according to the invention have a grain size of less than 45 ⁇ m and preferably less than 25 ⁇ m.
  • the products according to the invention have in the T4 state a high mechanical strength.
  • the breaking strength at ambient temperature is increased by more than 50% with respect to a 3XXX alloy product according to the application WO 02/055750 in the H12 state and by more than 10% with respect to a 6060 alloy product in the T4 state.
  • the advantage is confirmed for tests carried out at high temperature.
  • the tensile strength at 170 ° C. is increased by nearly 60% relative to a 3XXX alloy product according to the application WO 02/055750 in the H12 state and by almost 10% relative to to an alloy product 6060 in the T4 state.
  • the tubes according to the invention have, in the T4 state, a tensile strength R m greater than 170 MPa at room temperature and greater than 140 MPa at 170 ° C.
  • the tubes according to the preferred composition of The invention has in the T4 state a breaking strength Rm greater than 180 MPa at room temperature and greater than 150 MPa at 170 ° C.
  • the elongation at break A% obtained with the products according to the invention is high: greater than 25%, both at room temperature and at 170 ° C.
  • the product according to the invention thus has important advantages in terms of suitability. to shaping and resistance to the rupture especially with respect to 3XXX alloy products according to demand
  • the products according to the invention also have a high resistance to perforating corrosion, which makes it possible to obtain high durations of use without leakage.
  • the products according to the invention do not exhibit deep pits during a salt spray test of SWAAT type according to the ASTM G85A3 standard, whereas under the same conditions, they are observed for AA6106 alloy products. , AA6060 and even for AA6060 alloy products in which titanium has been added.
  • the combined addition of zinc and titanium enables the products according to the invention to achieve a corrosion resistance in the T4 state equivalent to that obtained with the 3XXX alloy products according to the application WO 02/055750. .
  • a preferred form of the spun product according to the invention is a cylindrical tube having only one cavity.
  • the spun products according to the invention can be used especially as tubes in the manufacture of motor vehicles.
  • the spun products according to the invention can be used as tubes for fuel lines, oil, brake fluid or refrigerant for automobiles and as tubes for heat exchangers for engine cooling and / or air conditioning systems.
  • passenger compartment especially if they use CO2 as a refrigerant gas.
  • the tubes, in particular the drawn tubes, according to the invention are more particularly adapted to be used in the form of cylindrical tubes having only one cavity for the fluid transfer lines used in passenger compartment air-conditioning systems of motor vehicles using CO2 as a refrigerant gas.
  • the alloys A, B, C and D correspond to compositions of the prior art, alloy A is part of the 5xxx series, alloy B according to the application WO02 / 055750 is part of the 3XXX series, the alloys C and D are part of the 6XXX series.
  • the alloy E is an alloy 6060 in which titanium has been added and the alloy F is in accordance with the invention.
  • compositions (% by weight) are indicated in Table 1.
  • the alloy billet A was spun into finished lengths of straight tubes, which were then drawn and annealed to a diameter of 16 mm and a thickness of 1.25 mm in the final state O.
  • the alloy billets B, C, D, E and F were spun into tube crowns.
  • the 6XXX alloy products (C, D, E and F) were hardened on press.
  • the tensile strength R m (in MPa), the yield strength R p o , 2 (in MPa) and the elongation at break A% were measured on samples of the 6 tubes. , at room temperature and at 140 0 C and 170 0 C so as to simulate the conditions of use of the tube in an air conditioning system using CO2 as a refrigerant. The results are shown in Table 2.
  • the spun products obtained with the four alloys C, D, E, F of the 6xxx series have mechanical characteristics that are quite similar to each other and comparable to those obtained with alloy A of the 5XXX series.
  • the alloy F according to the invention has among the 6XXX alloys tested the best properties, in particular with a higher tensile strength of more than 10% for a test carried out at ambient temperature and of nearly 10% for a test carried out at 170 ° C. C, compared to that obtained with AA6060 alloy.
  • the alloy F according to the invention has, in particular, improved mechanical characteristics with respect to the alloy B according to WO02 / 055750 of the prior art: a rupture strength R m increased by more than 50% both at room temperature at 140 ° C.
  • the average grain size was measured by the intercepts method on samples of tubes B, D, E and F. The results are shown in Table 4.
  • the tubes obtained with the alloy according to the invention have fine grains. equiaxes of the order of 25 microns.
  • Corrosion resistance was measured using the Sea Water Acetic Acid Test (SWAAT) according to ASTM G85 A3. The measurements were made for periods of 500 cycles at the temperature of 49 ° C., on three tubes of length 200 mm each of alloys A, B, C, D, E and F. At the end of the test, the tubes were removed from the chamber and stripped in a solution of nitric acid concentrated to 68% in order to dissolve the corrosion products. On each tube, the depth of the pits by defocusing is measured optically on the surface and the average of the depths of the 5 deepest stings. The average Pmoy of the values obtained for the 3 tubes is then calculated. Corrosion resistance is better when Pmoy is weak. The results of 5 successive SWAAT test campaigns are shown in Table 3. The number of signs * indicates the number of tubes drilled in the batch of three tubes tested.
  • the alloy F according to the invention has a corrosion resistance which is much higher than that of the other alloys C, D, E of the same series 6xxx, and that of the alloy A of the series 5xxx.
  • the alloy F does not exhibit deep pitting, it being understood that in the context of the present invention the term deep stitch means a Pmoy value greater than 0.5 mm.
  • Titanium Test E alloy pits deeper than the F alloy, demonstrating the beneficial effect on the corrosion resistance of the combined addition of Ti and Zn, compared with the addition of titanium. alone.
  • the alloy F according to the invention offers a corrosion resistance equivalent to that of the alloy B, according to the application WO02 / 055750 of the prior art, known for its advantageous properties of corrosion resistance.
  • the alloy F according to the invention offers an advantageous combination of high mechanical properties at operating temperatures of automotive air conditioning systems using CO2 fluid, and high resistance to the necessary perforating corrosion so as to obtain high durations of use. without leakage.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
EP08835140.8A 2007-07-27 2008-07-21 Aus einer al-mg-si-legierung hergestelltes extrudiertes produkt mit erhöhter korrosionsresistenz Active EP2171111B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705511A FR2919307B1 (fr) 2007-07-27 2007-07-27 Produit file en alliage d'aluminium ai-mg-si a resistance a la corrosion amelioree
PCT/FR2008/001073 WO2009043992A1 (fr) 2007-07-27 2008-07-21 Produit file en alliage d'aluminium al-mg-si a resistance a la corrosion amelioree

Publications (2)

Publication Number Publication Date
EP2171111A1 true EP2171111A1 (de) 2010-04-07
EP2171111B1 EP2171111B1 (de) 2017-03-22

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP08835140.8A Active EP2171111B1 (de) 2007-07-27 2008-07-21 Aus einer al-mg-si-legierung hergestelltes extrudiertes produkt mit erhöhter korrosionsresistenz

Country Status (9)

Country Link
US (1) US20100200205A1 (de)
EP (1) EP2171111B1 (de)
JP (1) JP2010534765A (de)
KR (1) KR20100051081A (de)
CN (1) CN101765669A (de)
BR (1) BRPI0814132A2 (de)
FR (1) FR2919307B1 (de)
MX (1) MX2010000786A (de)
WO (1) WO2009043992A1 (de)

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Publication number Priority date Publication date Assignee Title
US8690207B2 (en) * 2008-12-04 2014-04-08 Norsk Hydro Asa Impact absorbing member and a method for making same
CN102146543A (zh) * 2010-02-05 2011-08-10 古河Sky株式会社 挤压性质和牺牲阳极性质优异的连接件用铝合金挤压材料
FR2996857B1 (fr) * 2012-10-17 2015-02-27 Constellium France Elements de chambres a vide en alliage d'aluminium
CN103540814A (zh) * 2013-10-17 2014-01-29 常熟市良益金属材料有限公司 一种铝镁合金
KR102437942B1 (ko) 2014-01-21 2022-08-29 아르코닉 테크놀로지스 엘엘씨 6xxx 알루미늄 합금
CN103993206B (zh) * 2014-04-16 2016-05-25 池州市光明塑钢有限公司 一种印刷用铝合金型材及其制备方法
CN103911533A (zh) * 2014-04-26 2014-07-09 广东兴发铝业有限公司 冷藏集装箱用6061铝合金挤压型材配方
CN104152758A (zh) * 2014-08-12 2014-11-19 山东裕航特种合金装备有限公司 一种汽车减震器用高强铝合金空心型材生产工艺
CN104313415A (zh) * 2014-11-12 2015-01-28 江苏礼德铝业有限公司 一种铝合金
ES2828958T3 (es) 2015-12-23 2021-05-28 Norsk Hydro As Método para la producción de una aleación de aluminio tratable térmicamente con propiedades mecánicas mejoradas
CN111575559B (zh) * 2020-07-07 2021-06-29 福建祥鑫股份有限公司 一种耐腐蚀6系铝合金

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US4829944A (en) * 1986-06-25 1989-05-16 Showa Aluminum Corporation Intake manifold and process for producing same
US5976278A (en) * 1997-10-03 1999-11-02 Reynolds Metals Company Corrosion resistant, drawable and bendable aluminum alloy, process of making aluminum alloy article and article
FR2819525B1 (fr) * 2001-01-12 2003-02-28 Pechiney Rhenalu PRODUITS LAMINES OU FILES EN ALLIAGE D'ALUMINIUM Al-Mn A RESISTANCE A LA CORROSION AMELIOREE
EP1594999A4 (de) * 2002-12-27 2006-05-24 Showa Denko Kk Aluminiumrohr und herstellungsverfahren dafür
JP2005068557A (ja) * 2003-08-07 2005-03-17 Showa Denko Kk 高温強度に優れたアルミニウム合金、熱交換器用部材、熱交換チューブおよび熱交換器
JP4612510B2 (ja) * 2005-09-08 2011-01-12 カルソニックカンセイ株式会社 熱交換器用アルミニウム合金押出チューブおよび熱交換器ならびにチューブの製造方法
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Also Published As

Publication number Publication date
FR2919307A1 (fr) 2009-01-30
BRPI0814132A2 (pt) 2015-02-03
US20100200205A1 (en) 2010-08-12
MX2010000786A (es) 2010-03-30
JP2010534765A (ja) 2010-11-11
FR2919307B1 (fr) 2009-10-02
WO2009043992A1 (fr) 2009-04-09
CN101765669A (zh) 2010-06-30
KR20100051081A (ko) 2010-05-14
EP2171111B1 (de) 2017-03-22

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