EP0462056A1 - Tôle superplastique en alliage d'aluminium - Google Patents

Tôle superplastique en alliage d'aluminium Download PDF

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Publication number
EP0462056A1
EP0462056A1 EP91810411A EP91810411A EP0462056A1 EP 0462056 A1 EP0462056 A1 EP 0462056A1 EP 91810411 A EP91810411 A EP 91810411A EP 91810411 A EP91810411 A EP 91810411A EP 0462056 A1 EP0462056 A1 EP 0462056A1
Authority
EP
European Patent Office
Prior art keywords
aluminum alloy
hours
cold
strip
manganese
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.)
Withdrawn
Application number
EP91810411A
Other languages
German (de)
English (en)
Inventor
Philippe Fernandez
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.)
3A Composites International AG
Original Assignee
Alusuisse Lonza Services Ltd
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 Alusuisse Lonza Services Ltd filed Critical Alusuisse Lonza Services Ltd
Publication of EP0462056A1 publication Critical patent/EP0462056A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S420/00Alloys or metallic compositions
    • Y10S420/902Superplastic

Definitions

  • the invention relates to a method for producing a fine-grained recrystallized sheet suitable for superplastic forming from a cold-hardenable, hardenable aluminum alloy.
  • the plastic elongation of a superplastic aluminum alloy is usually in the range of 400-800%, i.e. far above the values of conventional alloys. This allows a wide range of design options in terms of function and design with economical one-piece production.
  • the diverse shapes are reproducible with high dimensional accuracy, there is no "spring-back".
  • the simple tools that can be used have a particularly advantageous effect, since they also allow small and medium-sized production series to be produced cost-effectively and can be produced in short delivery times. Shape changes can be made quickly at affordable costs.
  • the present invention has for its object to provide a method of the type mentioned, which allows a cost-effective production of an air-cooled, hardenable, non-corrosion-prone aluminum sheet with superplastic properties.
  • the object is achieved according to the invention in that an alloy with 3-5.5% magnesium, 2-8% zinc, 0-4% copper, 0-1% manganese, 0-0.5% iron, 0-0.4 % Chromium, 0-0.4% molybdenum, 0-0.4% zircon, 0-0.3% silicon and 0-0.05% titanium, rest of aluminum of commercial purity, homogenized after continuous casting, hot rolled, with high Cold rolling degree cold rolled to the final thickness and annealed and cooled in a final heat treatment with rapid heating for recrystallization.
  • An alloy with 4-5% magnesium and 2-6%, preferably 3-4% zinc is particularly suitable as the cold-hardenable, hardenable AlMgZn alloy. Here and for the rest, percentages by weight are always used.
  • the preferred proportions are 0-0.1% copper, 0.2-0.4% manganese, 0.15-0.25% chromium, 0-0.2% iron, 0-0.2 % Molybdenum, 0-0.1% zircon and 0-0.1% silicon, although the chromium content can also be 0-0.1% and the zirconium content can also be 0.15-0.25%.
  • the cast aluminum alloy blocks are freed from the cast skin and cut to length. These formats can be heated to a metal temperature of 420-450 ° C in a first homogenization stage for 2-12 hours, kept at this temperature for 4-12 hours and in a second homogenization stage to 480-530 ° C for 0.5-4 hours heated and kept at this temperature for 2-12 hours.
  • the formats can be heated to a metal temperature of 420-480 ° C. in a continuous homogenization for 4-12 hours and kept at this temperature for 10-30 hours.
  • the hot rolling is expediently carried out immediately after the homogenization annealing or after cooling and reheating to 350-500 ° C.
  • the homogenized formats are rolled onto a 4-30 mm thick band, especially around 6-10 mm.
  • the metal temperature is preferably between 325 and 345 ° C.
  • the hot-rolled strip is preferably intermediate annealed at 300-400 ° C. for 6-36 hours before cold rolling.
  • the hot-rolled strip which can be hardened due to the alloy composition, is additionally strengthened by cold working, in which it is preferably rolled with a degree of cold deformation of 60-95%, in particular 70-90%.
  • the final thickness is e.g. between 1.5 and 3 mm, especially around 2 mm.
  • the homogenization annealing serves to reduce the structural non-uniformities, such as segregations and precipitations, which arise when casting rolled ingots.
  • the cold deformation increases the mechanical strength, the 0.2% proof stress, tensile strength and hardness increase.
  • the recrystallization of the cold-rolled strip serves for extensive softening and is accompanied by a complete recrystallization of the aluminum alloy.
  • rapid heating is essential, which is preferably carried out in a salt bath at 490-510 ° C or in a continuous temperature furnace.
  • the recrystallization annealing should take place with a heating time of at most 8 minutes, in particular at most 3 minutes.
  • the softened belts are cooled in air or in water.
  • the softened aluminum strips have superplastic properties. In addition to the great elasticity with relatively high mechanical strength, they are particularly characterized by their extraordinarily low susceptibility to corrosion, also in relation to stress corrosion.
  • An aluminum alloy with 4.4% magnesium, 3.7% zinc, 0.5% copper, 0.7% manganese, 0.12% iron, 0.19% zircon and 0.07% silicon is produced in a vertical continuous casting process with electromagnetic molds cast into bars of 70x200x800 mm, using the usual Tib2 grain refining technique.
  • the casting temperature is around 720 ° C.
  • the cast skin is removed, the bar head and bar base are separated and the bar divided. These are heated to 440 ° C. for 3 hours in a first homogenization stage, kept at this temperature for 8 hours, heated to 500 ° C. for 1 hour in a second homogenization stage and kept at this temperature for 3 hours.
  • the ingots are rolled in several passes at 9 mm, the final temperature of the metal being between 325 and 345 ° C.
  • the recrystallization annealing is carried out with a heating time of 5 minutes in a liquid mixture of potassium and sodium nitrate at 500 ° C. After cooling in water, the tapes are cleaned and dried.
  • Example 1 In a method corresponding to Example 1 for producing a fine-grain recrystallized sheet suitable for superplastic deformation, an aluminum alloy is used with 4.3% magnesium, 3.6% zinc, 0.3% manganese, 0.11% iron, 0.20% zircon and 0.07% silicon.
  • the sheets of both examples show superplastic properties, they are checked for their expansion at 500 ° C, 520 ° C and 540 ° C.
  • Metallographic examinations show finely divided, globulitic grains of less than 10 ⁇ m, which are regularly distributed.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Metal Rolling (AREA)
  • Conductive Materials (AREA)
EP91810411A 1990-06-11 1991-05-30 Tôle superplastique en alliage d'aluminium Withdrawn EP0462056A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH1959/90 1990-06-11
CH1959/90A CH682326A5 (fr) 1990-06-11 1990-06-11

Publications (1)

Publication Number Publication Date
EP0462056A1 true EP0462056A1 (fr) 1991-12-18

Family

ID=4222606

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91810411A Withdrawn EP0462056A1 (fr) 1990-06-11 1991-05-30 Tôle superplastique en alliage d'aluminium

Country Status (3)

Country Link
US (1) US5122196A (fr)
EP (1) EP0462056A1 (fr)
CH (1) CH682326A5 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0799900A1 (fr) * 1996-04-04 1997-10-08 Hoogovens Aluminium Walzprodukte GmbH Alliage d'aluminium-magnesium à haute résistance mécanique pour structures soudées de grandes dimensions
CN104313413A (zh) * 2014-10-24 2015-01-28 北京科技大学 一种Al-Mg-Zn系合金及其合金板材的制备方法
CN112760578A (zh) * 2020-12-24 2021-05-07 上海交通大学 一种具有超塑性铝基复合材料板的制备方法

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07145441A (ja) * 1993-01-27 1995-06-06 Toyota Motor Corp 超塑性アルミニウム合金およびその製造方法
US5469912A (en) * 1993-02-22 1995-11-28 Golden Aluminum Company Process for producing aluminum alloy sheet product
US5480498A (en) * 1994-05-20 1996-01-02 Reynolds Metals Company Method of making aluminum sheet product and product therefrom
US5850755A (en) * 1995-02-08 1998-12-22 Segal; Vladimir M. Method and apparatus for intensive plastic deformation of flat billets
US5772804A (en) * 1995-08-31 1998-06-30 Kaiser Aluminum & Chemical Corporation Method of producing aluminum alloys having superplastic properties
US6423164B1 (en) 1995-11-17 2002-07-23 Reynolds Metals Company Method of making high strength aluminum sheet product and product therefrom
DE19944589A1 (de) * 1999-09-16 2001-03-22 Ejot Verbindungstech Gmbh & Co Schraubverbindung
US6783729B2 (en) * 2001-12-11 2004-08-31 Alcan International Limited Aluminum alloy for making naturally aged die cast products
CN1985021A (zh) * 2003-12-22 2007-06-20 卡伯特公司 高完整性溅射靶材以及其批量制造方法
US20060027308A1 (en) * 2004-08-05 2006-02-09 Mackenzie M S Method and apparatus for curing patches on composite structures having complex substrates
EP1683882B2 (fr) 2005-01-19 2010-07-21 Otto Fuchs KG Alliage d'Aluminium avec sensitivité à la trempe réduite et procédé de fabrication d'un produit demi-final lors de cet alliage
KR101466996B1 (ko) 2006-03-07 2014-12-01 캐보트 코포레이션 변형된 금속 물품을 제조하는 방법
US9039848B2 (en) * 2007-11-15 2015-05-26 Aleris Aluminum Koblenz Gmbh Al—Mg—Zn wrought alloy product and method of its manufacture
US8454078B2 (en) * 2009-11-17 2013-06-04 GM Global Technology Operations LLC Automotive vehicle door construction
US9315885B2 (en) 2013-03-09 2016-04-19 Alcoa Inc. Heat treatable aluminum alloys having magnesium and zinc and methods for producing the same
CN106834839A (zh) * 2016-11-28 2017-06-13 佛山市尚好门窗有限责任公司 一种增强荧光的金属
CN113774296B (zh) * 2021-09-08 2022-08-05 中国航发北京航空材料研究院 一种提高铝合金厚板及锻件综合性能的制备工艺

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984260A (en) * 1971-07-20 1976-10-05 British Aluminum Company, Limited Aluminium base alloys
US4021271A (en) * 1975-07-07 1977-05-03 Kaiser Aluminum & Chemical Corporation Ultrafine grain Al-Mg alloy product
EP0084571A1 (fr) * 1981-07-30 1983-08-03 Kasei Naoetsu Light Metal Industries Limited Procede de production d'une plaque en alliage d'aluminium superplastique
EP0297035A1 (fr) * 1987-06-23 1988-12-28 Alusuisse-Lonza Services Ag Alliage d'aluminium pour déformation superplastique
US4867805A (en) * 1988-02-03 1989-09-19 Agrawal Suphal P Superplastic aluminum alloys, alloy processes and component part formations thereof

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5911651B2 (ja) * 1980-10-29 1984-03-16 三井アルミニウム工業株式会社 超塑性アルミニウム合金及びその製造方法
JPS6025160A (ja) * 1983-07-22 1985-02-07 Seiko Electronic Components Ltd 非水電解液電池
JPS6086248A (ja) * 1983-10-17 1985-05-15 Kobe Steel Ltd 超塑性アルミニウム合金の製造方法
JPS60251260A (ja) * 1984-05-26 1985-12-11 Kobe Steel Ltd 超塑性アルミニウム合金の製造方法

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3984260A (en) * 1971-07-20 1976-10-05 British Aluminum Company, Limited Aluminium base alloys
US4021271A (en) * 1975-07-07 1977-05-03 Kaiser Aluminum & Chemical Corporation Ultrafine grain Al-Mg alloy product
EP0084571A1 (fr) * 1981-07-30 1983-08-03 Kasei Naoetsu Light Metal Industries Limited Procede de production d'une plaque en alliage d'aluminium superplastique
EP0297035A1 (fr) * 1987-06-23 1988-12-28 Alusuisse-Lonza Services Ag Alliage d'aluminium pour déformation superplastique
US4867805A (en) * 1988-02-03 1989-09-19 Agrawal Suphal P Superplastic aluminum alloys, alloy processes and component part formations thereof

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN, Band 10, Nr. 128 (C-345)[2185], 13. Mai 1986; & JP-A-60 251 260 (KOBE SEIKOSHO K.K.) 11-12-1985 *
PATENT ABSTRACTS OF JAPAN, Band 6, Nr. 158 (C-120)[1036], 19. August 1982; & JP-A-57 76 145 (MITSUI ARUMINIUMU KOGYO K.K.) 13-05-1982 *
PATENT ABSTRACTS OF JAPAN, Band 9, Nr. 228 (C-303)[1951], 13. September 1985; & JP-A-60 86 248 (KOBE SEIKOSHO K.K.) 15-05-1985 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0799900A1 (fr) * 1996-04-04 1997-10-08 Hoogovens Aluminium Walzprodukte GmbH Alliage d'aluminium-magnesium à haute résistance mécanique pour structures soudées de grandes dimensions
CN104313413A (zh) * 2014-10-24 2015-01-28 北京科技大学 一种Al-Mg-Zn系合金及其合金板材的制备方法
CN112760578A (zh) * 2020-12-24 2021-05-07 上海交通大学 一种具有超塑性铝基复合材料板的制备方法

Also Published As

Publication number Publication date
US5122196A (en) 1992-06-16
CH682326A5 (fr) 1993-08-31

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