EP0357743A1 - Hochfeste magnesiumlegierungen und verfahren, um derartige legierungen mittels rascher erstarrung zu erhalten. - Google Patents

Hochfeste magnesiumlegierungen und verfahren, um derartige legierungen mittels rascher erstarrung zu erhalten.

Info

Publication number
EP0357743A1
EP0357743A1 EP89903172A EP89903172A EP0357743A1 EP 0357743 A1 EP0357743 A1 EP 0357743A1 EP 89903172 A EP89903172 A EP 89903172A EP 89903172 A EP89903172 A EP 89903172A EP 0357743 A1 EP0357743 A1 EP 0357743A1
Authority
EP
European Patent Office
Prior art keywords
mum
alloy
less
spinning
magnesium
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
EP89903172A
Other languages
English (en)
French (fr)
Other versions
EP0357743B1 (de
Inventor
Gilles Regazzoni
Gilles Nussbaum
Haavard T Gjestland
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.)
Ferroglobe France SAS
Norsk Hydro ASA
Original Assignee
Pechiney Electrometallurgie SAS
Norsk Hydro ASA
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
Priority claimed from FR8802885A external-priority patent/FR2627780B1/fr
Application filed by Pechiney Electrometallurgie SAS, Norsk Hydro ASA filed Critical Pechiney Electrometallurgie SAS
Publication of EP0357743A1 publication Critical patent/EP0357743A1/de
Application granted granted Critical
Publication of EP0357743B1 publication Critical patent/EP0357743B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C23/00—Alloys based on magnesium
    • C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C23/00—Alloys based on magnesium
    • C22C23/04—Alloys based on magnesium with zinc or cadmium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/005—Amorphous alloys with Mg as the major constituent
    • 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
    • C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

Definitions

  • the present invention relates to magnesium-based alloys with high mechanical strength, as well as a process for obtaining these alloys by rapid solidification and consolidation by spinning. It relates in particular to alloys containing Al, at least Zn and / or Ca and which can contain manganese whose weight composition is situated within the following limits:
  • Ni ⁇ 0.01 the rest being magnesium.
  • alloys with high mechanical strength having a composition corresponding to that of the basic commercial alloys of the prior art, listed under the names AZ31, AZ61, AZ80 (wrought alloys) and AZ91, AZ92 (casting alloys), according to ASTM standard, or G-A3Z1, G-A6Z1, G-A8Z, G-A9Z1 and G-A9Z2 respectively according to French standard NF A 02-004; it also relates to alloys having a composition corresponding to those of said basic commercial alloys to which calcium is added. It should be noted that these alloys contain Mn as an addition element.
  • the alloys used comprise, on a magnesium basis, from 0 to 11 atom% of aluminum, from 0 to 4 atom% of zinc and from 0.5 to 4 atom% of an addition element such as silicon, germanium, cobalt, tin or antimony.
  • Aluminum or zinc can also be replaced up to 4% by neodymium, praseodymium, yttrium, ceriuni or manganese.
  • the alloys thus obtained have a breaking load of the order of 414 to 482 MPa, an elongation of up to 5% and good resistance to corrosion by aqueous solutions at 3% NaCl.
  • magnesium alloys with high mechanical strength, obtained by rapid solidification which contain, as alloying elements, from 0 to 15 atoms% of aluminum, and from 0 to 4 atom% of zinc (with a total of both between 2 and 15%) and a complementary addition of 0.2 to 3 atom% of at least one element chosen from the group comprising Mn, Ce, Nd, Pr, Y , Ag.
  • This process however requires the use of non-standard magnesium alloys comprising certain elements of addition of high price and of an often difficult solution, and a grinding of the ribbons, obtained during rapid solidification. , prior to compaction.
  • a first object of the present invention relates to magnesium-based alloys, consolidated after rapid solidification, with high mechanical characteristics, having a breaking load at least equal to 290 MPa, but more particularly at least 330 MPa and an elongation at break at least equal to 5% and having, in combination, the following characteristics:
  • the alloy must contain at least one of the elements Zn or Ca or a mixture of the two; when Zn is present, its content is preferably at least 0.2%.
  • Mn When Mn is present, it is an at least quaternary element and its minimum weight content is preferably 0.1%.
  • the alloy has the following preferred weight composition:
  • alloys containing calcium corresponding to the following weight compositions are of interest:
  • the calcium can be in the form of dispersoids of Al 2 Ca precipitated at the grain boundaries and / or in solid solution.
  • the particles of the intermetallic compound Al 2 Ca appear when the Ca concentration is sufficient; they are less than 1 mum in size and preferably less than 0.5 mum in size.
  • the presence of Mn is not necessary if there is already Ca.
  • the sum of the Al-Zn and / or Ca contents does not usually exceed 20%.
  • a second object of the present invention is a process for obtaining these alloys characterized in that said alloy, in the liquid state is added to rapid cooling, at a speed at least equal to 10 4 Ks-1, so to obtain a solidified product of which at least one of the dimensions is less than 150 mm, in that this solidified product is then compacted by spinning at a temperature between 200 and 350 ° C. 4. DESCRIPTION OF THE INVENTION
  • a feature of the invention is that it applies to magnesium alloys of the conventional type, normally intended for foundry (casting) or for working, without any additional addition of alloying element (s) intended to modify its structure as is the case in the prior art.
  • alloys of types G-A3Z1, G-A6Z1, G-A8Z, G-A9Z1, G-A9Z2 (according to French standard NF A 02704), including the chemical composition intervals, were preferably used. have been given previously; they contain in particular additions of Mn.
  • Ca can also be added to it to improve their mechanical characteristics obtained during consolidation at a higher temperature.
  • the process comprises the following stages: a- Elaboration of the alloy from its components (by the conventional processes), or preferably, use of ingots of alloys coming from the usual commercial circuits.
  • these methods are essentially the casting of a thin ribbon on a cooled rotating drum, the spraying of the liquid alloy on a renewed, strongly cooled surface, and the atomization of the liquid alloy in a jet of inert gas.
  • This device essentially comprises, with different variants, a tank of molten alloy, a nozzle for distributing the molten alloy on the surface of a revolving drum, energetically cooled and a means of protection, by inert gas, of the alloy in fusion against oxidation.
  • the operation was carried out on a water-cooled casting drum fitted with a cupro-beryllimum rim.
  • the molten alloy is ejected from the crucible by application of an argon overpressure.
  • the parameters of the casting are as follows:
  • - speed of rotation of the wheel it is of the order of 10 to 40 meters per second at the level of the cooled surface;
  • the alloy must be entirely liquid and fluid. Its temperature must be approximately 50 ° C higher (indicative value) than the liquidus temperature of the alloy.
  • the cooling rate is between 10 5 and 10 6 K. s-1 . Under the conditions described above, long ribbons 30 to 50 mm thick and 1 to 3 mm wide are obtained.
  • the second step aims to consolidate the hyper-dipped ribbons.
  • the spinning conditions were as follows: - temperature between 200 and 350 ° C, which corresponds to the temperature range for spinning conventional magnesium alloys. During our tests, the products, the container of the spinning press and the die were brought to the test temperature before spinning;
  • - feed speed of the press ram from 0.5 to 3 mm per second; in some cases, for example with the presence of Ca, it can be higher (for example 5 mm / sec).
  • the magnesium ribbons can either be directly introduced into the container of a press and spun, or precompacted cold or warm (temperature below, for example 250 ° C.), using a press, in the form of a billet whose density is close to 99% of the theoretical density of the alloy, this billet being subsequently spun, or introduced by cold pre-compacting them to 70% theoretical density, in a sheath made of magnesium or magnesium alloy or aluminum or aluminum alloy, itself introduced into the container of the spinning press; we can then, after spinning, remove the sheath by machining.
  • the sheath can be thin-walled (less than 1 mm) or thick (up to 4 mm). In all cases, it is preferable that the alloy constituting the sheath has a flow limit not exceeding the order of magnitude of that of the product to be spun, at the spinning temperature.
  • a rotating electrode is melted by an electron beam or an electric arc (atomization by rotating electrode), or a liquid jet is mechanically divided in contact with a rotating body and the fine droplets are projected onto a strongly cooled, renewed, or fixed surface, but kept clear, that is to say, without adhesion of the solidified metal particles on said surface; the droplets can also be projected into a stream of inert gas, at low temperature (centrifugal atomization).
  • the parameters of the operation must be chosen so that at least one of the dimensions of the metal particles is less than 150 ⁇ m.
  • the remainder of the method is in accordance with that of the first embodiment, for all the stages of consolidation of the metallic particles.
  • the alloy particles are obtained by atomization of liquid alloy in a jet of inert gas. This operation is also well known in itself and is not part of the invention. It makes it possible to provide particles of dimensions less than a hundred microns. These particles are generally spherical in shape, while those obtained in the previous variant are rather in the form of thin platelets.
  • the products obtained can, before spinning, be degassed at a temperature not exceeding 350 ° C.
  • the procedure can be as follows: the ribbons are cold pre-compacted in a box and all placed in a vacuum oven. The box is vacuum sealed and then spun. But degassing can also be done dynamically: the divided products are degassed and then compacted under vacuum in the form of a billet with closed porosities which is then spun.
  • TYS elastic limit measured at 0.2% elongation in tension
  • CYS elastic limit measured at 0.2% deformation in compression.
  • Table II gives the characteristics of alloys of equivalent compositions, obtained in a conventional manner:
  • the hardness, the elastic limit and the breaking load very strongly depend on the spinning conditions.
  • Table III gathers a certain number of mechanical characteristics of products in AZ91 alloys solidified quickly then compacted by spinning, according to the invention. The parameters were varied: spinning ratio (from 12 to 30), temperature and spinning speed (resp. 200-350 ° C and 0.5-3 mm / s).
  • the remarkable mechanical properties of the alloys according to the invention are essentially due to the fact that the process used leads to a very fine grain structure, of the order of a micrometer (0.7 to 1.5 on average).
  • the optical microscope does not make it possible to resolve the structure and it is only by electron microscopy that it can be verified that the products according to the invention are in fact constituted by a homogeneous matrix reinforced by particles of intermetallic compounds Mg 17 Al 12 of a size less than 0.5 mum, precipitated at the grain boundaries and also of Al 2 Ca, under certain conditions mentioned above.
  • the presence, in the grains, of precipitates ⁇ 0.2 mum of compound based on Al Mn Zn is also noted.
  • the general structure is equiaxial granular. The precipitates do not have the same morphology as the structural hardening precipitates observed on samples of the same alloys obtained by conventional metallurgy.
  • This structure also has remarkable thermal stability, since it remains unchanged after 24 hours of holding at 200 ° C for alloys containing no Ca and up to 350 ° C for those containing it. No softening or hardening occurs, which is not the case for conventional magnesium alloys with structural hardening.
  • the corrosion resistance is evaluated by a measurement of weight loss in a 5% aqueous solution (by weight), of NaCl, the result of which is expressed in "mcd" (milligrams per square centimeter per day).
  • the tests carried out on a set of products according to the invention give results of between 0.4 and 0.6 while the same alloys, transformed into conventional metallurgy, give results of between 0.6 and 2 mcd.
  • the corrosion resistance of the alloys according to the invention is at least equal to that of conventional alloys, and is in fact placed at the level of the resistance of high purity alloys, such as AZ91E produced by the Company DOW CHEMICAL. It can be seen that the alloys according to the invention generally exhibit corrosion without pitting and more homogeneous than that of said AZ91E alloys.
  • the presence of Ca further improves the corrosion resistance; it becomes very slow and extremely homogeneous.
  • the weight loss is 0.075 mg / cm 2 .day whereas for an AZ91 without calcium in test 4 it is 0.4 mg / cm 2 . day.
  • the resistance to softening by prolonged annealing at 200 ° C. constitutes a significant improvement compared to conventional alloys with structural hardening.
  • the corrosion resistance is at the level of that of high purity magnesium alloys which are the subject of a special development therefore at a significant additional cost.

Landscapes

  • 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)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
  • Continuous Casting (AREA)
  • Extrusion Of Metal (AREA)
EP89903172A 1988-02-26 1989-02-23 Hochfeste magnesiumlegierungen und verfahren, um derartige legierungen mittels rascher erstarrung zu erhalten Expired - Lifetime EP0357743B1 (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR8802885A FR2627780B1 (fr) 1988-02-26 1988-02-26 Alliages de magnesium a haute resistance mecanique et procede d'obtention de ces alliages par solidification rapide
FR8802885 1988-02-26
FR8901913 1989-02-01
FR898901913A FR2642439B2 (de) 1988-02-26 1989-02-01

Publications (2)

Publication Number Publication Date
EP0357743A1 true EP0357743A1 (de) 1990-03-14
EP0357743B1 EP0357743B1 (de) 1993-09-29

Family

ID=26226539

Family Applications (1)

Application Number Title Priority Date Filing Date
EP89903172A Expired - Lifetime EP0357743B1 (de) 1988-02-26 1989-02-23 Hochfeste magnesiumlegierungen und verfahren, um derartige legierungen mittels rascher erstarrung zu erhalten

Country Status (6)

Country Link
US (1) US4997622A (de)
EP (1) EP0357743B1 (de)
JP (1) JPH02503331A (de)
DE (1) DE68909544T2 (de)
FR (1) FR2642439B2 (de)
WO (1) WO1989008154A1 (de)

Families Citing this family (85)

* Cited by examiner, † Cited by third party
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US10016810B2 (en) 2015-12-14 2018-07-10 Baker Hughes, A Ge Company, Llc Methods of manufacturing degradable tools using a galvanic carrier and tools manufactured thereof
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JP2019063835A (ja) * 2017-10-04 2019-04-25 株式会社日本製鋼所 マグネシウム合金からなる鍛造用素材の製造方法
CN109321794B (zh) * 2018-10-31 2021-01-19 江苏理工学院 Al2Ca颗粒和碳纳米管混杂增强超轻镁锂基复合材料及制备方法
JP2021063256A (ja) * 2019-10-11 2021-04-22 三菱重工業株式会社 航空機部材の製造方法
CN115652157A (zh) * 2022-10-19 2023-01-31 重庆理工大学 一种低铝含量az系高性能铸造镁合金及其制备方法

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JPH02503331A (ja) 1990-10-11
EP0357743B1 (de) 1993-09-29
FR2642439B2 (de) 1993-04-16
DE68909544D1 (de) 1993-11-04
WO1989008154A1 (fr) 1989-09-08
FR2642439A2 (de) 1990-08-03
DE68909544T2 (de) 1994-01-27
US4997622A (en) 1991-03-05

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