EP4124668A1 - Alliage moulé - Google Patents

Alliage moulé Download PDF

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Publication number
EP4124668A1
EP4124668A1 EP21188809.4A EP21188809A EP4124668A1 EP 4124668 A1 EP4124668 A1 EP 4124668A1 EP 21188809 A EP21188809 A EP 21188809A EP 4124668 A1 EP4124668 A1 EP 4124668A1
Authority
EP
European Patent Office
Prior art keywords
weight
cast alloy
alloy according
iron
alloy
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.)
Pending
Application number
EP21188809.4A
Other languages
German (de)
English (en)
Inventor
Stuart Dr.-Ing. Wiesner
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.)
Aluminium Rheinfelden Alloys GmbH
Original Assignee
Aluminium Rheinfelden Alloys GmbH
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 Aluminium Rheinfelden Alloys GmbH filed Critical Aluminium Rheinfelden Alloys GmbH
Priority to EP21188809.4A priority Critical patent/EP4124668A1/fr
Priority to CN202210897320.6A priority patent/CN115679158A/zh
Priority to JP2022121099A priority patent/JP2023021070A/ja
Priority to US17/876,661 priority patent/US20230043878A1/en
Priority to KR1020220094634A priority patent/KR20230019055A/ko
Publication of EP4124668A1 publication Critical patent/EP4124668A1/fr
Pending legal-status Critical Current

Links

Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D18/00Pressure casting; Vacuum casting
    • B22D18/04Low pressure casting, i.e. making use of pressures up to a few bars to fill the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/007Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon

Definitions

  • the present invention relates to a casting alloy based on aluminum, iron and nickel with the addition of boron. Further the invention relates to the use of the alloy for high pressure die casting or gravity die casting.
  • the alloy according to the invention is used for the production of rotors and stators for electric motors and heat exchangers, cooling and heating elements in the electronics sector or in vehicle construction.
  • Rotor-Aluminum e.g. in qualities of 99.7% Al
  • a metallic body is placed in the die-casting mold and the aluminum rotor or stator is cast into this metallic body.
  • difficulties that arise when casting such an alloy are avoided, above all the high tendency to stick to steel, which otherwise leads to rapid wear of the casting mold.
  • Other typical disadvantages are high shrinkage, very high casting temperatures, poor mechanical machinability and particularly low strength (e.g. Rp0.2 of 20-40 MPa for the alloy Al99.7E).
  • alloys of the AlSi type are often used, e.g. the alloy AlSi9Sr (Castasil-21). Compared to Rotor-Aluminum, these alloy type is better castable. The tendency to stick to the casting mold, shrinkage, mold fillability and casting temperatures are more advantageous. However, the lower electric and thermal conductivity compared to Rotor-Aluminum are disadvantageous. With the help of a heat treatment, an electric conductivity of up to 28 MS / m can be achieved, the thermal conductivity is then 190 (W / K m). The yield strength of such an alloy (Rp0.2) is 80-100 MPa.
  • the applicant's patent EP3 235 916 B1 discloses an alloy of the AlMg4Fe2 (Castaduct-42) type, which is preferably used for crash-relevant structural components in automobile construction.
  • the metallurgical basis of this alloy is the Al3Fe eutectic.
  • the electric conductivity is 16-17 MS / m.
  • One object of the invention is, that at least one disadvantage of the alloys known from the prior art is solved.
  • the alloy has an electric conductivity, preferably of least 23 MS / m, more preferred over 30 MS / m.
  • the alloy should provide a high strength, preferably a Rp0.2 of at least 74 MPa, more preferred over 95 MPa.
  • the alloy according to the inventions consists of: Iron (Fe) 0,8 to3,0 % by weight Nickel (Ni) 0,1 to 3,5 % by weight Boron (B) 40 to 300 ppm Zinc (Zn) 0 - 5 % by weight Tin (Sn) 0 - 5 % by weight Copper (Cu) 0 - 3 % by weight Manganese (Mn) 0 - 1 % by weight Magnesium (Mg) 0 - 0,6 % by weight Phosphorus (P) 0- 500 ppm Silicon (Si) 0 - 0.4% and 0- 0.8% by weight of an element or a group of elements selected from chromium (Cr), lithium (Li), vanadium (V), titanium (Ti), calcium(Ca), molybdenum (Mo) and zirconium (Zr) and the remainder aluminum and inevitable impurities.
  • the iron content lies between 1.0-2.5% by weight.
  • iron content lies between 1.2-2.0% by weight.
  • the iron content lies between 1.4-1.9% by weight.
  • the nickel content lies between 0.3-3.0% by weight.
  • nickel content lies between 0.8-2.0% by weight.
  • the boron content lies between of 70-200 ppm.
  • the boron content lies between 100-1 60 ppm.
  • the boron content lies between 80-150 ppm.
  • the silicon content lies between 0- 0.3% by weight silicon.
  • the copper content lies between 0.2-3% by weight.
  • the copper content lies between 1.0-3.0% .
  • the zinc content lies 0-3% by weight zinc.
  • the zinc content lies between 0.5% to 4.0 by weight of zinc.
  • magnesium content lies between 0-0.4% by weight of magnesium.
  • the magnesium content lies between of 0.2-0.4%.
  • the manganese content lies between 0-0.1% by weight.
  • tin content lies between 0- 2.5% by weight.
  • tin content lies between 0.2-2.5% by weight.
  • the cast alloy is used for high pressure die-casting, preferably for high pressure die casting of rotors and stators for electric motors and heat exchangers, cooling and heating elements in the electronics sector or in vehicle construction.
  • a high pressure die casted product preferably rotors and stators for electric motors and heat exchangers, cooling and heating elements in the electronics sector or in vehicle construction are manufactured from a cast alloy according to the invention.
  • the castability of the alloy according to the invention is achieved by adding the alloying elements iron and nickel, whereby eutectic phases are formed (eutectic phases improve the castability of an alloy).
  • an Al9FeNi phase should be achieved which is, according to the literature, created in the ideal ternary system with a composition of 1.75 wt% Fe and 1.25 wt% Ni.
  • an Al3Fe or Al3Ni phase may also exist.
  • the Al3Ni phase occurs with a high Ni and at the same time a low Fe content.
  • the Fe content should be high and promote the formation of Al9FeNi together with a smaller amount of Al3Fe eutectic. In this way the tendency of the alloy to stick is reduced and the castability is improved.
  • the alloy according to the invention hardly reacts to heat treatments.
  • Heat treatment can have a positive effect on electric conductivity and thermal conductivity.
  • the metallurgical background is mostly an agglomeration of additional elements and a coarsening of the phases, which leads to a better conductivity of the Alpha-AI.
  • the Si content should not exceed 0.4% in order to ensure Si-free eutectics. Up to this level, only an enrichment in the alpha-AI phase is to be expected, which can slightly increase the strength.
  • Mg An element for increasing strength is Mg. It does not form phases with Fe, has a high solubility in Alpha-AI and however, has a negative effect on conductivity (electric and thermal conductivity). In addition, MgNi-containing phases can be formed, which interfere with the formation of an Al9FeNi phase.
  • the alloy according to the invention should therefore either be Mg-free or contain only a small proportion of Mg, preferably maximum 0.6%.
  • Further elements which may have a strength-increasing effect are Sn, Mn, Cr, Li, V, Ti, Ca, Ga, Bi, Mo and Zr.
  • Variants I and J both alloys, known from the prior art named Castaduct-42 and Castasil-21 are shown.
  • Variant T is a further known alloy named, Rotors-Al99.7.
  • Variant K to O refer to gravity die casting (GDC).
  • GDC gravity die casting

Landscapes

  • 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)
  • Crystallography & Structural Chemistry (AREA)
  • Induction Machinery (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Sealing Battery Cases Or Jackets (AREA)
  • Conductive Materials (AREA)
EP21188809.4A 2021-07-30 2021-07-30 Alliage moulé Pending EP4124668A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP21188809.4A EP4124668A1 (fr) 2021-07-30 2021-07-30 Alliage moulé
CN202210897320.6A CN115679158A (zh) 2021-07-30 2022-07-28 铸造合金
JP2022121099A JP2023021070A (ja) 2021-07-30 2022-07-29 鋳造合金
US17/876,661 US20230043878A1 (en) 2021-07-30 2022-07-29 Cast Alloy
KR1020220094634A KR20230019055A (ko) 2021-07-30 2022-07-29 주조 합금

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP21188809.4A EP4124668A1 (fr) 2021-07-30 2021-07-30 Alliage moulé

Publications (1)

Publication Number Publication Date
EP4124668A1 true EP4124668A1 (fr) 2023-02-01

Family

ID=77155681

Family Applications (1)

Application Number Title Priority Date Filing Date
EP21188809.4A Pending EP4124668A1 (fr) 2021-07-30 2021-07-30 Alliage moulé

Country Status (5)

Country Link
US (1) US20230043878A1 (fr)
EP (1) EP4124668A1 (fr)
JP (1) JP2023021070A (fr)
KR (1) KR20230019055A (fr)
CN (1) CN115679158A (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4080222A (en) * 1974-03-01 1978-03-21 Southwire Company Aluminum-iron-nickel alloy electrical conductor
JP2001254135A (ja) * 2000-03-13 2001-09-18 Ryoka Macs Corp 電気伝導性および熱伝導性に優れたアルミニウム合金材
US20160258042A1 (en) * 2015-03-06 2016-09-08 NanoAl LLC. High Temperature Creep Resistant Aluminum Superalloys
CN108130456A (zh) * 2017-12-22 2018-06-08 广州致远新材料科技有限公司 一种高导热压铸铝合金材料及其制备方法
EP3235916B1 (fr) 2016-04-19 2018-08-15 Rheinfelden Alloys GmbH & Co. KG Alliage de moulage

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4080222A (en) * 1974-03-01 1978-03-21 Southwire Company Aluminum-iron-nickel alloy electrical conductor
JP2001254135A (ja) * 2000-03-13 2001-09-18 Ryoka Macs Corp 電気伝導性および熱伝導性に優れたアルミニウム合金材
US20160258042A1 (en) * 2015-03-06 2016-09-08 NanoAl LLC. High Temperature Creep Resistant Aluminum Superalloys
EP3235916B1 (fr) 2016-04-19 2018-08-15 Rheinfelden Alloys GmbH & Co. KG Alliage de moulage
CN108130456A (zh) * 2017-12-22 2018-06-08 广州致远新材料科技有限公司 一种高导热压铸铝合金材料及其制备方法

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
ENGIN SEVDA ET AL: "The effects of microstructure and growth rate on microhardness, tensile strength, and electrical resistivity for directionally solidified Al-Ni-Fe alloys", JOURNAL OF ALLOYS AND COMPOUNDS, ELSEVIER SEQUOIA, LAUSANNE, CH, vol. 660, 19 November 2015 (2015-11-19), pages 23 - 31, XP029351393, ISSN: 0925-8388, DOI: 10.1016/J.JALLCOM.2015.11.080 *

Also Published As

Publication number Publication date
JP2023021070A (ja) 2023-02-09
US20230043878A1 (en) 2023-02-09
KR20230019055A (ko) 2023-02-07
CN115679158A (zh) 2023-02-03

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Inventor name: WIESNER, STUART