RU2018130158A - ALUMINUM AL-MG-SI THERMALLY STRENGTHENED ALUMINUM ALLOY - Google Patents

ALUMINUM AL-MG-SI THERMALLY STRENGTHENED ALUMINUM ALLOY Download PDF

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RU2018130158A
RU2018130158A RU2018130158A RU2018130158A RU2018130158A RU 2018130158 A RU2018130158 A RU 2018130158A RU 2018130158 A RU2018130158 A RU 2018130158A RU 2018130158 A RU2018130158 A RU 2018130158A RU 2018130158 A RU2018130158 A RU 2018130158A
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Russia
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aluminum alloy
paragraphs
alloy according
aluminum
maximum
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RU2018130158A
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Russian (ru)
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RU2737646C2 (en
RU2018130158A3 (en
Inventor
Хельмут АНТРЕКОВИЧ
Томас ЭБНЕР
Вернер ФРАГНЕР
Хельмут КАУФМАНН
Штефан ПОГАЧЕР
Рамона ПРИЛЛЬХОФЕР
Петер Й. УГГОВИТЦЕР
Марион ВЕРИНОС
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Амаг Роллинг Гмбх
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    • 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
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • C22C30/04—Alloys containing less than 50% by weight of each constituent containing tin or lead
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • C22C30/06—Alloys containing less than 50% by weight of each constituent containing zinc
    • 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
    • C22F1/047—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 of alloys with magnesium as the next major constituent

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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)
  • Cell Electrode Carriers And Collectors (AREA)
  • Laminated Bodies (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Sealing Battery Cases Or Jackets (AREA)
  • Heat Treatment Of Steel (AREA)
  • Conductive Materials (AREA)
  • Battery Electrode And Active Subsutance (AREA)
  • Materials For Medical Uses (AREA)
  • Continuous Casting (AREA)
  • Powder Metallurgy (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)

Claims (27)

1. Термически упрочняемый алюминиевый сплав на основе Al-Mg-Si, содержащий1. Thermally hardened aluminum alloy based on Al-Mg-Si, containing от 0,6 до 1 мас.% магния (Mg)from 0.6 to 1 wt.% magnesium (Mg) от 0,2 до 0,7 мас.% кремния (Si)0.2 to 0.7 wt.% silicon (Si) от 0,16 до 0,7 мас.% железа (Fe)from 0.16 to 0.7 wt.% iron (Fe) от 0,05 до 0,4 мас.% меди (Cu)from 0.05 to 0.4 wt.% copper (Cu) максимум 0,15 мас.% марганца (Mn)maximum 0.15 wt.% manganese (Mn) максимум 0,35 мас.% хрома (Cr)maximum 0.35 wt.% chromium (Cr) максимум 0,2 мас.% циркония (Zr)maximum 0.2 wt.% zirconium (Zr) максимум 0,25 мас.% цинка (Zn)maximum 0.25 wt.% zinc (Zn) максимум 0,15 мас.% титана (Ti)maximum 0.15 wt.% titanium (Ti) 0,005-0,075 мас.% олова (Sn) и/или индия (In),0.005-0.075 wt.% Tin (Sn) and / or indium (In), а остальное - алюминий, а также обусловленные производством неизбежные примеси, причемand the rest is aluminum, as well as inevitable impurities due to production, moreover отношение массовых процентных содержаний Si/Fe меньше 2,5,the ratio of mass percentages of Si / Fe is less than 2.5, и содержание Si определяется по уравнениюand the Si content is determined by the equation мас.% Si = A + [0,3 * (мас.% Fe)]wt.% Si = A + [0.3 * (wt.% Fe)] с параметром A в интервале от 0,17 до 0,4 мас.%.with a parameter in the range from 0.17 to 0.4 wt.%. 2. Алюминиевый сплав по п. 1, отличающийся тем, что параметр A лежит в интервале от 0,26 до 0,34 мас.%.2. The aluminum alloy according to claim 1, characterized in that the parameter A lies in the range from 0.26 to 0.34 wt.%. 3. Алюминиевый сплав по п. 1 или 2, отличающийся тем, что параметр A составляет 0,3 мас.%.3. The aluminum alloy according to claim 1 or 2, characterized in that the parameter A is 0.3 wt.%. 4. Алюминиевый сплав по пп. 1, 2 или 3, отличающийся тем, что содержание Si определяется по уравнению4. Aluminum alloy according to paragraphs. 1, 2 or 3, characterized in that the Si content is determined by the equation мас.% Si = A + [0,3 * (мас.% Fe)] - мас.% Ti.wt.% Si = A + [0.3 * (wt.% Fe)] - wt.% Ti. 5. Алюминиевый сплав по любому из пп. 1-4, отличающийся тем, что отношение массовых процентных содержаний Si/Fe меньше 2.5. Aluminum alloy according to any one of paragraphs. 1-4, characterized in that the ratio of mass percentages of Si / Fe is less than 2. 6. Алюминиевый сплав по любому из пп. 1-5, отличающийся тем, что отношение массовых процентных содержаний Si/Mg лежит в интервале от 0,3 до 0,9.6. Aluminum alloy according to any one of paragraphs. 1-5, characterized in that the ratio of mass percentages of Si / Mg lies in the range from 0.3 to 0.9. 7. Алюминиевый сплав по любому из пп. 1-6, отличающийся тем, что алюминиевый сплав содержит по меньшей мере 0,25 мас.% меди (Cu).7. Aluminum alloy according to any one of paragraphs. 1-6, characterized in that the aluminum alloy contains at least 0.25 wt.% Copper (Cu). 8. Алюминиевый сплав по любому из пп. 1-7, отличающийся тем, что алюминиевый сплав содержит в интервале от 0,005 до 0,05 мас.% олова (Sn) в кристаллическом твердом растворе алюминия.8. Aluminum alloy according to any one of paragraphs. 1-7, characterized in that the aluminum alloy contains in the range from 0.005 to 0.05 wt.% Tin (Sn) in a crystalline solid solution of aluminum. 9. Алюминиевый сплав по любому из пп. 1-8, отличающийся тем, что алюминиевый сплав относится к серии 6xxx.9. Aluminum alloy according to any one of paragraphs. 1-8, characterized in that the aluminum alloy belongs to the 6xxx series. 10. Алюминиевый сплав по любому из пп. 1-9, отличающийся тем, что алюминиевый сплав содержит максимум 0,05 мас.% хрома (Cr) и более 0,05 мас.% циркония (Zr).10. Aluminum alloy according to any one of paragraphs. 1-9, characterized in that the aluminum alloy contains a maximum of 0.05 wt.% Chromium (Cr) and more than 0.05 wt.% Zirconium (Zr). 11. Алюминиевый сплав по любому из пп. 1-10, отличающийся тем, что алюминиевый сплав содержит по меньшей мере 0,02 мас.% хрома (Cr).11. Aluminum alloy according to any one of paragraphs. 1-10, characterized in that the aluminum alloy contains at least 0.02 wt.% Chromium (Cr).
RU2018130158A 2016-01-22 2017-01-20 THERMALLY HARDENED ALUMINIUM ALLOY BASED ON Al-Mg-Si RU2737646C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP16152467.3A EP3196324B1 (en) 2016-01-22 2016-01-22 Curable aluminium alloy on an al-mg-si-basis
EP16152467.3 2016-01-22
PCT/EP2017/051243 WO2017125582A1 (en) 2016-01-22 2017-01-20 Hardenable almgsi-based aluminum alloy

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RU2018130158A true RU2018130158A (en) 2020-02-25
RU2018130158A3 RU2018130158A3 (en) 2020-02-25
RU2737646C2 RU2737646C2 (en) 2020-12-02

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US (1) US20190024219A1 (en)
EP (2) EP3196324B1 (en)
JP (1) JP7208005B2 (en)
KR (1) KR102649425B1 (en)
CN (1) CN108779522B (en)
AU (1) AU2017208641A1 (en)
BR (1) BR112018014843B1 (en)
CA (1) CA3011631A1 (en)
CL (1) CL2018001954A1 (en)
ES (1) ES2702729T3 (en)
IL (1) IL260680B (en)
MX (1) MX2018008973A (en)
PL (1) PL3196324T3 (en)
RU (1) RU2737646C2 (en)
SG (2) SG10202007019WA (en)
SI (1) SI3196324T1 (en)
TR (1) TR201814631T1 (en)
WO (1) WO2017125582A1 (en)
ZA (1) ZA201804669B (en)

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WO2024086068A1 (en) * 2022-10-20 2024-04-25 Arconic Technologies, Llc New 6xxx aluminum alloys

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MX2018008973A (en) 2019-01-21
SI3196324T1 (en) 2019-03-29
SG11201806220YA (en) 2018-08-30
RU2737646C2 (en) 2020-12-02
KR102649425B1 (en) 2024-03-19
JP7208005B2 (en) 2023-01-18
JP2019507248A (en) 2019-03-14
BR112018014843B1 (en) 2022-11-29
CN108779522A (en) 2018-11-09
CA3011631A1 (en) 2017-07-27
EP3196324B1 (en) 2018-09-19
AU2017208641A1 (en) 2018-08-02
ES2702729T3 (en) 2019-03-05
TR201814631T1 (en) 2018-11-21
CL2018001954A1 (en) 2019-01-25
WO2017125582A1 (en) 2017-07-27
RU2018130158A3 (en) 2020-02-25
CN108779522B (en) 2020-12-11
KR20180136434A (en) 2018-12-24
IL260680B (en) 2021-08-31
US20190024219A1 (en) 2019-01-24
EP3196324A1 (en) 2017-07-26
SG10202007019WA (en) 2020-08-28
EP3443134A1 (en) 2019-02-20
BR112018014843A2 (en) 2020-10-27
PL3196324T3 (en) 2019-04-30
ZA201804669B (en) 2021-03-31

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