WO2020224627A1 - Matériau en alliage et procédé de production associé - Google Patents
Matériau en alliage et procédé de production associé Download PDFInfo
- Publication number
- WO2020224627A1 WO2020224627A1 PCT/CN2020/089072 CN2020089072W WO2020224627A1 WO 2020224627 A1 WO2020224627 A1 WO 2020224627A1 CN 2020089072 W CN2020089072 W CN 2020089072W WO 2020224627 A1 WO2020224627 A1 WO 2020224627A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- alloy material
- alloy
- alloy liquid
- temperature
- production process
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- 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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- 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
- C22F1/043—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 silicon as the next major constituent
Definitions
- the invention relates to the technical field of alloy materials, in particular to an alloy material and its production process.
- 6061-T6 is called aviation duralumin, which is light, high in strength and high in production cost. It is the abbreviation of T6 hardening treatment of 6061 aviation aluminum alloy. It has good formability, weldability, machinability, and medium strength. It can still maintain good operability after annealing. Typical applications are aviation fixtures, trucks, tower buildings, ships, pipelines and other building applications that require strength, weldability and corrosion resistance. How to improve its tensile strength and yield strength to increase its application range is exactly the problem that the inventors have to solve.
- the main purpose of the present invention is to provide an alloy material with high tensile strength and high yield strength.
- an alloy material comprising the following components by weight
- the Si content is 1.11%.
- the Mn content is 0.69%.
- An alloy material production process including the following steps:
- the smelting furnace is heated to 705-750°C at a rate of 260-280°C/h.
- the aluminum alloy material provided by the present invention has high strength, high hardness, excellent mechanical properties and mechanical properties, better tensile strength and yield strength, and can satisfy various applications. Requirements for strength, toughness, wear resistance, corrosion resistance, fatigue resistance, high temperature resistance, low temperature resistance, radiation resistance, fire resistance, explosion resistance, easy cutting, easy polishing, surface treatment, welding, and ultra-light are required.
- the process provided by the invention is simple and reasonable, and the production efficiency is high.
- An alloy material including the following components by weight,
- the Si content is 1.11%.
- the Mn content is 0.69%.
- the alloy material of this scheme has higher Si and Mn content, and has better tensile strength and yield strength.
- the specific comparison parameters are as follows:
- the alloy material provided by the present invention has a very large improvement in tensile strength and yield strength compared to 6061-T6.
- An alloy material production process including the following steps:
- the smelting furnace is heated to 705-750°C at a rate of 260-280°C/h.
- the aluminum alloy material provided by the invention has high strength, high hardness, excellent mechanical properties and mechanical properties, better tensile strength and yield strength, and can meet various requirements for strength, toughness, wear resistance, and corrosion resistance. , Fatigue resistance, high temperature resistance, low temperature resistance, radiation resistance, fire resistance, explosion resistance, easy cutting, easy polishing, surface treatment, welding and ultra-light requirements.
- the process provided by the invention is simple and reasonable, and the production efficiency is high.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Extrusion Of Metal (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
Abstract
La présente invention concerne un matériau en alliage et un procédé de production de barres fabriquées à partir de celui-ci. La présente invention concerne un matériau en alliage comprenant les composants suivants en poids : 0,8 à 1,2 % de Si, 0 à 0,5 % de Fe, 0,15 à 0,6 % de Cu, 0,2 à 0,8 % de Mn, 0,6 à 0,1 % de Mg, 0 à 0,1 % de Cr, 0 à 0,25 % de Zn et 0 à 0,1 % de Ti, le reste étant AL, la teneur en Si étant de 1,11 %, et la teneur en Mn étant de 0,69 %. L'invention concerne en outre un procédé de production d'un matériau en alliage comprenant les étapes suivantes consistant à : (1) Peser les matières premières de chaque composant en pourcentage en masse ; (2) placer les matières premières dans un four de fusion et les faire fondre en un liquide d'alliage, la température du liquide d'alliage pouvant atteindre 705 à 750 °C, maintenir ladite température pendant 45 à 60 min ; (3) réduire la température du liquide d'alliage à 520-580 °C, ajouter un agent de raffinage, augmenter la température à 670-710 °C, et réaliser une inspection des composants ; (4) laisser reposer le liquide d'alliage et refroidir celui-ci à 650-660 °C, effectuer un remplissage de moule, et refroidir le liquide d'alliage en barres. Le matériau en alliage fourni par la présente invention est caractérisé par une résistance à la traction élevée et une grande limite d'élasticité.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US17/283,017 US20210340649A1 (en) | 2019-05-08 | 2020-05-07 | Alloy material and process of manufacturing same |
JP2021525305A JP2022512995A (ja) | 2019-05-08 | 2020-05-07 | 合金材料の一種及びその生産プロセス |
EP20802186.5A EP3967784A4 (fr) | 2019-05-08 | 2020-05-07 | Matériau en alliage et procédé de production associé |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910380080.0 | 2019-05-08 | ||
CN201910380080.0A CN110079709A (zh) | 2019-05-08 | 2019-05-08 | 一种合金材料及其生产工艺 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2020224627A1 true WO2020224627A1 (fr) | 2020-11-12 |
Family
ID=67419151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2020/089072 WO2020224627A1 (fr) | 2019-05-08 | 2020-05-07 | Matériau en alliage et procédé de production associé |
Country Status (5)
Country | Link |
---|---|
US (1) | US20210340649A1 (fr) |
EP (1) | EP3967784A4 (fr) |
JP (1) | JP2022512995A (fr) |
CN (1) | CN110079709A (fr) |
WO (1) | WO2020224627A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110079709A (zh) * | 2019-05-08 | 2019-08-02 | 常熟希那基汽车零件有限公司 | 一种合金材料及其生产工艺 |
CN112921207A (zh) * | 2019-12-06 | 2021-06-08 | 湖南创安防爆电器有限公司 | 一种阻隔防爆材料 |
CN114855013B (zh) * | 2022-05-30 | 2023-02-28 | 栋梁铝业有限公司 | 一种低温快速挤压成型铝合金的方法及其应用 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2219860A1 (fr) * | 2007-11-05 | 2010-08-25 | Novelis Inc. | Produit de tôle plaquée et son procédé de production |
CN102776423A (zh) * | 2011-05-12 | 2012-11-14 | 张家港市金邦铝业有限公司 | 一种铝合金 |
WO2016115120A1 (fr) * | 2015-01-12 | 2016-07-21 | Novelis Inc. | Tôle d'aluminium hautement déformable pour l'industrie automobile à striage réduit ou nul et procédé de préparation |
CN106967894A (zh) * | 2017-04-13 | 2017-07-21 | 广西大学 | 一种6010铝合金熔铸工艺 |
CN108425046A (zh) * | 2018-03-28 | 2018-08-21 | 广西南南铝加工有限公司 | 阳极氧化用铝合金及其制备方法 |
CN109628860A (zh) * | 2018-12-17 | 2019-04-16 | 广东坚美铝型材厂(集团)有限公司 | 一种高强度Al-Mg-Si铝合金及其制备方法 |
CN110079709A (zh) * | 2019-05-08 | 2019-08-02 | 常熟希那基汽车零件有限公司 | 一种合金材料及其生产工艺 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH062064A (ja) * | 1992-06-15 | 1994-01-11 | Kobe Steel Ltd | 高強度高成形性Al−Mg−Si系合金とその製造方法 |
FR2713664B1 (fr) * | 1993-11-17 | 1996-05-24 | Pechiney Rhenalu | Alliage type Al-Si-Mg à ductilité et emboutissabilité améliorées et procédé d'obtention. |
JP2000282163A (ja) * | 1999-03-30 | 2000-10-10 | Kobe Steel Ltd | 張出し成形性及び曲げ成形性に優れたAl−Mg−Si系合金板 |
TW200536946A (en) * | 2003-12-11 | 2005-11-16 | Nippon Light Metal Co | Method for producing Al-Mg-Si alloy excellent in bake-hardenability and hemmability |
JP5758676B2 (ja) * | 2011-03-31 | 2015-08-05 | 株式会社神戸製鋼所 | 成形加工用アルミニウム合金板およびその製造方法 |
JP6316747B2 (ja) * | 2012-06-27 | 2018-04-25 | 株式会社Uacj | ブロー成形用アルミニウム合金板およびその製造方法 |
JP2018070947A (ja) * | 2016-10-28 | 2018-05-10 | 株式会社神戸製鋼所 | アルミニウム合金板 |
-
2019
- 2019-05-08 CN CN201910380080.0A patent/CN110079709A/zh active Pending
-
2020
- 2020-05-07 EP EP20802186.5A patent/EP3967784A4/fr not_active Withdrawn
- 2020-05-07 WO PCT/CN2020/089072 patent/WO2020224627A1/fr unknown
- 2020-05-07 US US17/283,017 patent/US20210340649A1/en not_active Abandoned
- 2020-05-07 JP JP2021525305A patent/JP2022512995A/ja active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2219860A1 (fr) * | 2007-11-05 | 2010-08-25 | Novelis Inc. | Produit de tôle plaquée et son procédé de production |
CN102776423A (zh) * | 2011-05-12 | 2012-11-14 | 张家港市金邦铝业有限公司 | 一种铝合金 |
WO2016115120A1 (fr) * | 2015-01-12 | 2016-07-21 | Novelis Inc. | Tôle d'aluminium hautement déformable pour l'industrie automobile à striage réduit ou nul et procédé de préparation |
CN106967894A (zh) * | 2017-04-13 | 2017-07-21 | 广西大学 | 一种6010铝合金熔铸工艺 |
CN108425046A (zh) * | 2018-03-28 | 2018-08-21 | 广西南南铝加工有限公司 | 阳极氧化用铝合金及其制备方法 |
CN109628860A (zh) * | 2018-12-17 | 2019-04-16 | 广东坚美铝型材厂(集团)有限公司 | 一种高强度Al-Mg-Si铝合金及其制备方法 |
CN110079709A (zh) * | 2019-05-08 | 2019-08-02 | 常熟希那基汽车零件有限公司 | 一种合金材料及其生产工艺 |
Non-Patent Citations (1)
Title |
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See also references of EP3967784A4 * |
Also Published As
Publication number | Publication date |
---|---|
EP3967784A4 (fr) | 2022-08-10 |
CN110079709A (zh) | 2019-08-02 |
EP3967784A1 (fr) | 2022-03-16 |
JP2022512995A (ja) | 2022-02-07 |
US20210340649A1 (en) | 2021-11-04 |
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