SU666897A1 - Alluminium-based alloy - Google Patents
Alluminium-based alloy Download PDFInfo
- Publication number
- SU666897A1 SU666897A1 SU772470788A SU2470788A SU666897A1 SU 666897 A1 SU666897 A1 SU 666897A1 SU 772470788 A SU772470788 A SU 772470788A SU 2470788 A SU2470788 A SU 2470788A SU 666897 A1 SU666897 A1 SU 666897A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- alloy
- based alloy
- alluminium
- aluminum
- mechanical
- Prior art date
Links
- 229910045601 alloy Inorganic materials 0.000 title description 12
- 239000000956 alloy Substances 0.000 title description 12
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Landscapes
- Manufacture And Refinement Of Metals (AREA)
Description
(54) СПЛАВ НА ОСНОВЕ AJTIOIWHHH(54) AJTIOIWHHH BASED ALLOY
1one
Изобретение относитс к металлургии сплавов на основе алюмини , предназначенных дл использовани в различных област х народного хоз йства дл изделий неответственного назначени .The invention relates to the metallurgy of aluminum-based alloys, intended for use in various areas of national economy for non-critical applications.
Известен сплав на основе алюмини , содержащий, вес.%: цинк 1,8-4,0, магний 1,0-2,7; медь 1,0-3,0; кремний 0,1-1.6; марганец 0,01-0,8; хром 0,001-0,25, титан 0,001-0,15; цирконий 0,001-0,15;° железо 0,01-1,0; никель 0,001-0,2; свинец О,001-0,ОЬ, олово 0,001-0,05, сурьму 0,001-0,05; алюминий-остальное p-j.Known alloy based on aluminum, containing, wt.%: Zinc 1.8-4.0, magnesium 1.0-2.7; copper 1.0-3.0; silicon 0.1-1.6; manganese 0.01-0.8; chromium 0.001-0.25, titanium 0.001-0.15; zirconium 0.001-0.15; ° iron 0.01-1.0; nickel 0.001-0.2; lead О, 001-0, ОЬ, tin 0,001-0,05, antimony 0,001-0,05; aluminum rest p-j.
Сплав обладает средним уровнем еханических свойств и вовлечение в него неиспользуемых оборотных отходов, содержащих литий и кгщмий, не пред- 20 ставл етс возможным.The alloy has an average level of mechanical properties and the involvement in it of unused recycling waste containing lithium and kgms is not possible.
Наиболее близким к предложенному вл етс сплав на основе алюмини , содержащий , вес.%: цинк 3, магНИИ 0,6-2,5-, марганец и,2-0,5; хром 25 0,15-0,25, титан 0,01-1,2, цирконий 0,01-0,2, бериллий 0,0005-0,0015, . алюминий - остальное, в сплаве допускаетс также присутствие следующих злементов, вес.The closest to the proposed is an aluminum-based alloy containing, in wt.%: Zinc 3, magnetic institute 0.6-2.5, manganese and, 2-0.5; chromium 25 0.15-0.25, titanium 0.01-1.2, zirconium 0.01-0.2, beryllium 0.0005-0.0015,. aluminum - the rest; the presence of the following elements, weight, is also allowed in the alloy.
железо 1,0, кремний 2,0, бор 0,1, кадг-мй 0,2; серебро 0,5 и (или) медь 0,5 Р.iron 1.0, silicon 2.0, boron 0.1, cad-mi 0.2; silver 0.5 and (or) copper 0.5 R.
Известный сплав имеет недостаточно высокие прочностные свойства.Known alloy has not enough high strength properties.
С целью повышени 1.1еханических свойств, а также объема использовани вторичного сырь в сплав на основе алюмини , содержащий цинк, магний , медь, кремний, марганеи, хром, титан, цирконий, железо, бериллий дополнительно введен по крайней мере один металл, выбранный из группы, .содержащей кадмий и литий, при следующем соотношении компонентов, вес.In order to improve the 1.1 mechanical properties, as well as the volume of use of secondary raw materials, at least one metal selected from the group containing cadmium and lithium, with the following ratio of components, weight.
4,1-6,54.1-6.5
1,0-2,71.0-2.7
1,0-3,01.0-3.0
0,1-2,00.1-2.0
0,01-0,80.01-0.8
0,001-0,250.001-0.25
0,001-0,150.001-0.15
0,001-0,150.001-0.15
0,01-1,5 0,0001-0,01 ранный из группы, содериращей0.01-1.5 0.0001-0.01 wounded from the group
литий-0,001-1,0lithium-0,001-1,0
Кадмий0,001-0,5Cadmium0.001-0.5
Алюминий Остальное В сплаве допускаетс присутств следуклцих примесей, вес.%: Никель --.,0,0001-0,2 Олово0,0001-0,05Aluminum Else In the alloy, the presence of the following impurities is allowed, wt.%: Nickel - .0001-0.2 Tin0.0001-0.05
Свинец а,0001-0,05 Дл опр обовани предложенного сплава были приготовлены плавки, тавы которых приведены в табл. 1. БЫЛИ отлиты слитки 270 и .70 мм. После гомогенизащии при 24 Lead a, 0001-0.05 For fusing the proposed alloy, melts were prepared, the tavas of which are listed in Table. 1. There were cast ingots of 270 and .70 mm. After homogenizing at 24
проводили прессование прутков 20 мм и полос мм. Результаты определени гор челомкости, приведены в табл. 2, механические и коррозионные свойства - в табл. 3 дл закален ного и естественно состаренного состо ни . Как видно из данных табл. 2 и 3. предложенный сплав имеет преимущества по механическим и литейным свойствам (гор челомкости) по сравнению с ИЗВеСТНЕз1М.carried out the extrusion of rods 20 mm and mm bands. The results of determining the mountains of chelomkost are given in table. 2, mechanical and corrosion properties - in table. 3 for the hardened and naturally aged state. As can be seen from the data table. 2 and 3. The proposed alloy has advantages in mechanical and casting properties (of chelokomosti mountains) as compared with IZVESTNZ1M.
Как видно из данных табл. 2 и 3 предложенный сплав обладает хорошим комплексом механических и технологических свой ст в.As can be seen from the data table. 2 and 3, the proposed alloy has a good complex of mechanical and technological features of its own.
Таблица2Table 2
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU772470788A SU666897A1 (en) | 1977-04-04 | 1977-04-04 | Alluminium-based alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU772470788A SU666897A1 (en) | 1977-04-04 | 1977-04-04 | Alluminium-based alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU666897A1 true SU666897A1 (en) | 1981-01-30 |
Family
ID=20702795
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU772470788A SU666897A1 (en) | 1977-04-04 | 1977-04-04 | Alluminium-based alloy |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU666897A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2716722C2 (en) * | 2014-10-26 | 2020-03-16 | КАЙЗЕР АЛЮМИНУМ ФАБРИКЕЙТЕД ПРОДАКТС, ЭлЭлСи | Aluminum-lithium alloys with high strength, high deformability and low cost |
| CN111778434A (en) * | 2020-08-04 | 2020-10-16 | 保定市兴润车桥制造有限公司 | High-strength aluminum alloy material for axle |
| US12123078B2 (en) | 2019-02-20 | 2024-10-22 | Howmet Aerospace Inc. | Aluminum-magnesium-zinc aluminum alloys |
-
1977
- 1977-04-04 SU SU772470788A patent/SU666897A1/en active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2716722C2 (en) * | 2014-10-26 | 2020-03-16 | КАЙЗЕР АЛЮМИНУМ ФАБРИКЕЙТЕД ПРОДАКТС, ЭлЭлСи | Aluminum-lithium alloys with high strength, high deformability and low cost |
| US12123078B2 (en) | 2019-02-20 | 2024-10-22 | Howmet Aerospace Inc. | Aluminum-magnesium-zinc aluminum alloys |
| CN111778434A (en) * | 2020-08-04 | 2020-10-16 | 保定市兴润车桥制造有限公司 | High-strength aluminum alloy material for axle |
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