RU2447174C1 - Aluminium-based cast alloy - Google Patents
Aluminium-based cast alloy Download PDFInfo
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- RU2447174C1 RU2447174C1 RU2011112952/02A RU2011112952A RU2447174C1 RU 2447174 C1 RU2447174 C1 RU 2447174C1 RU 2011112952/02 A RU2011112952/02 A RU 2011112952/02A RU 2011112952 A RU2011112952 A RU 2011112952A RU 2447174 C1 RU2447174 C1 RU 2447174C1
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- RU
- Russia
- Prior art keywords
- alloy
- aluminium
- casting
- cast alloy
- aluminum
- Prior art date
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- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 11
- 239000000956 alloy Substances 0.000 title abstract description 20
- 229910045601 alloy Inorganic materials 0.000 title abstract description 20
- 239000004411 aluminium Substances 0.000 title abstract 2
- 239000010949 copper Substances 0.000 claims description 10
- 239000010936 titanium Substances 0.000 claims description 10
- 239000011777 magnesium Substances 0.000 claims description 9
- 239000011701 zinc Substances 0.000 claims description 7
- 229910052749 magnesium Inorganic materials 0.000 claims description 5
- 239000011572 manganese Substances 0.000 claims description 5
- 229910052706 scandium Inorganic materials 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 3
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 claims 1
- 239000000203 mixture Substances 0.000 abstract description 4
- 229910052751 metal Inorganic materials 0.000 abstract description 2
- 239000002184 metal Substances 0.000 abstract description 2
- 239000000126 substance Substances 0.000 abstract 2
- 238000005272 metallurgy Methods 0.000 abstract 1
- 238000005266 casting Methods 0.000 description 19
- 229910017818 Cu—Mg Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 229910018131 Al-Mn Inorganic materials 0.000 description 1
- 229910018182 Al—Cu Inorganic materials 0.000 description 1
- 229910018461 Al—Mn Inorganic materials 0.000 description 1
- 229910018575 Al—Ti Inorganic materials 0.000 description 1
- 229910018580 Al—Zr Inorganic materials 0.000 description 1
- BJZIJOLEWHWTJO-UHFFFAOYSA-H dipotassium;hexafluorozirconium(2-) Chemical compound [F-].[F-].[F-].[F-].[F-].[F-].[K+].[K+].[Zr+4] BJZIJOLEWHWTJO-UHFFFAOYSA-H 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000009856 non-ferrous metallurgy Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003908 quality control method Methods 0.000 description 1
Landscapes
- Continuous Casting (AREA)
Abstract
Description
Изобретение относится к цветной металлургии, в частности, к литейным сплавам на основе алюминия, применяемым в авиационной технике и других отраслях машиностроения для нагруженных деталей внутреннего набора фюзеляжа, деталей управления, силовых кронштейнов и др. взамен штамповок, работающих длительно до 250°C.The invention relates to non-ferrous metallurgy, in particular, to casting alloys based on aluminum, used in aircraft and other engineering industries for loaded parts of the internal fuselage set, control parts, power brackets, etc. in exchange for stampings operating for a long time up to 250 ° C.
Известен литейный сплав на основе алюминия, содержащий (мас.%):Known casting alloy based on aluminum, containing (wt.%):
Сплав обладает пониженными значениями механических и литейных свойств.The alloy has reduced values of mechanical and casting properties.
Известен высокопрочный литейный сплав на основе алюминия, содержащий (мас.%):Known high-strength casting alloy based on aluminum, containing (wt.%):
Известен также высокопрочный литейный сплав на основе алюминия, содержащий (мас.%):Also known is a high-strength casting alloy based on aluminum, containing (wt.%):
Известные сплавы имеют низкую технологичность при литье в песчаные формы.Known alloys have low manufacturability when casting in sand forms.
Наиболее близким аналогом, взятым за прототип, является литейный сплав на основе алюминия, содержащий медь, магний, титан, цирконий при следующем соотношении компонентов, мас.%:The closest analogue taken for the prototype is a casting alloy based on aluminum, containing copper, magnesium, titanium, zirconium in the following ratio of components, wt.%:
Недостатком сплава-прототипа являются недостаточно высокие литейные свойства, предел прочности и качество отливок.The disadvantage of the prototype alloy is not high enough casting properties, tensile strength and quality of castings.
Технической задачей предлагаемого изобретения является создание литейного сплава на основе алюминия, обладающего повышенными литейными свойствами (жидкотекучестью и горячеломкостью), пределом прочности, что позволит повысить качество сложных по конфигурации фасонных отливок.The technical task of the invention is the creation of a casting alloy based on aluminum with improved casting properties (fluidity and heat resistance), tensile strength, which will improve the quality of complex configuration shaped castings.
Поставленная техническая задача достигается тем, что предложен литейный сплав на основе алюминия, содержащий медь, магний, титан, цирконий, отличающийся тем, что дополнительно содержит марганец, цинк, скандий при следующем соотношении компонентов (мас.%):The technical task is achieved by the fact that the proposed casting alloy based on aluminum, containing copper, magnesium, titanium, zirconium, characterized in that it further contains manganese, zinc, scandium in the following ratio of components (wt.%):
Установлено, что при заявленном соотношении и содержании компонентов при введении марганца, цинка, скандия повышаются литейные и прочностные свойства.It is established that with the stated ratio and content of components with the introduction of manganese, zinc, scandium, the foundry and strength properties increase.
Примеры осуществленияExamples of implementation
Пример 1.Example 1
Приготовление опытного сплава в электропечи состава Al - 3,5% Cu - 0,2% Mg - 0,1% Ti - 0,1% Zr - 0,2% Mn - 0,5% Zn - 0,15% Sc.Preparation of an experimental alloy in an electric furnace with the composition Al - 3.5% Cu - 0.2% Mg - 0.1% Ti - 0.1% Zr - 0.2% Mn - 0.5% Zn - 0.15% Sc.
В предварительно нагретую электропечь загрузили и расплавили чушковой алюминий. Затем вводили лигатуры Al-Cu, Al-Mn и Al-Ti, Al-Sc, Al-Zr, магний и цинк, расплав перемешивали, выстаивали, обрабатывали фторцирконатом калия. Состав опытного сплава и значения механических и технологических свойств приведены в таблицах 1, 2.Aluminum was loaded and melted into the preheated electric furnace. Then ligatures Al-Cu, Al-Mn and Al-Ti, Al-Sc, Al-Zr, magnesium and zinc were introduced, the melt was mixed, aged, treated with potassium fluorozirconate. The composition of the experimental alloy and the values of mechanical and technological properties are given in tables 1, 2.
Примеры 2, 3 - аналогичны примеру 1, пример 4 - прототип. Составы сплавов приведены в таблице 1.Examples 2, 3 are similar to example 1, example 4 is a prototype. The alloy compositions are shown in table 1.
В таблице 2 приведены механические и технологические свойства образцов, вырезанных из отливок предлагаемого сплава и сплава-прототипа, системы Al-Cu-Mg.Table 2 shows the mechanical and technological properties of samples cut from castings of the proposed alloy and prototype alloy, the Al-Cu-Mg system.
Механические свойства определялись после термообработки по режиму Т5: закалка + искусственное старение, для сплава-прототипа по режиму Т4: закалка + естественное старение.The mechanical properties were determined after heat treatment according to the T5 mode: hardening + artificial aging, for the prototype alloy according to the T4 mode: hardening + natural aging.
Из таблицы 2 следует, что для отливок (корпуса, крышки) из предлагаемого сплава технологические свойства значительно выше по сравнению с прототипом: жидкотекучесть повышается на 20-24%, горячеломкость снижается на 60%, линейная усадка снижается на 15%. Предел прочности возрастает на 5-7,5%.From table 2 it follows that for castings (body, lid) of the proposed alloy, the technological properties are significantly higher compared to the prototype: fluidity increases by 20-24%, heat resistance decreases by 60%, linear shrinkage decreases by 15%. The tensile strength increases by 5-7.5%.
Фасонные отливки прошли контроль качества. Брака по литью не обнаружено.Shaped castings passed quality control. No castings were found.
Таким образом, применение предлагаемого сплава системы Al-Cu-Mg в изделиях для фасонных отливок сложной конфигурации деталей внутреннего набора позволит получать качественные отливки с высокими технологическими свойствами при прочностных свойствах на уровне прототипа. Это снизит металлоемкость и повысит надежность в эксплуатации и ресурс изделий.Thus, the use of the proposed alloy of the Al-Cu-Mg system in products for shaped castings of complex configuration of parts of the inner set will allow to obtain high-quality castings with high technological properties with strength properties at the level of the prototype. This will reduce the metal consumption and increase the reliability in operation and resource of products.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2011112952/02A RU2447174C1 (en) | 2011-04-05 | 2011-04-05 | Aluminium-based cast alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2011112952/02A RU2447174C1 (en) | 2011-04-05 | 2011-04-05 | Aluminium-based cast alloy |
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| Publication Number | Publication Date |
|---|---|
| RU2447174C1 true RU2447174C1 (en) | 2012-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2011112952/02A RU2447174C1 (en) | 2011-04-05 | 2011-04-05 | Aluminium-based cast alloy |
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| RU (1) | RU2447174C1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109112372A (en) * | 2018-10-17 | 2019-01-01 | 合肥月煌新型装饰材料有限公司 | A kind of high-strength abrasion-proof aluminum alloy materials and preparation method thereof |
| CN111020319A (en) * | 2019-12-02 | 2020-04-17 | 南昌航空大学 | A special wire for additive manufacturing of high-strength aluminum-copper alloy and its preparation method and application |
| CN117701960A (en) * | 2023-12-18 | 2024-03-15 | 中南大学 | A high-elongation cast Al-Cu-Zn-Mg alloy with good thermal crack resistance and its preparation method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2454509A1 (en) * | 2001-07-25 | 2003-02-06 | Showa Denko K.K. | Aluminum alloy excellent in machinability, and aluminum alloy material and method for production thereof |
| RU2218437C1 (en) * | 2002-06-26 | 2003-12-10 | Региональный общественный фонд содействия защите интеллектуальной собственности | Alloy of aluminum-manganese system and product of this alloy |
| FR2855834A1 (en) * | 2003-06-06 | 2004-12-10 | Corus Aluminium Walzprod Gmbh | High strength aluminum alloy products with high fatigue resistance for use as the sheets and panels of aircraft structural components for the fuselage and wings |
-
2011
- 2011-04-05 RU RU2011112952/02A patent/RU2447174C1/en active IP Right Revival
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2454509A1 (en) * | 2001-07-25 | 2003-02-06 | Showa Denko K.K. | Aluminum alloy excellent in machinability, and aluminum alloy material and method for production thereof |
| RU2218437C1 (en) * | 2002-06-26 | 2003-12-10 | Региональный общественный фонд содействия защите интеллектуальной собственности | Alloy of aluminum-manganese system and product of this alloy |
| FR2855834A1 (en) * | 2003-06-06 | 2004-12-10 | Corus Aluminium Walzprod Gmbh | High strength aluminum alloy products with high fatigue resistance for use as the sheets and panels of aircraft structural components for the fuselage and wings |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109112372A (en) * | 2018-10-17 | 2019-01-01 | 合肥月煌新型装饰材料有限公司 | A kind of high-strength abrasion-proof aluminum alloy materials and preparation method thereof |
| CN111020319A (en) * | 2019-12-02 | 2020-04-17 | 南昌航空大学 | A special wire for additive manufacturing of high-strength aluminum-copper alloy and its preparation method and application |
| CN111020319B (en) * | 2019-12-02 | 2021-10-08 | 南昌航空大学 | A special wire for additive manufacturing of high-strength aluminum-copper alloy and its preparation method and application |
| CN117701960A (en) * | 2023-12-18 | 2024-03-15 | 中南大学 | A high-elongation cast Al-Cu-Zn-Mg alloy with good thermal crack resistance and its preparation method |
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