CN105543572A - Wear-resisting aluminum alloy material - Google Patents
Wear-resisting aluminum alloy material Download PDFInfo
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- CN105543572A CN105543572A CN201510951320.XA CN201510951320A CN105543572A CN 105543572 A CN105543572 A CN 105543572A CN 201510951320 A CN201510951320 A CN 201510951320A CN 105543572 A CN105543572 A CN 105543572A
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- Prior art keywords
- wear
- aluminum alloy
- alloy material
- aluminium alloy
- magnesium
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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
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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
- C22C21/02—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
- 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
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
The invention discloses a wear-resisting aluminum alloy material. The wear-resisting aluminum alloy material is characterized by consisting of the following main elements in percentage by weight: 0.2-0.5% of carbon, 0.4-0.8% of silicon, 0.3-0.7% of magnesium, 0.05-0.10% of nickel, 0.10-0.30% of iron, 0.06-0.11% of manganese, 0.4-0.7% of molybdenum, 0.03-0.07% of boron, 0.02-0.06% of copper and the balance of Al; the wear-resisting aluminum alloy material is formed by mixing the raw material components, melting the raw material components, refining the raw material components, pressing the raw material components into blank, and sintering the blank at a high temperature. The wear-resisting aluminum alloy material disclosed by the invention uses simple materials, and is low in preparation cost; a certain proportion of metal elements such as magnesium, nickel, iron, manganese and the like are added, so that the wear resistance of the aluminum alloy is increased while the hardness of the aluminum alloy is guaranteed, and the surface brightness of the aluminum alloy is not affected, and therefore, the wear-resisting aluminum alloy material is suitable for being used in all industries.
Description
Technical field
The invention belongs to a kind of alloy material, particularly a kind of wear-resistant aluminium alloy material.
Background technology
At present along with industrial expansion, the application of alloy widely, because aluminium alloy density is little, erosion resistance is stronger relative to ordinary steel, therefore the application of aluminium alloy widely, and aluminium alloy density is low, but strength ratio is higher, close to or exceed high-quality steel, plasticity is good, can be processed into various section bar, has excellent electroconductibility, thermal conductivity and corrosion stability, industrially widely use, usage quantity is only second to steel.Aluminium alloy can be divided into Behaviors of Deformed Aluminum Alloys and the large class of cast aluminium alloy two by working method: wrought aluminium alloy can bear press working.The aluminium alloy material of various form, specification can be processed into.Mainly for the manufacture of air material, door and window for building etc.Behaviors of Deformed Aluminum Alloys is divided into again not heat-treatable strengthened type aluminium alloy and heat-treatable strengthened type aluminium alloy.Not heat-treatable strengthened type does not improve mechanical property by thermal treatment, and can only realize strengthening by cold deformation, it mainly comprises rafifinal, industrial rafifinal, commercial-purity aluminium and corrosion-resisting aluminium etc.Heat-treatable strengthened type aluminium alloy can improve mechanical property by heat treatment such as quenching and timeliness, and it can be divided into duralumin, wrought aluminium, ultralumin and particular aluminum alloy etc.Cast aluminium alloy according to chemical composition can be divided into aluminum silicon alloy, aluminum-copper alloy, aluminum magnesium alloy, aluminium-zinc alloy and Al rare earth alloy, and wherein aluminum silicon alloy has again hyper eutectic silicon aluminium alloy, Eutectic Silicon in Al-Si Cast Alloys aluminium alloy, and single Eutectic Silicon in Al-Si Cast Alloys aluminium alloy, cast aluminium alloy uses under as cast condition.Some aluminium alloys can adopt thermal treatment to obtain good mechanical property, physicals and corrosion resistance.
Aluminum alloy materials is in the market varied.But for some occasions, such as door and window, cable etc., people have been not content with practicality for the requirement of this kind of aluminium alloy and density is light, due to long use, the wearing and tearing of aluminium alloy can be caused, therefore produce a kind of wear-resistant aluminum alloy supply market, extremely urgent.
Summary of the invention
The technical problem to be solved in the present invention is for the deficiencies in the prior art, proposes a kind of wear-resistant aluminium alloy material.
The technical problem to be solved in the present invention is achieved through the following technical solutions, and a kind of wear-resistant aluminium alloy material, is characterized in, its principal element and weight percent are:
Carbon: 0.2-0.5%;
Silicon: 0.4-0.8%;
Magnesium: 0.3-0.7%;
Nickel: 0.05-0.10%;
Iron: 0.10-0.30%;
Manganese: 0.06-0.11%;
Molybdenum: 0.4-0.7%;
Boron: 0.03-0.07%;
Copper: 0.02-0.06%;
Surplus is Al;
Described wear-resistant aluminium alloy material by above-mentioned each feed composition through mixing, melting, refining, be pressed into base and high fever and sinter and form.
In wear-resistant aluminium alloy material of the present invention, preferred technical scheme feature is further:
1, described wear-resistant aluminium alloy material also comprises titanium: 0.02-0.044%;
2, its principal element and weight percent are:
Carbon: 0.3-0.5%;
Silicon: 0.6-0.8%;
Magnesium: 0.5-0.7%;
Nickel: 0.08-0.10%;
Iron: 0.20-0.30%;
Manganese: 0.08-0.11%;
Molybdenum: 0.5-0.7%;
Boron: 0.05-0.07%;
Copper: 0.04-0.06%;
Titanium: 0.03-0.044%
Surplus is Al;
3, its principal element and weight percent are:
Carbon: 0.5%;
Silicon: 0.7%;
Magnesium: 0.6%;
Nickel: 0.09%;
Iron: 0.25%;
Manganese: 0.10%;
Molybdenum: 0.6%;
Boron: 0.06%;
Copper: 0.05%;
Titanium: 0.04%
Surplus is Al.
Compared with prior art, materials of the present invention are simple, cost of manufacture is cheap, add the rub proofness that the metallic elements such as a certain proportion of magnesium, nickel, iron, manganese too increase aluminium alloy while ensure that the hardness of aluminium alloy simultaneously, do not affect the surface brightness of aluminium alloy, be applicable to every profession and trade and use.
Embodiment
Below further describe concrete technical scheme of the present invention, so that those skilled in the art understands the present invention further, and do not form the restriction of its power.
Embodiment 1, a kind of wear-resistant aluminium alloy material, is characterized in, its principal element and weight percent are:
Carbon: 0.2-0.5%;
Silicon: 0.4-0.8%;
Magnesium: 0.3-0.7%;
Nickel: 0.05-0.10%;
Iron: 0.10-0.30%;
Manganese: 0.06-0.11%;
Molybdenum: 0.4-0.7%;
Boron: 0.03-0.07%;
Copper: 0.02-0.06%;
Surplus is Al;
Described wear-resistant aluminium alloy material by above-mentioned each feed composition through mixing, melting, refining, be pressed into base and high fever and sinter and form.
Embodiment 2, the wear-resistant aluminium alloy material according to embodiment 1, described wear-resistant aluminium alloy material also comprises titanium: 0.02-0.044%.
Embodiment 3, the wear-resistant aluminium alloy material according to embodiment 1 or 2, its principal element and weight percent are:
Carbon: 0.3-0.5%;
Silicon: 0.6-0.8%;
Magnesium: 0.5-0.7%;
Nickel: 0.08-0.10%;
Iron: 0.20-0.30%;
Manganese: 0.08-0.11%;
Molybdenum: 0.5-0.7%;
Boron: 0.05-0.07%;
Copper: 0.04-0.06%;
Titanium: 0.03-0.044%
Surplus is Al.
Embodiment 4, the wear-resistant aluminium alloy material according to embodiment 1,2 or 3, its principal element and weight percent are:
Carbon: 0.5%;
Silicon: 0.7%;
Magnesium: 0.6%;
Nickel: 0.09%;
Iron: 0.25%;
Manganese: 0.10%;
Molybdenum: 0.6%;
Boron: 0.06%;
Copper: 0.05%;
Titanium: 0.04%
Surplus is Al.
Claims (4)
1. a wear-resistant aluminium alloy material, is characterized in that, its principal element and weight percent are:
Carbon: 0.2-0.5%;
Silicon: 0.4-0.8%;
Magnesium: 0.3-0.7%;
Nickel: 0.05-0.10%;
Iron: 0.10-0.30%;
Manganese: 0.06-0.11%;
Molybdenum: 0.4-0.7%;
Boron: 0.03-0.07%;
Copper: 0.02-0.06%;
Surplus is Al;
Described wear-resistant aluminium alloy material by above-mentioned each feed composition through mixing, melting, refining, be pressed into base and high fever and sinter and form.
2. wear-resistant aluminium alloy material according to claim 1, is characterized in that: described wear-resistant aluminium alloy material also comprises titanium: 0.02-0.044%.
3. wear-resistant aluminium alloy material according to claim 1, is characterized in that, its principal element and weight percent are:
Carbon: 0.3-0.5%;
Silicon: 0.6-0.8%;
Magnesium: 0.5-0.7%;
Nickel: 0.08-0.10%;
Iron: 0.20-0.30%;
Manganese: 0.08-0.11%;
Molybdenum: 0.5-0.7%;
Boron: 0.05-0.07%;
Copper: 0.04-0.06%;
Titanium: 0.03-0.044%
Surplus is Al.
4. a kind of Lightweight Radiation Protective alloy material according to claim 1, is characterized in that, its principal element and weight percent are:
Carbon: 0.5%;
Silicon: 0.7%;
Magnesium: 0.6%;
Nickel: 0.09%;
Iron: 0.25%;
Manganese: 0.10%;
Molybdenum: 0.6%;
Boron: 0.06%;
Copper: 0.05%;
Titanium: 0.04%
Surplus is Al.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510951320.XA CN105543572A (en) | 2015-12-19 | 2015-12-19 | Wear-resisting aluminum alloy material |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510951320.XA CN105543572A (en) | 2015-12-19 | 2015-12-19 | Wear-resisting aluminum alloy material |
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| CN105543572A true CN105543572A (en) | 2016-05-04 |
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| CN201510951320.XA Pending CN105543572A (en) | 2015-12-19 | 2015-12-19 | Wear-resisting aluminum alloy material |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106011565A (en) * | 2016-07-14 | 2016-10-12 | 安徽恒兴装饰工程有限公司 | Novel aluminum alloy material and production process thereof |
| CN106086534A (en) * | 2016-06-30 | 2016-11-09 | 国网山东省电力公司电力科学研究院 | A kind of aluminum carbon copper alloy earthing material of high-strength corrosion-resisting |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104467642A (en) * | 2014-12-23 | 2015-03-25 | 常熟高嘉能源科技有限公司 | Corrosion-resistant solar assembly frame |
| CN104789820A (en) * | 2015-03-23 | 2015-07-22 | 苏州市神龙门窗有限公司 | Abrasion-proof aluminum alloy material containing earth elements and treatment process of abrasion-proof aluminum alloy material |
-
2015
- 2015-12-19 CN CN201510951320.XA patent/CN105543572A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104467642A (en) * | 2014-12-23 | 2015-03-25 | 常熟高嘉能源科技有限公司 | Corrosion-resistant solar assembly frame |
| CN104789820A (en) * | 2015-03-23 | 2015-07-22 | 苏州市神龙门窗有限公司 | Abrasion-proof aluminum alloy material containing earth elements and treatment process of abrasion-proof aluminum alloy material |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106086534A (en) * | 2016-06-30 | 2016-11-09 | 国网山东省电力公司电力科学研究院 | A kind of aluminum carbon copper alloy earthing material of high-strength corrosion-resisting |
| CN106011565A (en) * | 2016-07-14 | 2016-10-12 | 安徽恒兴装饰工程有限公司 | Novel aluminum alloy material and production process thereof |
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Application publication date: 20160504 |