CN108913966A - A kind of aluminum alloy materials - Google Patents
A kind of aluminum alloy materials Download PDFInfo
- Publication number
- CN108913966A CN108913966A CN201810282188.1A CN201810282188A CN108913966A CN 108913966 A CN108913966 A CN 108913966A CN 201810282188 A CN201810282188 A CN 201810282188A CN 108913966 A CN108913966 A CN 108913966A
- Authority
- CN
- China
- Prior art keywords
- aluminum alloy
- alloy materials
- aluminium
- manganese
- copper
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- 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
- C22C21/12—Alloys based on aluminium with copper 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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/14—Alloys based on aluminium with copper 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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
Abstract
The invention discloses a kind of aluminum alloy materials, are related to field of alloy preparation technology.Including：10%~15% copper；0.15%~0.3% manganese；Surplus is aluminium.
Description
Technical field
The present invention relates to field of alloy preparation technology, more particularly relate to a kind of aluminum alloy materials.
Background technique
Aluminium alloy is that the alloy of one or more alloying element compositions is then added using aluminium as matrix element.Aluminium alloy
Density is low, but intensity is relatively high, and there is excellent electric conductivity, thermal conductivity and corrosion stability etc., so that aluminum alloy materials are in electricity
Lixing industry has obtained relatively broad application.
The features such as high strength alumin ium alloy has intensity high, and plasticity is good, and solderability is good and fine corrosion resistance, is answered extensively
It is many dual-use at present for the various structural members and the high high stress welding structural element of other intensity requirements of aircraft
Indispensable important feature material in aircraft, transport facility.
As space flight and aviation technology develops increasingly raising to material requirements, it is higher that researcher is just putting forth effort mining inetesity,
The high-strength weldable aluminum alloy of high comprehensive performance is at present the comprehensive performance of the high strength alumin ium alloy of raising welding, mainly
While pursuing material high intensity, reduce since intensity is improved to anti-stress corrosion performance, fracture toughness and fatigue strength etc.
Cause adverse effect.
Summary of the invention
The embodiment of the present invention provides a kind of aluminum alloy materials, which has high-intensitive and corrosion resistance.
The embodiment of the present invention provides a kind of aluminum alloy materials, mainly includes：
10%~15% copper；
0.15%~0.3% manganese；Surplus is aluminium.
Preferably, further include：
0~0.2% silicon.
Preferably, further include：
0~0.2% iron.
Preferably, further include：
0~0.15% titanium.
Preferably, further include：
0~0.15% chromium.
Preferably, further include：
0~0.3% zinc.
It preferably, further include any one following combination：
0~0.2% silicon, 0~0.2% iron, 0~0.15% titanium, 0~0.15% chromium, 0~0.3% zinc.
In the embodiment of the present invention, a kind of aluminum alloy materials are provided, mainly include 10%~15% copper；0.15%~
0.3% manganese.In above-mentioned aluminum alloy materials, by being added to copper into aluminum alloy materials, to be effectively increased aluminium alloy
The intensity of material improves the ductility of aluminum alloy materials；Further, due to increasing manganese material, aluminium alloy production is improved
The surface quality and surface treatment properties of product.
Specific embodiment
The following is a clear and complete description of the technical scheme in the embodiments of the invention, it is clear that described embodiment
Only a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, the common skill in this field
Art personnel every other embodiment obtained without making creative work belongs to the model that the present invention protects
It encloses.
Embodiment 1
A kind of aluminum alloy materials, the raw material comprising following components：
12% copper, 0.15% manganese, remaining material are aluminium.
Embodiment 2
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.18% manganese, 0.04% silicon, remaining material are aluminium.
Embodiment 3
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.2% manganese, 0.16% iron, remaining material are aluminium.
Embodiment 4
A kind of aluminum alloy materials, the raw material comprising following components：
14% copper, 0.18% manganese, 0.08% titanium, remaining material are aluminium.
Embodiment 5
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.18% manganese, 0.06% chromium, remaining material are aluminium.
Embodiment 6
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.2% manganese, 0.1% zinc, remaining material are aluminium.
Embodiment 7
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.2% manganese, 0.06% silicon, 0.16% iron, remaining material are aluminium.
Embodiment 8
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.2% manganese, 0.16% silicon, 0.08% titanium, remaining material are aluminium.
Embodiment 9
A kind of aluminum alloy materials, the raw material comprising following components：
14% copper, 0.18% manganese, 0.04% silicon, 0.06% chromium, remaining material are aluminium.
Embodiment 10
15% copper, 0.15% manganese, 0.04% silicon, 0.1% zinc, remaining material are aluminium.
Embodiment 11
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.15% manganese, 0.16% iron, 0.1% titanium, remaining material are aluminium.
Embodiment 12
14% copper, 0.2% manganese, 0.14% iron, 0.08% chromium, remaining material are aluminium.
Embodiment 13
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.18% manganese, 0.14% iron, 0.08% zinc, remaining material are aluminium.
Embodiment 14
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.15% manganese, 0.06% titanium, 0.06% chromium, remaining material are aluminium.
Embodiment 15
A kind of aluminum alloy materials, the raw material comprising following components：
14% copper, 0.2% manganese, 0.1% titanium, 0.1% zinc, remaining material are aluminium.
Embodiment 16
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.15% manganese, 0.1% chromium, 0.05% zinc, remaining material are aluminium.
Embodiment 17
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.15% manganese, 0.05% silicon, 0.16 iron, 0.11% titanium, remaining material are aluminium.
Embodiment 18
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.16% manganese, 0.06 silicon, 0.15% iron, 0.01% chromium, remaining material are aluminium.
Embodiment 19
A kind of aluminum alloy materials, the raw material comprising following components：
14% copper, 0.2% manganese, 0.04 silicon, 0.2% iron, 0.13% zinc, remaining material are aluminium.
Embodiment 20
A kind of aluminum alloy materials, the raw material comprising following components：
14% copper, 0.22% manganese, 0.04% iron, 0.12 titanium, 0.08% chromium, remaining material are aluminium.
Embodiment 21
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.18% manganese, 0.04% silicon, 0.06 titanium, 0.15 zinc, remaining material are aluminium.
Embodiment 22
A kind of aluminum alloy materials, the raw material comprising following components：
13% copper, 0.2% manganese, 0.04 silicon, 0.16% iron, 0.06% titanium, 0.08% chromium, remaining material
Material is aluminium.
Embodiment 23
A kind of aluminum alloy materials, the raw material comprising following components：
12% copper, 0.2% manganese, 0.06% silicon, 0.18% iron, 0.06% titanium, 0.08% zinc, remaining
Material is aluminium.
Embodiment 24
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.21% manganese, 0.04% silicon, 0.16% iron, 0.06% titanium, 0.1% zinc, remaining
Material is aluminium.
Embodiment 25
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.19% manganese, 0.06% silicon, 0.08% titanium, 0.1% chromium, 0.08% zinc, remaining
Material is aluminium.
Embodiment 26
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.16% manganese, 0.16% iron, 0.08% titanium, 0.1% chromium, 0.06% zinc, remaining
Material is aluminium.
Embodiment 27
A kind of aluminum alloy materials, the raw material comprising following components：
15% copper, 0.15% manganese, 0.04% silicon, 0.16% iron, 0.06% titanium, 0.08% chromium,
0.08% zinc, remaining material are aluminium.
It mainly include 10%~15% copper in conclusion providing a kind of aluminum alloy materials in the embodiment of the present invention；
0.15%~0.3% manganese.In above-mentioned aluminum alloy materials, by being added to copper into aluminum alloy materials, to effectively increase
The intensity of aluminum alloy materials, improves the ductility of aluminum alloy materials；Further, it due to increasing manganese material, improves
The surface quality and surface treatment properties of alloy product.
Although preferred embodiments of the present invention have been described, it is created once a person skilled in the art knows basic
Property concept, then additional changes and modifications may be made to these embodiments.So it includes excellent that the following claims are intended to be interpreted as
It selects embodiment and falls into all change and modification of the scope of the invention.
Obviously, various changes and modifications can be made to the invention without departing from essence of the invention by those skilled in the art
Mind and range.In this way, if these modifications and changes of the present invention belongs to the range of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to include these modifications and variations.
Claims (7)
1. a kind of aluminum alloy materials, which is characterized in that including：
10%~15% copper；
0.15%~0.3% manganese；
Surplus is aluminium.
2. aluminum alloy materials as described in claim 1, which is characterized in that further include：
0~0.2% silicon.
3. aluminum alloy materials as described in claim 1, which is characterized in that further include：
0~0.2% iron.
4. aluminum alloy materials as described in claim 1, which is characterized in that further include：
0~0.15% titanium.
5. aluminum alloy materials as described in claim 1, which is characterized in that further include：
0~0.15% chromium.
6. aluminum alloy materials as described in claim 1, which is characterized in that further include：
0~0.3% zinc.
7. aluminum alloy materials as described in claim 1, which is characterized in that further include any one or more following combination：
0~0.2% silicon, 0~0.2% iron, 0~0.15% titanium, 0~0.15% chromium, 0~0.3% zinc.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810282188.1A CN108913966A (en) | 2018-04-02 | 2018-04-02 | A kind of aluminum alloy materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810282188.1A CN108913966A (en) | 2018-04-02 | 2018-04-02 | A kind of aluminum alloy materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108913966A true CN108913966A (en) | 2018-11-30 |
Family
ID=64402811
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810282188.1A Pending CN108913966A (en) | 2018-04-02 | 2018-04-02 | A kind of aluminum alloy materials |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB733881A (en) * | 1952-02-27 | 1955-07-20 | Aluminum Co Of America | Improvements in or relating to aluminium base alloys |
| JPH04318145A (en) * | 1991-04-17 | 1992-11-09 | Kobe Steel Ltd | Al-mg superplasticity aluminum alloy sheet excellent in strength and corrosion resistance and its manufacture |
| CN1174895A (en) * | 1997-01-05 | 1998-03-04 | 吉林工业大学 | Aluminium-base electric power plant fly-ash compsite material and preparation method and device |
| CN101476412A (en) * | 2008-11-14 | 2009-07-08 | 张家港市华杨金属制品有限公司 | Aluminum alloy lock core |
| CN102586659A (en) * | 2011-01-06 | 2012-07-18 | 盐城生态之光照明科技有限公司 | High-efficient radiator material for high-power LED (light-emitting diode) lighting lamp |
| CN105018870A (en) * | 2014-04-24 | 2015-11-04 | 金生智 | LED (light-emitting diode) radiator material and manufacturing process thereof |
-
2018
- 2018-04-02 CN CN201810282188.1A patent/CN108913966A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB733881A (en) * | 1952-02-27 | 1955-07-20 | Aluminum Co Of America | Improvements in or relating to aluminium base alloys |
| JPH04318145A (en) * | 1991-04-17 | 1992-11-09 | Kobe Steel Ltd | Al-mg superplasticity aluminum alloy sheet excellent in strength and corrosion resistance and its manufacture |
| CN1174895A (en) * | 1997-01-05 | 1998-03-04 | 吉林工业大学 | Aluminium-base electric power plant fly-ash compsite material and preparation method and device |
| CN101476412A (en) * | 2008-11-14 | 2009-07-08 | 张家港市华杨金属制品有限公司 | Aluminum alloy lock core |
| CN102586659A (en) * | 2011-01-06 | 2012-07-18 | 盐城生态之光照明科技有限公司 | High-efficient radiator material for high-power LED (light-emitting diode) lighting lamp |
| CN105018870A (en) * | 2014-04-24 | 2015-11-04 | 金生智 | LED (light-emitting diode) radiator material and manufacturing process thereof |
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Application publication date: 20181130 |
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