CN105568089A - Light-weight radiation-resistant alloy material - Google Patents
Light-weight radiation-resistant alloy material Download PDFInfo
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- CN105568089A CN105568089A CN201510951318.2A CN201510951318A CN105568089A CN 105568089 A CN105568089 A CN 105568089A CN 201510951318 A CN201510951318 A CN 201510951318A CN 105568089 A CN105568089 A CN 105568089A
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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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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Abstract
The invention relates to a light-weight radiation-resistant alloy material which is characterized by comprising the following materials in percentage by weight: 0.05-0.10% of Fe, 0.02-0.05% of Mn, 0.02-0.06% of Si, 0.02-0.05% of Sa, 2.1-3.1% of Cu, 2.5-3.5% of Mg, 0.01-0.015% of Cr, 6-8% of Zn, 0.07-0.10% of Ti, 0.010-0.20% of Zr, 0.10-0.25% of W and the balance of Al. The light-weight radiation-resistant alloy material has the advantages of simple materials and low manufacturing cost. The added rare-earth metal has the functions of resisting radiation and the like. The other metal elements are added to enhance the hardness of the aluminum alloy and ensure the quality of the aluminum alloy, so that the aluminum alloy has wider applicability.
Description
Technical field
The invention belongs to a kind of alloy material, particularly a kind of Lightweight Radiation Protective alloy material.
Background technology
This year develops rapidly along with industry, the purposes of alloy material is increasing, alloy material is of many uses, such as the partition of computer desk, for making cable, for the making of door and window, therefore, people get more and more for the requirement of aluminium alloy, go out outside the beautiful glossiness again of outward appearance, also need quality light, shipment for convenience detach etc., existing light aluminum alloy material often intensity and hardness lower, severe impact power and heavy burden can not be born, simultaneously for some places, aluminium alloy also needs to have radiation proof function, negative effect can be produced to human body for a long time under radiation environment, cause headache, insomnia, amnesia, elevation of blood pressure or decline, there is the symptoms such as circumscribed exception in heart, as long-term operation under the super-strength environment of electromagnetic radiation, the serious some of the staff that may cause miscarry, cataract, even bring out carcinogenic and transgenation etc., therefore, be badly in need of a kind of lightweight in the market, high rigidity and again can radiation-resistant aluminum alloy materials.
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 hard Lightweight Radiation Protective alloy material.
The technical problem to be solved in the present invention is achieved through the following technical solutions, a kind of Lightweight Radiation Protective alloy material, be characterized in, comprising weight ratio shared by each component of following material is: Fe:0.05-0.10, Mn:0.02-0.05, Si:0.02-0.06, Sa:0.02-0.05, Cu:2.1-3.1, Mg2.5-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.010-0.20, W:0.10-0.25, surplus is Al.
In a kind of excavator gear of the present invention alloy material, preferred technical scheme feature is further:
1, described Lightweight Radiation Protective alloy material also comprises Ce:2-4;
2, comprising weight ratio shared by each component of following material is: Fe:0.07-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:2.5-3.1, Mg3-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al;
3, comprising weight ratio shared by each component of following material is: Fe:0.08-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:3-3.1, Mg3-3.5, Cr:0.013-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al;
4, comprising weight ratio shared by each component of following material is: Fe:0.08, Mn:0.045, Si:0.05, Sa:0.04, Cu:3, Mg3.5, Cr:0.015, Zn:7, Ti:0.09, Zr:0.20, W:0.24, Ce:4 surplus is Al.
Compared with prior art, materials of the present invention are simple, and cost of manufacture is cheap, add rare earth metal, serve the effects such as radioprotective, add other metallic element simultaneously, ensure that the quality of aluminium alloy while adding the hardness of aluminium alloy, the application of the aluminium alloy being is more extensive.
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 Lightweight Radiation Protective alloy material, be characterized in, comprising weight ratio shared by each component of following material is: Fe:0.05-0.10, Mn:0.02-0.05, Si:0.02-0.06, Sa:0.02-0.05, Cu:2.1-3.1, Mg2.5-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.010-0.20, W:0.10-0.25, surplus is Al.
Embodiment 2, a kind of Lightweight Radiation Protective alloy material according to embodiment 1, described Lightweight Radiation Protective alloy material also comprises Ce:2-4.
Embodiment 3, a kind of Lightweight Radiation Protective alloy material according to embodiment 1 or 2, comprising weight ratio shared by each component of following material is: Fe:0.07-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:2.5-3.1, Mg3-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al.
Embodiment 4, a kind of Lightweight Radiation Protective alloy material according to embodiment 1,2 or 3, comprising weight ratio shared by each component of following material is: Fe:0.08-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:3-3.1, Mg3-3.5, Cr:0.013-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al.
Embodiment 5, a kind of Lightweight Radiation Protective alloy material according to embodiment 1,2,3 or 4, comprising weight ratio shared by each component of following material is: Fe:0.08, Mn:0.045, Si:0.05, Sa:0.04, Cu:3, Mg3.5, Cr:0.015, Zn:7, Ti:0.09, Zr:0.20, W:0.24, Ce:4 surplus is Al.
Claims (5)
1. a Lightweight Radiation Protective alloy material, it is characterized in that, comprising weight ratio shared by each component of following material is: Fe:0.05-0.10, Mn:0.02-0.05, Si:0.02-0.06, Sa:0.02-0.05, Cu:2.1-3.1, Mg2.5-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.010-0.20, W:0.10-0.25, surplus is Al.
2. Lightweight Radiation Protective alloy material according to claim 1, is characterized in that: described Lightweight Radiation Protective alloy material also comprises Ce:2-4.
3. a kind of Lightweight Radiation Protective alloy material according to claim 1, it is characterized in that, comprising weight ratio shared by each component of following material is: Fe:0.07-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:2.5-3.1, Mg3-3.5, Cr:0.01-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al.
4. a kind of Lightweight Radiation Protective alloy material according to claim 1, it is characterized in that, comprising weight ratio shared by each component of following material is: Fe:0.08-0.10, Mn:0.04-0.05, Si:0.04-0.06, Sa:0.03-0.05, Cu:3-3.1, Mg3-3.5, Cr:0.013-0.015, Zn:6-8Ti:0.07-0.10, Zr:0.10-0.20, W:0.20-0.25, Ce:3-4 surplus is Al.
5. a kind of Lightweight Radiation Protective alloy material according to claim 1, it is characterized in that, comprising weight ratio shared by each component of following material is: Fe:0.08, Mn:0.045, Si:0.05, Sa:0.04, Cu:3, Mg3.5, Cr:0.015, Zn:7, Ti:0.09, Zr:0.20, W:0.24, Ce:4 surplus is Al.
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CN201510951318.2A CN105568089A (en) | 2015-12-19 | 2015-12-19 | Light-weight radiation-resistant alloy material |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107955894A (en) * | 2017-12-13 | 2018-04-24 | 苏州浩焱精密模具有限公司 | A kind of mould high-strength aluminium-magnesium alloy material |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102431237A (en) * | 2010-09-21 | 2012-05-02 | 古河Sky株式会社 | High-strengh aluminum alloy brazing sheet and method of manufacture |
CN103233148A (en) * | 2012-08-23 | 2013-08-07 | 北京有色金属研究总院 | Aluminum alloy product suitable for structure and function integration, and preparation method thereof |
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Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102431237A (en) * | 2010-09-21 | 2012-05-02 | 古河Sky株式会社 | High-strengh aluminum alloy brazing sheet and method of manufacture |
US20120129003A1 (en) * | 2010-09-21 | 2012-05-24 | Furukawa-Sky Aluminum Corp. | High-strenght aluminum alloy brazing sheet and method of manufacture |
CN103233148A (en) * | 2012-08-23 | 2013-08-07 | 北京有色金属研究总院 | Aluminum alloy product suitable for structure and function integration, and preparation method thereof |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107955894A (en) * | 2017-12-13 | 2018-04-24 | 苏州浩焱精密模具有限公司 | A kind of mould high-strength aluminium-magnesium alloy material |
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