CN106367658A - High-toughness non-ferrous casting - Google Patents
High-toughness non-ferrous casting Download PDFInfo
- Publication number
- CN106367658A CN106367658A CN201611067300.7A CN201611067300A CN106367658A CN 106367658 A CN106367658 A CN 106367658A CN 201611067300 A CN201611067300 A CN 201611067300A CN 106367658 A CN106367658 A CN 106367658A
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- CN
- China
- Prior art keywords
- accounts
- parts
- zirconium
- tellurium
- indium
- Prior art date
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
-
- 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
- C22C21/003—Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
-
- 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
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/04—Alloys containing less than 50% by weight of each constituent containing tin or lead
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
The invention discloses a high-toughness non-ferrous casting. The high-toughness non-ferrous casting comprises a casting body which is of an integrated structure. The casting body comprises, by weight, 40-45 parts of aluminum, 21-26 parts of copper, 7-11 parts of nickel, 4-8 parts of tin, 6-9 parts of cobalt, 3-6 parts of zirconium, 2-5 parts of zirconium, 1-4 parts of indium and 2-4 parts of tellurium. The high-toughness non-ferrous casting is made of multiple components and thus has the advantages of being good in toughness, good in tear resistance, stable in product performance, good in corrosion resistance and long in service life.
Description
Technical field
The present invention relates to a kind of high-ductility non-ferrous casting.
Background technology
In recent years, Chinese Foundry equipment industry achieved swift and violent development, various metallic articles used in prior art
Often there is also a lot of problems, such as in order to reduce when often only being produced single absolute construction when producing, but using
Cost, to be completed using metal ingredient inexpensively to make, but finished product is of low quality, and to be completed using expensive metal
Make, then the cost of finished product too high it is impossible to promote on a large scale, lead to the scope of application to substantially reduce.
Content of the invention
It is an object of the invention to provide a kind of be obtained using Multiple components, have that good toughness, tear resistance be good, product
Can stable, the high-ductility non-ferrous casting of good corrosion resistance, long service life.
The technical scheme is that, a kind of high-ductility non-ferrous casting, including foundry goods body, described foundry goods body is one
Body formula structure, is made up of aluminum, copper, nickel, stannum, cobalt, zirconium, gallium, indium and tellurium, and parts by weight shared by each composition are respectively as follows: described aluminum
Account for 40-45 part, described copper accounts for 21-26 part, described nickel accounts for 7-11 part, described stannum accounts for 4-8 part, described cobalt accounts for 6-9 part, described zirconium accounts for
3-6 part, described gallium accounts for 2-5 part, and described indium accounts for 1-4 part, and described tellurium accounts for 2-4 part.
In a preferred embodiment of the present invention, the parts by weight shared by each composition of described foundry goods body are particularly as follows: described
Aluminum accounts for 41 parts, and described copper accounts for 22 parts, and described nickel accounts for 8 parts, and described stannum accounts for 5 parts, and described cobalt accounts for 7 parts, and described zirconium accounts for 4 parts, described gallium
Account for 3 parts, described indium accounts for 2 parts, and described tellurium accounts for 3 parts.
In a preferred embodiment of the present invention, the parts by weight shared by each composition of described foundry goods body are particularly as follows: described
Aluminum accounts for 44 parts, and described copper accounts for 25 parts, and described nickel accounts for 10 parts, and described stannum accounts for 7 parts, and described cobalt accounts for 8 parts, and described zirconium accounts for 5 parts, described gallium
Account for 4 parts, described indium accounts for 3 parts, and described tellurium accounts for 4 parts.
Of the present invention the present invention adopts Multiple components to be obtained for a kind of high-ductility non-ferrous casting, has good toughness, anti-
Lancinating is good, properties of product are stable, good corrosion resistance, long service life.
Specific embodiment
Below presently preferred embodiments of the present invention is described in detail so that advantages and features of the invention can be easier to by
It will be appreciated by those skilled in the art that apparent clearly defining thus making to protection scope of the present invention.
Of the present invention for a kind of high-ductility non-ferrous casting, including foundry goods body, described foundry goods body is integral type knot
Structure, is made up of aluminum, copper, nickel, stannum, cobalt, zirconium, gallium, indium and tellurium, and parts by weight shared by each composition are respectively as follows: described aluminum and account for 40-45
Part, described copper accounts for 21-26 part, and described nickel accounts for 7-11 part, and described stannum accounts for 4-8 part, and described cobalt accounts for 6-9 part, and described zirconium accounts for 3-6 part,
Described gallium accounts for 2-5 part, and described indium accounts for 1-4 part, and described tellurium accounts for 2-4 part.
Further, particularly as follows: described aluminum accounts for 41 parts, described copper accounts for the parts by weight shared by each composition of described foundry goods body
22 parts, described nickel accounts for 8 parts, and described stannum accounts for 5 parts, and described cobalt accounts for 7 parts, and described zirconium accounts for 4 parts, and described gallium accounts for 3 parts, and described indium accounts for 2 parts,
Described tellurium accounts for 3 parts.
Further, particularly as follows: described aluminum accounts for 44 parts, described copper accounts for the parts by weight shared by each composition of described foundry goods body
25 parts, described nickel accounts for 10 parts, and described stannum accounts for 7 parts, and described cobalt accounts for 8 parts, and described zirconium accounts for 5 parts, and described gallium accounts for 4 parts, and described indium accounts for 3
Part, described tellurium accounts for 4 parts.
Proportioning is carried out so that the properties of product height obtaining differs by each composition Different Weight percentage ratio.
Of the present invention the present invention adopts Multiple components to be obtained for a kind of high-ductility non-ferrous casting, has good toughness, anti-
Lancinating is good, properties of product are stable, good corrosion resistance, long service life.
The foregoing is only the specific embodiment of the present invention, but protection scope of the present invention is not limited thereto, any
Those of ordinary skill in the art disclosed herein technical scope in, the change that can expect without creative work or
Replace, all should be included within the scope of the present invention.Therefore, protection scope of the present invention should be limited with claims
Fixed protection domain is defined.
Claims (3)
1. a kind of high-ductility non-ferrous casting, including foundry goods body it is characterised in that: described foundry goods body be integral type structure,
It is made up of aluminum, copper, nickel, stannum, cobalt, zirconium, gallium, indium and tellurium, parts by weight shared by each composition are respectively as follows: described aluminum and account for 40-45 part,
Described copper accounts for 21-26 part, and described nickel accounts for 7-11 part, and described stannum accounts for 4-8 part, and described cobalt accounts for 6-9 part, and described zirconium accounts for 3-6 part, described
Gallium accounts for 2-5 part, and described indium accounts for 1-4 part, and described tellurium accounts for 2-4 part.
2. high-ductility non-ferrous casting according to claim 1 it is characterised in that: shared by each composition of described foundry goods body
Particularly as follows: described aluminum accounts for 41 parts, described copper accounts for 22 parts to parts by weight, and described nickel accounts for 8 parts, and described stannum accounts for 5 parts, and described cobalt accounts for 7 parts,
Described zirconium accounts for 4 parts, and described gallium accounts for 3 parts, and described indium accounts for 2 parts, and described tellurium accounts for 3 parts.
3. high-ductility non-ferrous casting according to claim 1 it is characterised in that: shared by each composition of described foundry goods body
Particularly as follows: described aluminum accounts for 44 parts, described copper accounts for 25 parts to parts by weight, and described nickel accounts for 10 parts, and described stannum accounts for 7 parts, and described cobalt accounts for 8
Part, described zirconium accounts for 5 parts, and described gallium accounts for 4 parts, and described indium accounts for 3 parts, and described tellurium accounts for 4 parts.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201611067300.7A CN106367658A (en) | 2016-11-29 | 2016-11-29 | High-toughness non-ferrous casting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201611067300.7A CN106367658A (en) | 2016-11-29 | 2016-11-29 | High-toughness non-ferrous casting |
Publications (1)
Publication Number | Publication Date |
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CN106367658A true CN106367658A (en) | 2017-02-01 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201611067300.7A Pending CN106367658A (en) | 2016-11-29 | 2016-11-29 | High-toughness non-ferrous casting |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH09143599A (en) * | 1995-11-15 | 1997-06-03 | Mitsubishi Heavy Ind Ltd | Titanium-aluminum intermetallic compound base alloy |
CN102851554A (en) * | 2012-09-18 | 2013-01-02 | 褚介平 | Aluminum casting high in elongation and tensile strength |
CN102969113A (en) * | 2012-11-20 | 2013-03-13 | 无锡常安通用金属制品有限公司 | Hard magnetic alloy and preparation thereof |
CN105568114A (en) * | 2015-12-24 | 2016-05-11 | 芜湖恒耀汽车零部件有限公司 | Copper-aluminum alloy material used for automobile exhaust pipe and preparation method of copper-aluminum alloy material |
CN105648282A (en) * | 2016-02-26 | 2016-06-08 | 江西德义半导体科技有限公司 | Gallium-aluminum alloy and preparation method thereof |
-
2016
- 2016-11-29 CN CN201611067300.7A patent/CN106367658A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH09143599A (en) * | 1995-11-15 | 1997-06-03 | Mitsubishi Heavy Ind Ltd | Titanium-aluminum intermetallic compound base alloy |
CN102851554A (en) * | 2012-09-18 | 2013-01-02 | 褚介平 | Aluminum casting high in elongation and tensile strength |
CN102969113A (en) * | 2012-11-20 | 2013-03-13 | 无锡常安通用金属制品有限公司 | Hard magnetic alloy and preparation thereof |
CN105568114A (en) * | 2015-12-24 | 2016-05-11 | 芜湖恒耀汽车零部件有限公司 | Copper-aluminum alloy material used for automobile exhaust pipe and preparation method of copper-aluminum alloy material |
CN105648282A (en) * | 2016-02-26 | 2016-06-08 | 江西德义半导体科技有限公司 | Gallium-aluminum alloy and preparation method thereof |
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PB01 | Publication | ||
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RJ01 | Rejection of invention patent application after publication | ||
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Application publication date: 20170201 |