CN106739268A - A kind of durable composite metal product of superhigh intensity - Google Patents
A kind of durable composite metal product of superhigh intensity Download PDFInfo
- Publication number
- CN106739268A CN106739268A CN201611041768.9A CN201611041768A CN106739268A CN 106739268 A CN106739268 A CN 106739268A CN 201611041768 A CN201611041768 A CN 201611041768A CN 106739268 A CN106739268 A CN 106739268A
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- CN
- China
- Prior art keywords
- parts
- accounts
- zinc
- aluminium
- magnesium
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/016—Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of aluminium or aluminium alloys
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- 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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- 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
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/752—Corrosion inhibitor
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Abstract
Present invention is disclosed a kind of durable composite metal product of superhigh intensity, including top layer the first metal layer and the second metal layer of internal layer, the first metal layer is made up of aluminium, zinc, copper, magnesium and antimony, and parts by weight shared by each composition are respectively:The aluminium accounts for 45 49 parts, and the zinc accounts for 10 14 parts, and the copper accounts for 8 12 parts, and the magnesium accounts for 6 10 parts, and the antimony accounts for 25 parts, and the second metal layer is made up of aluminium, zinc, copper, magnesium and zirconium, and parts by weight shared by each composition are respectively:The aluminium accounts for 55 60 parts, and the zinc accounts for 12 15 parts, and the copper accounts for 9 13 parts, and the magnesium accounts for 7 12 parts, and the zirconium accounts for 58 parts.The present invention using composite construction set, with layer difference sense, intensity is high, fracture toughness is strong, corrosion resistance is strong the characteristics of.
Description
Technical field
The present invention relates to a kind of durable composite metal product of superhigh intensity.
Background technology
Steel Wire Products Industry includes structured metal product manufacture, metal tools manufacture, container and packaging container of metal
Manufacture, stainless steel and similar daily metallic article manufacture etc..With the progress and the development of science and technology of society, metallic article is in work
The utilization of the various fields of recent life of industry, agricultural and people is more and more extensive, also to the value that social creativity is increasing.It is existing
The various metallic articles used in technology often only produce single absolute construction when being produced, but are often also deposited when using
In many problems, often Performance comparision is single when such as homogenous material is used, it is impossible to reach the expected using effect of enterprise instantly,
Cannot promote the use of on a large scale.
The content of the invention
Set using composite construction it is an object of the invention to provide one kind, with the sense of layer difference, intensity is high, fracture toughness
The durable composite metal product of superhigh intensity of the characteristics of by force, corrosion resistance is strong.
The technical scheme is that, a kind of durable composite metal product of superhigh intensity, including top layer the first metal layer
With the second metal layer of internal layer, the first metal layer is made up of aluminium, zinc, copper, magnesium and antimony, parts by weight shared by each composition point
It is not:The aluminium accounts for 45-49 parts, and the zinc accounts for 10-14 parts, and the copper accounts for 8-12 parts, and the magnesium accounts for 6-10 parts, and the antimony accounts for 2-
5 parts, the second metal layer is made up of aluminium, zinc, copper, magnesium and zirconium, and parts by weight shared by each composition are respectively:The aluminium is accounted for
55-60 parts, the zinc accounts for 12-15 parts, and the copper accounts for 9-13 parts, and the magnesium accounts for 7-12 parts, and the zirconium accounts for 5-8 parts.
In a preferred embodiment of the present invention, parts by weight shared by each composition of the first metal layer are specially:It is described
Aluminium accounts for 46 parts, and the zinc accounts for 11 parts, and the copper accounts for 9 parts, and the magnesium accounts for 7 parts, and the antimony accounts for 3 parts, the second metal layer it is each into
Parts by weight shared by point are specially:The aluminium accounts for 56 parts, and the zinc accounts for 13 parts, and the copper accounts for 10 parts, and the magnesium accounts for 8 parts, described
Zirconium accounts for 6 parts.
In a preferred embodiment of the present invention, parts by weight shared by each composition of the first metal layer are specially:It is described
Aluminium accounts for 48 parts, and the zinc accounts for 13 parts, and the copper accounts for 11 parts, and the magnesium accounts for 9 parts, and the antimony accounts for 4 parts, the second metal layer it is each into
Parts by weight shared by point are specially:The aluminium accounts for 59 parts, and the zinc accounts for 14 parts, and the copper accounts for 12 parts, and the magnesium accounts for 11 parts, described
Zirconium accounts for 7 parts.
Of the present invention is a kind of durable composite metal product of superhigh intensity, and the present invention is set using composite construction, has
The characteristics of layer difference is felt, intensity is high, fracture toughness is strong, corrosion resistance is strong.
Specific embodiment
Presently preferred embodiments of the present invention is described in detail below 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 being defined so as to be made to protection scope of the present invention.
Of the present invention be a kind of durable composite metal product of superhigh intensity, including top layer the first metal layer and internal layer
Second metal layer, the first metal layer is made up of aluminium, zinc, copper, magnesium and antimony, and parts by weight shared by each composition are respectively:Institute
State aluminium and account for 45-49 parts, the zinc accounts for 10-14 parts, and the copper accounts for 8-12 parts, and the magnesium accounts for 6-10 parts, and the antimony accounts for 2-5 parts, institute
State second metal layer to be made up of aluminium, zinc, copper, magnesium and zirconium, parts by weight shared by each composition are respectively:The aluminium accounts for 55-60 parts,
The zinc accounts for 12-15 parts, and the copper accounts for 9-13 parts, and the magnesium accounts for 7-12 parts, and the zirconium accounts for 5-8 parts.
Further, parts by weight shared by each composition of the first metal layer are specially:The aluminium accounts for 46 parts, and the zinc is accounted for
11 parts, the copper accounts for 9 parts, and the magnesium accounts for 7 parts, and the antimony accounts for 3 parts, and parts by weight shared by each composition of second metal layer are specific
For:The aluminium accounts for 56 parts, and the zinc accounts for 13 parts, and the copper accounts for 10 parts, and the magnesium accounts for 8 parts, and the zirconium accounts for 6 parts.
Further, parts by weight shared by each composition of the first metal layer are specially:The aluminium accounts for 48 parts, and the zinc is accounted for
13 parts, the copper accounts for 11 parts, and the magnesium accounts for 9 parts, and the antimony accounts for 4 parts, parts by weight tool shared by each composition of second metal layer
Body is:The aluminium accounts for 59 parts, and the zinc accounts for 14 parts, and the copper accounts for 12 parts, and the magnesium accounts for 11 parts, and the zirconium accounts for 7 parts.
Matched by each composition Different Weight percentage so that the properties of product height for obtaining differs.
Of the present invention is a kind of durable composite metal product of superhigh intensity, and the present invention is set using composite construction, has
The characteristics of layer difference is felt, intensity is high, fracture toughness is strong, corrosion resistance is strong.
Specific embodiment of the invention is the foregoing is only, but protection scope of the present invention is not limited thereto, it is any
Those of ordinary skill in the art disclosed herein technical scope in, the change that can expect without creative work or
Replace, should all 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 the first metal layer of the durable composite metal product of superhigh intensity, including top layer and the second metal layer of internal layer, its
It is characterised by:The first metal layer is made up of aluminium, zinc, copper, magnesium and antimony, and parts by weight shared by each composition are respectively:It is described
Aluminium accounts for 45-49 parts, and the zinc accounts for 10-14 parts, and the copper accounts for 8-12 parts, and the magnesium accounts for 6-10 parts, and the antimony accounts for 2-5 parts, described
Second metal layer is made up of aluminium, zinc, copper, magnesium and zirconium, and parts by weight shared by each composition are respectively:The aluminium accounts for 55-60 parts, institute
State zinc and account for 12-15 parts, the copper accounts for 9-13 parts, and the magnesium accounts for 7-12 parts, and the zirconium accounts for 5-8 parts.
2. the durable composite metal product of superhigh intensity according to claim 1, it is characterised in that:The first metal layer is each
Parts by weight are specially shared by composition:The aluminium accounts for 46 parts, and the zinc accounts for 11 parts, and the copper accounts for 9 parts, and the magnesium accounts for 7 parts, described
Antimony accounts for 3 parts, and parts by weight shared by each composition of second metal layer are specially:The aluminium accounts for 56 parts, and the zinc accounts for 13 parts, described
Copper accounts for 10 parts, and the magnesium accounts for 8 parts, and the zirconium accounts for 6 parts.
3. the durable composite metal product of superhigh intensity according to claim 1, it is characterised in that:The first metal layer is each
Parts by weight are specially shared by composition:The aluminium accounts for 48 parts, and the zinc accounts for 13 parts, and the copper accounts for 11 parts, and the magnesium accounts for 9 parts, institute
State antimony and account for 4 parts, parts by weight shared by each composition of second metal layer are specially:The aluminium accounts for 59 parts, and the zinc accounts for 14 parts, institute
State copper and account for 12 parts, the magnesium accounts for 11 parts, and the zirconium accounts for 7 parts.
Priority Applications (1)
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CN201611041768.9A CN106739268A (en) | 2016-11-24 | 2016-11-24 | A kind of durable composite metal product of superhigh intensity |
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CN201611041768.9A CN106739268A (en) | 2016-11-24 | 2016-11-24 | A kind of durable composite metal product of superhigh intensity |
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CN201611041768.9A Pending CN106739268A (en) | 2016-11-24 | 2016-11-24 | A kind of durable composite metal product of superhigh intensity |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002038230A (en) * | 2000-07-26 | 2002-02-06 | Daido Metal Co Ltd | Aluminum alloy for bearing |
JP2006257451A (en) * | 2005-03-15 | 2006-09-28 | Chokoon Zairyo Kenkyusho:Kk | Structure of oxidation-resistant coating formed on heat-resistant alloy and coating method |
US20070122648A1 (en) * | 2005-10-13 | 2007-05-31 | Corus Aluminium Walzprodukte Gmbh | Multi-layered brazing sheet |
CN106148772A (en) * | 2016-08-02 | 2016-11-23 | 王映朴 | Aluminium alloys for auto body plate |
-
2016
- 2016-11-24 CN CN201611041768.9A patent/CN106739268A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002038230A (en) * | 2000-07-26 | 2002-02-06 | Daido Metal Co Ltd | Aluminum alloy for bearing |
JP2006257451A (en) * | 2005-03-15 | 2006-09-28 | Chokoon Zairyo Kenkyusho:Kk | Structure of oxidation-resistant coating formed on heat-resistant alloy and coating method |
US20070122648A1 (en) * | 2005-10-13 | 2007-05-31 | Corus Aluminium Walzprodukte Gmbh | Multi-layered brazing sheet |
CN106148772A (en) * | 2016-08-02 | 2016-11-23 | 王映朴 | Aluminium alloys for auto body plate |
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