CN104044311A - High-plasticity hot galvanizing alloy material - Google Patents
High-plasticity hot galvanizing alloy material Download PDFInfo
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- CN104044311A CN104044311A CN201410265674.4A CN201410265674A CN104044311A CN 104044311 A CN104044311 A CN 104044311A CN 201410265674 A CN201410265674 A CN 201410265674A CN 104044311 A CN104044311 A CN 104044311A
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Abstract
The invention relates to a high-plasticity hot galvanizing alloy material which comprises a hot galvanizing underlying metal, a stellite layer, a permalloy layer and a half-metal material layer, wherein the stellite layer, the permalloy layer and the half-metal material layer are sequentially arranged on the surface of the hot galvanizing underlying metal; the stellite layer is a cobalt-chromium-tungsten alloy, the permalloy layer is an iron-nickel alloy, the half-metal material layer is perovskite, the cobalt-chromium-tungsten alloy accounts for 26-35 percent of the weight of an alloy material main body, the iron-nickel alloy accounts for 18-40 percent of the weight of the alloy material main body, and the perovskite accounts for 36-55 percent of the weight of the alloy material main body. The high-plasticity hot galvanizing alloy material provided by the invention is better in thermoplasticity, and has the advantages of lowering the production cost of a metal material, increasing the economic benefit and improving the product quality.
Description
Technical field
The present invention relates to a kind of metal material, be specifically related to a kind of high-ductility hot-dip galvanized alloy material.
Background technology
Alloy material is a kind of mixture.In a lot of fields, all bring into play very large effect, replaced a lot of traditional materials.Alloy material is divided into metal and metal alloy compositions, nonmetal and metal alloy compositions, nonmetal and non-metal alloy material by its composition.With common single wild phase alloy material ratio, its impact strength, fatigue strength and fracture toughness significantly improve, and have special hot expansibility.Be divided into that interlaminar hybrid, interlayer mix, sandwich mixes, in layer/interlayer mixes and surpasses and mix alloy material.Alloy material sixties, for meeting the needs of the sophisticated technology material therefors such as Aero-Space, successively research and production take the alloy material that high-performance fiber is reinforcing material.In order to distinguish with first generation galss fiber reinforced resin alloy material, this alloy material is called to Advanced Alloy Material.Advanced Alloy Material, except as structural material, also can be used as functional material, but existing alloy material thermoplastic property is poor.
Summary of the invention
For the problems referred to above, main purpose of the present invention is to provide the high-ductility hot-dip galvanized alloy material that a kind of thermoplastic property is good.
The present invention is achieved by the following technical solutions: a kind of high-ductility hot-dip galvanized alloy material is provided, described alloy material comprises: galvanizing underlying metal, and be provided with successively stellite layer on described galvanizing underlying metal surface, permalloy layer and semi-metallic layer, described stellite layer is cobalt-chromium-tungsten alloy, described permalloy layer is iron-nickel alloy, described semi-metallic layer is perovskite, described cobalt-chromium-tungsten alloy accounts for the 26%-35% of alloy material body weight, described iron-nickel alloy accounts for the 18%-40% of alloy material body weight, described perovskite accounts for the 36%-55% of alloy material body weight.
Preferably, described cobalt-chromium-tungsten alloy accounts for 30% of alloy material body weight, and described iron-nickel alloy accounts for 40% of alloy material body weight, and described perovskite accounts for 40% of alloy material body weight.
Preferably, the thickness of described stellite layer is 0.6mm.
Preferably, described perovskite comprises sodium, cerium zinc or niobium.
Preferably, on described semi-metallic layer, be also provided with memory alloy layer.
Preferably, described in, having memory alloy layer is copper gold kirsite.
Preferably, described copper gold kirsite accounts for 8% of alloy material body weight.
Preferably, the thickness of described memory alloy layer is 0.5 micron.
A kind of high-ductility hot-dip galvanized alloy material of the present invention, thermoplastic property is good, reduces the production cost of metal material simultaneously, increases economic efficiency, and improves product quality.
The specific embodiment
For making the object, technical solutions and advantages of the present invention clearer, those skilled in the art can understand other advantages of the present invention and effect easily by the disclosed content of this description.The present invention can also be implemented or be applied by the other different specific embodiment, and the every details in this description also can be based on different viewpoints and application, carries out various modifications or change not deviating under spirit of the present invention.
The invention provides a kind of high-ductility hot-dip galvanized alloy material, described alloy material comprises: galvanizing underlying metal, and be provided with successively stellite layer on described galvanizing underlying metal surface, permalloy layer and semi-metallic layer, described stellite layer is cobalt-chromium-tungsten alloy, described permalloy layer is iron-nickel alloy, described semi-metallic layer is perovskite, described cobalt-chromium-tungsten alloy accounts for the 26%-35% of alloy material body weight, described iron-nickel alloy accounts for the 18%-40% of alloy material body weight, described perovskite accounts for the 36%-55% of alloy material body weight.
In the present embodiment, described cobalt-chromium-tungsten alloy accounts for 30% of alloy material body weight, and described iron-nickel alloy accounts for 40% of alloy material body weight, and described perovskite accounts for 40% of alloy material body weight.
Wherein, the thickness of described stellite layer is 0.6mm.Described perovskite comprises sodium, cerium zinc or niobium.
In addition, on described semi-metallic layer, be also provided with memory alloy layer.It is described that to have memory alloy layer be copper gold kirsite.Described copper gold kirsite accounts for 8% of alloy material body weight.The thickness of described memory alloy layer is 0.5 micron.
A kind of high-ductility hot-dip galvanized alloy material of the present invention, thermoplastic property is good, reduces the production cost of metal material simultaneously, increases economic efficiency, and improves product quality.
Above-mentioned explanation illustrates and has described some preferred embodiments of the present invention, but as previously mentioned, be to be understood that the present invention is not limited to disclosed form herein, should not regard the eliminating to other embodiment as, and can be used for various other combinations, modification and environment, and can, in invention contemplated scope described herein, by technology or the knowledge of above-mentioned instruction or association area, change.And the change that those skilled in the art carry out and variation do not depart from the spirit and scope of the present invention, all should be in the protection domain of claims of the present invention.
Claims (8)
1. a high-ductility hot-dip galvanized alloy material, it is characterized in that, described alloy material comprises: galvanizing underlying metal, and be provided with successively stellite layer on described galvanizing underlying metal surface, permalloy layer and semi-metallic layer, described stellite layer is cobalt-chromium-tungsten alloy, described permalloy layer is iron-nickel alloy, described semi-metallic layer is perovskite, described cobalt-chromium-tungsten alloy accounts for the 26%-35% of alloy material body weight, described iron-nickel alloy accounts for the 18%-40% of alloy material body weight, described perovskite accounts for the 36%-55% of alloy material body weight.
2. high-ductility hot-dip galvanized alloy material according to claim 1, it is characterized in that, described cobalt-chromium-tungsten alloy accounts for 30% of alloy material body weight, and described iron-nickel alloy accounts for 40% of alloy material body weight, and described perovskite accounts for 40% of alloy material body weight.
3. high-ductility hot-dip galvanized alloy material according to claim 1, is characterized in that, the thickness of described stellite layer is 0.6mm.
4. high-ductility hot-dip galvanized alloy material according to claim 1, is characterized in that, described perovskite comprises sodium, cerium zinc or niobium.
5. high-ductility hot-dip galvanized alloy material according to claim 1, is characterized in that, on described semi-metallic layer, is also provided with memory alloy layer.
6. high-ductility hot-dip galvanized alloy material according to claim 5, is characterized in that, described in to have memory alloy layer be copper gold kirsite.
7. high-ductility hot-dip galvanized alloy material according to claim 5, is characterized in that, described copper gold kirsite accounts for 8% of alloy material body weight.
8. high-ductility hot-dip galvanized alloy material according to claim 5, is characterized in that, the thickness of described memory alloy layer is 0.5 micron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201410265674.4A CN104044311A (en) | 2014-06-13 | 2014-06-13 | High-plasticity hot galvanizing alloy material |
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| CN201410265674.4A CN104044311A (en) | 2014-06-13 | 2014-06-13 | High-plasticity hot galvanizing alloy material |
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| CN104044311A true CN104044311A (en) | 2014-09-17 |
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| CN201410265674.4A Pending CN104044311A (en) | 2014-06-13 | 2014-06-13 | High-plasticity hot galvanizing alloy material |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107225821A (en) * | 2017-06-21 | 2017-10-03 | 华北理工大学 | A kind of composite material with high stability |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107225821A (en) * | 2017-06-21 | 2017-10-03 | 华北理工大学 | A kind of composite material with high stability |
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Application publication date: 20140917 |