CN105039825A - Preparation method of high-temperature alloy - Google Patents
Preparation method of high-temperature alloy Download PDFInfo
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- CN105039825A CN105039825A CN201510546102.8A CN201510546102A CN105039825A CN 105039825 A CN105039825 A CN 105039825A CN 201510546102 A CN201510546102 A CN 201510546102A CN 105039825 A CN105039825 A CN 105039825A
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Abstract
The invention relates to a preparation method of a high-temperature alloy. The preparation method is characterized in that the high-temperature alloy comprises the following components in parts by mass: 3-10 parts of C, 10-15 parts of Si, 3-10 parts of Mn, 2-4 parts of S, 2-4 parts of P, 6-10 parts of Fe, 10-20 parts of Cu, 3-6 parts of Ti, 2-4 parts of Mo and 20-40 parts of Mg. The high-temperature alloy is relatively high in wearing resistance, meets the requirements of special industries, and has a wider application range.
Description
Technical field
The present invention relates to a kind of alloy preparation method, particularly a kind of high temperature alloy preparation method.
Background technology
Alloy is the material with metallic character synthesized by two or more metal and metal or the certain method of nonmetal warp.Generally obtain by fusing into uniform liquid and solidify.According to the number of component, binary alloy, ternary alloy and multicomponent alloy can be divided into.Due to the character of alloy excellence, be widely used in industries such as industry, chemical industry, aviation, iron and steel, along with expanding economy, the requirement of alloy is more and more higher, there is the problems such as abrasive wear resistance is inadequate, non-refractory in alloy in the market, therefore, a kind of new scheme of exigence solves this technical problem.
Summary of the invention
The present invention is just for the technical problem existed in prior art, and provide a kind of high temperature alloy preparation method, this Wear Resistance is higher, and good flame resistance, meet the needs of special industry, range of application is more extensive.
To achieve these goals, technical scheme of the present invention is as follows: a kind of high temperature alloy preparation method, is characterized in that, described high temperature alloy is as follows according to mass fraction proportioning: C:3-10 part, Si:10-15 part, Mn:3-10 part, S:2-4 part, P:2-4 part, Fe:6-10 part: Cu:10-20 part, Ti:3-6 part, Mo:2-4 part, Mg:20-40 part.
A kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:3 part, Si:10 part, Mn:3 part, S:2 part, P:2 part, Fe:6 part: Cu:10 part, Ti:3 part, Mo:2 part, Mg:20 part.
A kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:10 part, Si:15 part, Mn:10 part, S:4 part, P:4 part, Fe:10 part: Cu:20 part, Ti:6 part, Mo:4 part, Mg:40 part.
A kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:6 part, Si:12 part, Mn:6 part, S:3 part, P:3 part, Fe:8 part: Cu:15 part, Ti:5 part, Mo:3 part, Mg:30 part.
Relative to prior art, advantage of the present invention is as follows: 1) technical solution of the present invention design is ingenious, and cost is lower, is convenient to apply on a large scale; 2) this high temperature alloy intensity is high, and wear resistance is good, good stability, and good flame resistance.
Embodiment
In order to strengthen, to understanding of the present invention and understanding, introducing further the present invention below in conjunction with embodiment.
embodiment 1:a kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:3 part, Si:10 part, Mn:3 part, S:2 part, P:2 part, Fe:6 part: Cu:10 part, Ti:3 part, Mo:2 part, Mg:20 part.
embodiment 2:a kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:10 part, Si:15 part, Mn:10 part, S:4 part, P:4 part, Fe:10 part: Cu:20 part, Ti:6 part, Mo:4 part, Mg:40 part.
embodiment 3:a kind of high temperature alloy preparation method, described high temperature alloy is as follows according to mass fraction proportioning: C:6 part, Si:12 part, Mn:6 part, S:3 part, P:3 part, Fe:8 part: Cu:15 part, Ti:5 part, Mo:3 part, Mg:30 part.
It should be noted that above-described embodiment, be not used for limiting protection scope of the present invention, equivalents done on the basis of technique scheme or the alternative scope all falling into the claims in the present invention and protect.
Claims (4)
1. a high temperature alloy preparation method, it is characterized in that, described high temperature alloy is as follows according to mass fraction proportioning: C:3-10 part, Si:10-15 part, Mn:3-10 part, S:2-4 part, P:2-4 part, Fe:6-10 part: Cu:10-20 part, Ti:3-6 part, Mo:2-4 part, Mg:20-40 part.
2. high temperature alloy preparation method according to claim 1, is characterized in that, described high temperature alloy is as follows according to mass fraction proportioning: C:3 part, Si:10 part, Mn:3 part, S:2 part, P:2 part, Fe:6 part: Cu:10 part, Ti:3 part, Mo:2 part, Mg:20 part.
3. high temperature alloy preparation method according to claim 1, is characterized in that, described high temperature alloy is as follows according to mass fraction proportioning: C:10 part, Si:15 part, Mn:10 part, S:4 part, P:4 part, Fe:10 part: Cu:20 part, Ti:6 part, Mo:4 part, Mg:40 part.
4. high temperature alloy preparation method according to claim 1, is characterized in that, described high temperature alloy is as follows according to mass fraction proportioning: C:6 part, Si:12 part, Mn:6 part, S:3 part, P:3 part, Fe:8 part: Cu:15 part, Ti:5 part, Mo:3 part, Mg:30 part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510546102.8A CN105039825A (en) | 2015-08-31 | 2015-08-31 | Preparation method of high-temperature alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510546102.8A CN105039825A (en) | 2015-08-31 | 2015-08-31 | Preparation method of high-temperature alloy |
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| CN105039825A true CN105039825A (en) | 2015-11-11 |
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| CN201510546102.8A Pending CN105039825A (en) | 2015-08-31 | 2015-08-31 | Preparation method of high-temperature alloy |
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Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103343271A (en) * | 2013-07-08 | 2013-10-09 | 中南大学 | Light and pressure-proof fast-decomposed cast magnesium alloy |
| CN103397233A (en) * | 2013-07-01 | 2013-11-20 | 安徽三联泵业股份有限公司 | Magnesium alloy hot-working die steel and preparation method thereof |
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2015
- 2015-08-31 CN CN201510546102.8A patent/CN105039825A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103397233A (en) * | 2013-07-01 | 2013-11-20 | 安徽三联泵业股份有限公司 | Magnesium alloy hot-working die steel and preparation method thereof |
| CN103343271A (en) * | 2013-07-08 | 2013-10-09 | 中南大学 | Light and pressure-proof fast-decomposed cast magnesium alloy |
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Application publication date: 20151111 |
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| RJ01 | Rejection of invention patent application after publication |