CN104911406A - Nickel-chromium die alloy - Google Patents
Nickel-chromium die alloy Download PDFInfo
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- CN104911406A CN104911406A CN201410094680.8A CN201410094680A CN104911406A CN 104911406 A CN104911406 A CN 104911406A CN 201410094680 A CN201410094680 A CN 201410094680A CN 104911406 A CN104911406 A CN 104911406A
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- nickel
- chromium
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Abstract
The invention relates to a nickel-chromium die alloy, which comprises the following components by weight part: 0.05-0.12 parts of sodium, 0.5-1 part of carbon, 20-30 parts of chromium, 40-45 parts of nickel, 10-15 parts of aluminum, 0.05-0.09 parts of grape straw, 0.1-0.35 parts of potassium, 0.2-0.56 parts of titanium and 0.8-1.25 parts of phosphor. The nickel-chromium die alloy has the advantages that a plurality of metal elements is combined, alloy intensity and wear resistance are greatly increased, stability is increased, and enterprise requirement can be satisfied.
Description
Technical field
The present invention relates to a kind of nickel chromium triangle mould alloy.
Background technology
Along with the development of science and technology, the increasing extent of mould application is extensive, for manufacturing the product mold of multi items, short run or frequent updating remodeling as the moulds such as injection mould, blow die, compression mould, require to have that the manufacturing cycle is short, manufacture difficulty is little and the feature that cost is low, and the punching block die manufacturing cost usually adopted in prior art is high, the cycle is long, the advantage of lower cost of nichrome material, is therefore used widely in this type of mould applications of manufacture.But simple metal can not meet the requirement as aspects such as plasticity, hardness, intensity, therefore usually adds alloying element to improve its physical and mechanical properties.
Therefore, for solving the problem, spy provides a kind of new technical scheme.
Summary of the invention
The invention provides a kind of nickel chromium triangle mould alloy.
The technical solution used in the present invention is:
A kind of nickel chromium triangle mould alloy, comprises the composition of following weight part:
Sodium 0.05-0.12 part;
Carbon 0.5-1 part;
Chromium 20-30 part;
Nickel 40-45 part;
Aluminium 10-15 part;
Grape stalk 0.05-0.09 part;
Potassium 0.1-0.35 part;
Titanium 0.2-0.56 part;
Phosphorus 0.8-1.25 part.
Advantage of the present invention is: the combination of Determination of multiple metal elements, greatly increases intensity and the wear resistance of alloy, improves stability simultaneously, meet the demand of enterprise.
Embodiment
In order to deepen the understanding of the present invention, below in conjunction with embodiment, the invention will be further described, and this embodiment only for explaining the present invention, does not form limiting the scope of the present invention.
Embodiment 1
A kind of nickel chromium triangle mould alloy, comprises the composition of following weight part:
0.05 part, sodium;
0.5 part, carbon;
Chromium 20 parts;
40 parts, nickel;
10 parts, aluminium;
Grape stalk 0.05 part;
0.1 part, potassium;
Titanium 0.2 part;
0.8 part, phosphorus.
Embodiment 2
A kind of nickel chromium triangle mould alloy, comprises the composition of following weight part:
0.1 part, sodium;
0.8 part, carbon;
Chromium 25 parts;
42 parts, nickel;
12 parts, aluminium;
Grape stalk 0.065 part;
0.25 part, potassium;
Titanium 0.34 part;
1 part, phosphorus.
Embodiment 3
A kind of nickel chromium triangle mould alloy, comprises the composition of following weight part:
0.12 part, sodium;
1 part, carbon;
Chromium 30 parts;
45 parts, nickel;
15 parts, aluminium;
Grape stalk 0.09 part;
0.35 part, potassium;
Titanium 0.56 part;
1.25 parts, phosphorus.
Advantage of the present invention is: the combination of Determination of multiple metal elements, greatly increases intensity and the wear resistance of alloy, improves stability simultaneously, meet the demand of enterprise.
The above is only preferred embodiment of the present invention, is not restriction the present invention being made to any other form, and any amendment done according to technical spirit of the present invention or equivalent variations, still belong to the present invention's scope required for protection.
Claims (1)
1. a nickel chromium triangle mould alloy, is characterized in that: the composition comprising following weight part:
Sodium 0.05-0.12 part;
Carbon 0.5-1 part;
Chromium 20-30 part;
Nickel 40-45 part;
Aluminium 10-15 part;
Grape stalk 0.05-0.09 part;
Potassium 0.1-0.35 part;
Titanium 0.2-0.56 part;
Phosphorus 0.8-1.25 part.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410094680.8A CN104911406A (en) | 2014-03-15 | 2014-03-15 | Nickel-chromium die alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410094680.8A CN104911406A (en) | 2014-03-15 | 2014-03-15 | Nickel-chromium die alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
CN104911406A true CN104911406A (en) | 2015-09-16 |
Family
ID=54080845
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410094680.8A Pending CN104911406A (en) | 2014-03-15 | 2014-03-15 | Nickel-chromium die alloy |
Country Status (1)
Country | Link |
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CN (1) | CN104911406A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070102075A1 (en) * | 2005-11-07 | 2007-05-10 | Huntington Alloys Corporation | High strength corrosion resistant alloy for oil patch application |
CN1978685A (en) * | 2005-12-09 | 2007-06-13 | 中国科学院兰州化学物理研究所 | Nickel-aluminium-chronium alloy and its preparing method |
CN102876953A (en) * | 2012-09-27 | 2013-01-16 | 无锡宏昌五金制造有限公司 | High-temperature nickel-chromium alloy |
CN103276248A (en) * | 2013-05-06 | 2013-09-04 | 无锡山发精铸科技有限公司 | High-temperature alloy for inblock cast worm gear |
-
2014
- 2014-03-15 CN CN201410094680.8A patent/CN104911406A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070102075A1 (en) * | 2005-11-07 | 2007-05-10 | Huntington Alloys Corporation | High strength corrosion resistant alloy for oil patch application |
CN1978685A (en) * | 2005-12-09 | 2007-06-13 | 中国科学院兰州化学物理研究所 | Nickel-aluminium-chronium alloy and its preparing method |
CN102876953A (en) * | 2012-09-27 | 2013-01-16 | 无锡宏昌五金制造有限公司 | High-temperature nickel-chromium alloy |
CN103276248A (en) * | 2013-05-06 | 2013-09-04 | 无锡山发精铸科技有限公司 | High-temperature alloy for inblock cast worm gear |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150916 |
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WD01 | Invention patent application deemed withdrawn after publication |