CN105316522A - Copper-nickel alloy convenient to produce for casting processing - Google Patents
Copper-nickel alloy convenient to produce for casting processing Download PDFInfo
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- CN105316522A CN105316522A CN201510871668.8A CN201510871668A CN105316522A CN 105316522 A CN105316522 A CN 105316522A CN 201510871668 A CN201510871668 A CN 201510871668A CN 105316522 A CN105316522 A CN 105316522A
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Abstract
The invention discloses a copper-nickel alloy convenient to produce for casting processing. The copper-nickel alloy consists of the following nine components in parts by weight: 101-105 parts of copper, 25-29 parts of manganese, 7-10 parts of nickel, 4-7 parts of cobalt, 13-16 parts of aluminum, 8-11 parts of tin, 5-8 parts of antimony, 10-13 parts of tantalum, and 12-15 parts of molybdenum. The copper-nickel alloy consists of the following nine components of the copper, the manganese, the nickel, the cobalt, the aluminum, the tin, the antimony, the tantalum and the molybdenum, and has the characteristics of being high in strength, high in hardness, good in abrasion resistance, good in corrosion resistance, good in high temperature resistance, and long in service life.
Description
Technical field
The present invention relates to alloy field, be specifically related to a kind of casting processing White brass alloy being convenient to produce.
Background technology
In recent years, Chinese Foundry equipment industry achieves swift and violent development, moulding equipment, coremaking equipment, sand preparing machine, cast equipment etc. all achieve significant progress in product performance, reliability, level of automation etc., and progressively stride forward to Green foundry direction.
The component material of the various product used in prior art is carrying out often occurring flaw because of various situation in process of manufacture, and the intensity of cast material and performance can not get ensureing, cause product to be easily worn, not corrosion-resistant, work-ing life is short.
Summary of the invention
The object of the present invention is to provide a kind of copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth that adopt to be grouped into, have that intensity is high, hardness is large, wear-resistant, solidity to corrosion good, the casting processing White brass alloy being convenient to produce of the feature of high temperature resistant, long service life.
Technical scheme of the present invention is, a kind of casting processing White brass alloy being convenient to produce, the described casting processing White brass alloy being convenient to produce is grouped into by copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be respectively: described copper accounts for 101-105 part, described manganese accounts for 25-29 part, described nickel accounts for 7-10 part, described cobalt accounts for 4-7 part, described aluminium accounts for 13-16 part, described tin accounts for 8-11 part, described antimony accounts for 5-8 part, and described tantalum accounts for 10-13 part, and described molybdenum accounts for 12-15 part.
In a preferred embodiment of the present invention, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 102 parts, described manganese accounts for 26 parts, described nickel accounts for 8 parts, and described cobalt accounts for 5 parts, and described aluminium accounts for 14 parts, described tin accounts for 9 parts, described antimony accounts for 6 parts, and described tantalum accounts for 11 parts, and described molybdenum accounts for 13 parts.
In a preferred embodiment of the present invention, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 104 parts, described manganese accounts for 28 parts, described nickel accounts for 9 parts, and described cobalt accounts for 6 parts, and described aluminium accounts for 15 parts, described tin accounts for 10 parts, described antimony accounts for 7 parts, and described tantalum accounts for 12 parts, and described molybdenum accounts for 14 parts.
Of the present invention is a kind of casting processing White brass alloy being convenient to produce, the present invention adopts copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth to be grouped into, and has that intensity is high, hardness is large, wear-resistant, solidity to corrosion good, a feature of high temperature resistant, long service life.
Embodiment
Below preferred embodiment of the present invention is described in detail, can be easier to make advantages and features of the invention be readily appreciated by one skilled in the art, thus more explicit defining is made to protection scope of the present invention.
Of the present invention is a kind of casting processing White brass alloy being convenient to produce, the described casting processing White brass alloy being convenient to produce is grouped into by copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be respectively: described copper accounts for 101-105 part, described manganese accounts for 25-29 part, described nickel accounts for 7-10 part, described cobalt accounts for 4-7 part, described aluminium accounts for 13-16 part, described tin accounts for 8-11 part, described antimony accounts for 5-8 part, described tantalum accounts for 10-13 part, and described molybdenum accounts for 12-15 part.
Further, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 102 parts, described manganese accounts for 26 parts, described nickel accounts for 8 parts, and described cobalt accounts for 5 parts, and described aluminium accounts for 14 parts, described tin accounts for 9 parts, described antimony accounts for 6 parts, and described tantalum accounts for 11 parts, and described molybdenum accounts for 13 parts.
Further, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 104 parts, described manganese accounts for 28 parts, described nickel accounts for 9 parts, and described cobalt accounts for 6 parts, and described aluminium accounts for 15 parts, described tin accounts for 10 parts, described antimony accounts for 7 parts, and described tantalum accounts for 12 parts, and described molybdenum accounts for 14 parts.
Carry out proportioning by each composition Different Weight per-cent, the functional alloy property height obtained is differed.
Of the present invention is a kind of casting processing White brass alloy being convenient to produce, the present invention adopts copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth to be grouped into, and has that intensity is high, hardness is large, wear-resistant, solidity to corrosion good, a feature of high temperature resistant, 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 are in the technical scope disclosed by the present invention; the change can expected without creative work or replacement, all should be encompassed within protection scope of the present invention.Therefore, the protection domain that protection scope of the present invention should limit with claims is as the criterion.
Claims (3)
1. be convenient to the casting processing White brass alloy of production for one kind, it is characterized in that: described in be convenient to produce casting processing White brass alloy be grouped into by copper, manganese, nickel, cobalt, aluminium, tin, antimony, tantalum and molybdenum nine kinds of one-tenth, describedly be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be respectively: described copper accounts for 101-105 part, described manganese accounts for 25-29 part, described nickel accounts for 7-10 part, described cobalt accounts for 4-7 part, described aluminium accounts for 13-16 part, described tin accounts for 8-11 part, described antimony accounts for 5-8 part, described tantalum accounts for 10-13 part, and described molybdenum accounts for 12-15 part.
2. the casting processing White brass alloy being convenient to produce according to claim 1, it is characterized in that: described in be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 102 parts, described manganese accounts for 26 parts, described nickel accounts for 8 parts, and described cobalt accounts for 5 parts, and described aluminium accounts for 14 parts, described tin accounts for 9 parts, described antimony accounts for 6 parts, and described tantalum accounts for 11 parts, and described molybdenum accounts for 13 parts.
3. the casting processing White brass alloy being convenient to produce according to claim 1, it is characterized in that: described in be convenient to parts by weight shared by each composition in the casting processing White brass alloy produced and be specially: described copper accounts for 104 parts, described manganese accounts for 28 parts, described nickel accounts for 9 parts, and described cobalt accounts for 6 parts, and described aluminium accounts for 15 parts, described tin accounts for 10 parts, described antimony accounts for 7 parts, and described tantalum accounts for 12 parts, and described molybdenum accounts for 14 parts.
Priority Applications (1)
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CN201510871668.8A CN105316522A (en) | 2015-12-02 | 2015-12-02 | Copper-nickel alloy convenient to produce for casting processing |
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CN201510871668.8A CN105316522A (en) | 2015-12-02 | 2015-12-02 | Copper-nickel alloy convenient to produce for casting processing |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61143543A (en) * | 1984-12-13 | 1986-07-01 | Kawasaki Steel Corp | Copper alloy for antisticking of marine life |
JPH0525568A (en) * | 1991-07-22 | 1993-02-02 | Furukawa Electric Co Ltd:The | Easy-to-work high strength copper alloy and its production |
JPH05156390A (en) * | 1991-12-09 | 1993-06-22 | Furukawa Electric Co Ltd:The | Ultra high-strength fine wire and its manufacture |
US6531003B2 (en) * | 1998-02-26 | 2003-03-11 | Mitsui Mining & Smelting Co., Ltd. | Abrasion resistant copper alloy, copper alloy powder for build-up cladding, and engine cylinder head |
JP2009052097A (en) * | 2007-08-28 | 2009-03-12 | Keiichi Araki | Damping member |
CN103122423A (en) * | 2011-11-19 | 2013-05-29 | 大连得达科技发展有限公司 | Alloy material |
-
2015
- 2015-12-02 CN CN201510871668.8A patent/CN105316522A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61143543A (en) * | 1984-12-13 | 1986-07-01 | Kawasaki Steel Corp | Copper alloy for antisticking of marine life |
JPH0525568A (en) * | 1991-07-22 | 1993-02-02 | Furukawa Electric Co Ltd:The | Easy-to-work high strength copper alloy and its production |
JPH05156390A (en) * | 1991-12-09 | 1993-06-22 | Furukawa Electric Co Ltd:The | Ultra high-strength fine wire and its manufacture |
US6531003B2 (en) * | 1998-02-26 | 2003-03-11 | Mitsui Mining & Smelting Co., Ltd. | Abrasion resistant copper alloy, copper alloy powder for build-up cladding, and engine cylinder head |
JP2009052097A (en) * | 2007-08-28 | 2009-03-12 | Keiichi Araki | Damping member |
CN103122423A (en) * | 2011-11-19 | 2013-05-29 | 大连得达科技发展有限公司 | Alloy material |
Non-Patent Citations (3)
Title |
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史文等: "《金属材料及热处理》", 28 February 2011, 上海科学技术出版社 * |
李庆峰等: "《金属材料与成型工艺基础》", 28 February 2012, 冶金工业出版社 * |
李英亮等: "《紧固件概论》", 31 January 2014, 国防工业出版社 * |
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