CN105695796A - White copper alloy for casting machining of materials - Google Patents

White copper alloy for casting machining of materials Download PDF

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Publication number
CN105695796A
CN105695796A CN201610245781.XA CN201610245781A CN105695796A CN 105695796 A CN105695796 A CN 105695796A CN 201610245781 A CN201610245781 A CN 201610245781A CN 105695796 A CN105695796 A CN 105695796A
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CN
China
Prior art keywords
parts
accounts
casting
rapidoprint
niobium
Prior art date
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.)
Pending
Application number
CN201610245781.XA
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Chinese (zh)
Inventor
顾云龙
王小平
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xiangcheng District Suzhou City Sensible Composite Material Factory
Original Assignee
Xiangcheng District Suzhou City Sensible Composite Material Factory
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xiangcheng District Suzhou City Sensible Composite Material Factory filed Critical Xiangcheng District Suzhou City Sensible Composite Material Factory
Priority to CN201610245781.XA priority Critical patent/CN105695796A/en
Publication of CN105695796A publication Critical patent/CN105695796A/en
Pending legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • C22C30/02Alloys containing less than 50% by weight of each constituent containing copper

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Continuous Casting (AREA)

Abstract

The invention discloses a white copper alloy for casting machining of materials. The white copper alloy is composed of nine components including copper, cobalt, nickel, iron, manganese, tungsten, niobium, indium and titanium. The white copper alloy for casting machining of the materials comprises, by weight, 95-100 parts of the copper, 18-22 parts of the cobalt, 23-26 parts of the nickel, 5-8 parts of the iron, 7-10 parts of the manganese, 9-12 parts of the tungsten, 4-7 parts of the niobium, 3-6 parts of the indium, and 11-14 parts of the titanium. The white copper alloy is composed of the nine components including the copper, the cobalt, the nickel, the iron, the manganese, the tungsten, the niobium, the indium and the titanium and has the beneficial effects of being high in strength, good in corrosion resistance, thermoelectricity and abrasion resistance and long in service life.

Description

A kind of casting rapidoprint White brass alloy
Technical field
The present invention relates to alloy field, be specifically related to a kind of casting rapidoprint White brass alloy。
Background technology
In recent years, Chinese Foundry equipment industry achieves swift and violent development, mo(u)lding equipment, coremaking equipment, sand preparing machine, casting equipment etc. all achieve significant progress in properties of product, reliability, automaticity etc., and progressively stride forward to Green foundry direction。
Often there is flaw because of various situations in carrying out process of manufacture in the parts material of the various product used in prior art, and the intensity of founding materials and performance can not get ensureing, causing that product is easily worn, not corrosion-resistant, service life is short。
Summary of the invention
It is an object of the invention to provide and a kind of adopt copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium to be grouped into, there is intensity height, corrosion resistance is good, pyroelectricity is good, wearability is good, the casting rapidoprint White brass alloy of the feature of long service life。
The technical scheme is that, a kind of casting rapidoprint White brass alloy, described casting rapidoprint White brass alloy is grouped into by copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium, in described casting rapidoprint White brass alloy, parts by weight shared by each composition are respectively as follows: described copper and account for 95-100 part, described cobalt accounts for 18-22 part, described nickel accounts for 23-26 part, described ferrum accounts for 5-8 part, described manganese accounts for 7-10 part, described tungsten accounts for 9-12 part, described niobium accounts for 4-7 part, and described indium accounts for 3-6 part, and described titanium accounts for 11-14 part。
In a preferred embodiment of the present invention, in described casting rapidoprint White brass alloy, parts by weight shared by each composition are particularly as follows: described copper accounts for 96 parts, described cobalt accounts for 19 parts, described nickel accounts for 24 parts, and described ferrum accounts for 6 parts, and described manganese accounts for 8 parts, described tungsten accounts for 10 parts, described niobium accounts for 5 parts, and described indium accounts for 4 parts, and described titanium accounts for 12 parts。
In a preferred embodiment of the present invention, in described casting rapidoprint White brass alloy, parts by weight shared by each composition are particularly as follows: described copper accounts for 99 parts, described cobalt accounts for 21 parts, described nickel accounts for 25 parts, and described ferrum accounts for 7 parts, and described manganese accounts for 9 parts, described tungsten accounts for 11 parts, described niobium accounts for 6 parts, and described indium accounts for 5 parts, and described titanium accounts for 13 parts。
Of the present invention is a kind of casting rapidoprint White brass alloy, and the present invention adopts copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium to be grouped into, and has intensity height, corrosion resistance is good, pyroelectricity is good, wearability is good, the feature of long service life。
Detailed description of the invention
Below presently preferred embodiments of the present invention is described in detail, so that advantages and features of the invention can be easier to be readily appreciated by one skilled in the art, thus protection scope of the present invention being made apparent clear and definite defining。
Of the present invention is a kind of casting rapidoprint White brass alloy, described casting rapidoprint White brass alloy is grouped into by copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium, in described casting rapidoprint White brass alloy, parts by weight shared by each composition are respectively as follows: described copper and account for 95-100 part, described cobalt accounts for 18-22 part, described nickel accounts for 23-26 part, described ferrum accounts for 5-8 part, described manganese accounts for 7-10 part, described tungsten accounts for 9-12 part, described niobium accounts for 4-7 part, described indium accounts for 3-6 part, and described titanium accounts for 11-14 part。
Further, in described casting rapidoprint White brass alloy, shared by each composition, parts by weight are particularly as follows: described copper accounts for 96 parts, and described cobalt accounts for 19 parts, and described nickel accounts for 24 parts, described ferrum accounts for 6 parts, and described manganese accounts for 8 parts, and described tungsten accounts for 10 parts, described niobium accounts for 5 parts, and described indium accounts for 4 parts, and described titanium accounts for 12 parts。
Further, in described casting rapidoprint White brass alloy, shared by each composition, parts by weight are particularly as follows: described copper accounts for 99 parts, and described cobalt accounts for 21 parts, and described nickel accounts for 25 parts, described ferrum accounts for 7 parts, and described manganese accounts for 9 parts, and described tungsten accounts for 11 parts, described niobium accounts for 6 parts, and described indium accounts for 5 parts, and described titanium accounts for 13 parts。
Proportioning is carried out so that the functional alloy property height obtained differs by each composition Different Weight percentage ratio。
Of the present invention is a kind of casting rapidoprint White brass alloy, and the present invention adopts copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium to be grouped into, and has intensity height, corrosion resistance is good, pyroelectricity is good, wearability is good, the feature of 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 that disclosed herein; the change can expected without creative work or replacement, all should be encompassed within protection scope of the present invention。Therefore, protection scope of the present invention should be as the criterion with claims protection defined。

Claims (3)

1. a casting rapidoprint White brass alloy, it is characterized in that: described casting rapidoprint White brass alloy is grouped into by copper, cobalt, nickel, ferrum, manganese, tungsten, niobium, indium and nine kinds of one-tenth of titanium, in described casting rapidoprint White brass alloy, parts by weight shared by each composition are respectively as follows: described copper and account for 95-100 part, described cobalt accounts for 18-22 part, described nickel accounts for 23-26 part, described ferrum accounts for 5-8 part, described manganese accounts for 7-10 part, described tungsten accounts for 9-12 part, described niobium accounts for 4-7 part, described indium accounts for 3-6 part, and described titanium accounts for 11-14 part。
2. casting rapidoprint White brass alloy according to claim 1, it is characterized in that: in described casting rapidoprint White brass alloy, parts by weight shared by each composition are particularly as follows: described copper accounts for 96 parts, described cobalt accounts for 19 parts, described nickel accounts for 24 parts, and described ferrum accounts for 6 parts, and described manganese accounts for 8 parts, described tungsten accounts for 10 parts, described niobium accounts for 5 parts, and described indium accounts for 4 parts, and described titanium accounts for 12 parts。
3. casting rapidoprint White brass alloy according to claim 1, it is characterized in that: in described casting rapidoprint White brass alloy, parts by weight shared by each composition are particularly as follows: described copper accounts for 99 parts, described cobalt accounts for 21 parts, described nickel accounts for 25 parts, and described ferrum accounts for 7 parts, and described manganese accounts for 9 parts, described tungsten accounts for 11 parts, described niobium accounts for 6 parts, and described indium accounts for 5 parts, and described titanium accounts for 13 parts。
CN201610245781.XA 2016-04-20 2016-04-20 White copper alloy for casting machining of materials Pending CN105695796A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610245781.XA CN105695796A (en) 2016-04-20 2016-04-20 White copper alloy for casting machining of materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610245781.XA CN105695796A (en) 2016-04-20 2016-04-20 White copper alloy for casting machining of materials

Publications (1)

Publication Number Publication Date
CN105695796A true CN105695796A (en) 2016-06-22

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Family Applications (1)

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CN201610245781.XA Pending CN105695796A (en) 2016-04-20 2016-04-20 White copper alloy for casting machining of materials

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CN (1) CN105695796A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106273885A (en) * 2016-08-15 2017-01-04 苏州润利电器有限公司 A kind of hardware stamping part two-layer compound high-strength alloy

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3628949A (en) * 1969-12-16 1971-12-21 Driver Co Wilbur B Thermocouple extension wire
JPS5562138A (en) * 1978-10-31 1980-05-10 Sumitomo Special Metals Co Ltd Alloy for compensating lead wire for ca thermocouple
CN103484719A (en) * 2013-09-29 2014-01-01 苏州市凯业金属制品有限公司 Copper-nickel alloy metal pipe
RU2566098C1 (en) * 2014-12-22 2015-10-20 Юлия Алексеевна Щепочкина Copper-based alloy

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3628949A (en) * 1969-12-16 1971-12-21 Driver Co Wilbur B Thermocouple extension wire
JPS5562138A (en) * 1978-10-31 1980-05-10 Sumitomo Special Metals Co Ltd Alloy for compensating lead wire for ca thermocouple
CN103484719A (en) * 2013-09-29 2014-01-01 苏州市凯业金属制品有限公司 Copper-nickel alloy metal pipe
RU2566098C1 (en) * 2014-12-22 2015-10-20 Юлия Алексеевна Щепочкина Copper-based alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
原梅妮: "《航空工程材料与失效分析》", 31 May 2014, 中国石化出版社 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106273885A (en) * 2016-08-15 2017-01-04 苏州润利电器有限公司 A kind of hardware stamping part two-layer compound high-strength alloy

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Application publication date: 20160622