CN102628121A - Manufacturing method of complex copper-zinc alloy shell - Google Patents

Manufacturing method of complex copper-zinc alloy shell Download PDF

Info

Publication number
CN102628121A
CN102628121A CN201210082004XA CN201210082004A CN102628121A CN 102628121 A CN102628121 A CN 102628121A CN 201210082004X A CN201210082004X A CN 201210082004XA CN 201210082004 A CN201210082004 A CN 201210082004A CN 102628121 A CN102628121 A CN 102628121A
Authority
CN
China
Prior art keywords
zinc alloy
alloy
copper
complex copper
zinc
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
CN201210082004XA
Other languages
Chinese (zh)
Inventor
朱春来
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201210082004XA priority Critical patent/CN102628121A/en
Publication of CN102628121A publication Critical patent/CN102628121A/en
Pending legal-status Critical Current

Links

Landscapes

  • Conductive Materials (AREA)

Abstract

The present invention relates to a manufacturing method of a complex copper-zinc alloy shell. The method comprises the following steps: 1) sampling: selecting a certain ratio of Zn, C, Mn, Si, Nb, Ti, V, Mo, Cr, Al and Cu; 2) placing the materials in a 5t cover-type resistance furnace for smelting with gas and slag removal, thus carrying out refining with high cleanliness; 3) moulding a shell; 4) carrying out homogeneous annealing treatment for 24 h at of 440 to 460 DEG C. The invention is characterized in that the method optimizes composition of complex copper zinc alloy through experiment and combines with a heat treatment technology, so as to further refine crystal grains and distribution morphology of the second phase of the Cu-Zn alloy, improve stability, strength and toughness of the alloy, and in that the process operation and equipment requirement are simple.

Description

A kind of method of manufacture of complicated copper-zinc alloy housing
Technical field
The present invention relates to a kind of radiating shell, particularly a kind of method of manufacture of the radiating shell of processing by complicated copper-zinc alloy that has that special heat radiation needs.
 
Background technology
In the prior art, various engineerings and workplace all be unable to do without automatic equipment, and some special occasions have strict demand for equipment temperature at work, except some extra cooling of tool and means, also need to adopt the good material of thermal diffusivity usually; The heat-conductive characteristic of copper is very high, yet the reserves of copper are limited, and price was also constantly soaring in recent years, had increased production cost, so in the actual production, often adopts copper-zinc alloy as substituting.
Common copper-zinc alloy is the basis with copper, and zinc is made main adding elements, and it has yellow attractive in appearance, and copper-zinc alloy has good performance of heat dissipation equally, and it is cheap to compare pure Cu, has certain mechanical property again, therefore is used widely.Ordinary copper-zinc binary alloy comprises multiple tissue, and wherein α is the substitutional solid solution of zinc in copper mutually, but the about 38%Zn of normal temperature solid solution has face-centered cubic lattice, and plasticity is good, and the cold and hot working that suits to carry out increases along with dissolving the Zn amount among the Cu, and the solution strengthening effect strengthens; β is the sosoloid of electron compound CuZn for base mutually, has body centered structure.Except α, β mutually, generally also have the γ phase in the copper-zinc alloy, γ is to be the sosoloid of base with the sophisticated electronic compound mutually, has complicated cubic(al)grating, γ phase character is crisp firmly, and is unfavorable to the copper alloy performance.
In order to improve the performance of common copper-zinc alloy; In the prior art, in copper-zinc alloy, add a small amount of tin, aluminium, manganese, iron, silicon, nickel, lead and other elements usually, constitute ternary, quaternary even quinary alloy; Be complicated copper-zinc alloy, also claim special copper-zinc alloy.The tissue of complicated copper-zinc alloy generally can be calculated according to " the zinc equivalent coefficient " of addition element in the copper-zinc alloy.In copper zinc alloy, add a small amount of other alloying elements, α/(alpha+beta) phase region in the Cu-Zn state graph is moved to the left or to the right.So the tissue of special copper-zinc alloy is equivalent in the common copper-zinc alloy to increase or to have reduced the tissue of zinc content usually.For example, in the Cu-Zn alloy, add the tissue behind 1% Si, promptly be equivalent in the Cu-Zn alloy, increase by the alloy structure of 10% Si.So Si " zinc equivalent " is 10.Again for example, if " zinc equivalent coefficient " maximum of Si makes α/(alpha+beta) phase boundary in the Cu-Zn system significantly shift to the copper side, promptly dwindle alpha phase zone strongly.Ni " zinc equivalent coefficient " is negative value, promptly enlarges alpha phase zone.
Multielement enhanced on a small quantity is a kind of approach that improves alloy property; Yet, be polynary complicated sosoloid mutually because the α in the special copper-zinc alloy reaches β mutually, add the γ phase that possibly occur; A spot of element have the influence of two aspects simultaneously; Possibly improve on the one hand solidity to corrosion, the strength property of alloy, then increase the fragility of material on the other hand, influence the performances such as bending and machinability of alloy.So, select and set of dispense just can obtain through a large amount of experiments and comparative analysis than needing for the material of alloy.
 
Summary of the invention
The present invention just provides a kind of method of manufacture of the radiating shell of being processed by complicated copper-zinc alloy that has that special heat radiation needs, and it draws through experiment has good performance of heat dissipation and mechanical property.
Technical scheme of the present invention is following:
A kind of method of manufacture of complicated copper-zinc alloy housing comprises following steps:
1) draw materials, select the raw material of following chemical component weight per-cent:
Zn:?28~30%, C:0.02~0.03%;
Mn:2.1~2.3%; Si:0.15~0.20%,
Nb:0.04~0.06%, Ti:0.02~0.04%,
V:0.05~0.09%, Mo:0.1~0.4%,
Cr:0.55~0.65%, Al:0.06~0.10%
All the other are Cu and impurity;
2) above-mentioned materials is placed melting in the 5t bell-type resistance furnace, degasification slagging-off in fusion process, thus carry out the high-cleanness, high refining;
3) cast the casting mold of housing;
4) handle through the homo genizing annelaing of 440 ° of C~460 ° C of 24 hours.
Characteristics of the present invention are; Through testing the proportioning of the complicated copper-zinc alloy in preferred place; And combine with thermal treatment process; Further refinement Cu-Zn is the crystal grain and second distributional pattern mutually of alloy, improves stability and the intensity and the toughness of this alloy, and technological operation and equipment requirements are simple.
 
Embodiment
Below in conjunction with specific examples technical scheme of the present invention is further specified.Make the radiating shell of processing by complicated copper-zinc alloy that has that special heat radiation needs of the present invention through following steps.
Embodiment 1
1) draw materials, select the raw material of following chemical component weight per-cent:
Zn:?28%, C:0.02%;
Mn:2.1%; Si:0.15%,
Nb:0.04%, Ti:0.02%,
V:0.05%, Mo:0.1%,
Cr:0.55%, Al:0.06%
All the other are Cu and impurity;
2) above-mentioned materials is placed melting in the 5t bell-type resistance furnace, degasification slagging-off in fusion process, thus carry out the high-cleanness, high refining;
3) cast the casting mold of housing;
4) handle through the homo genizing annelaing about 440 ° of C of 24 hours.
The radiating shell that makes carries out the test force performance on the CMT5105 electronic universal tester, and carries out the fracture toughness property experiment in MTS material experiment technology.Through test; The ys of having of adopting that the present invention the makes radiating shell that special heat radiation needs is processed by complicated copper-zinc alloy is 634MPa; Fracture toughness property be 936
Figure 201210082004X100002DEST_PATH_IMAGE001
; Its grain size distribution is even, when possessing excellent heat dispersion performance, also has good mechanical property.
 
Embodiment 2
1) draw materials, select the raw material of following chemical component weight per-cent:
Zn:?30%, C:?0.03%;
Mn:2.3%; Si:?0.20%,
Nb:0.06%, Ti:?0.04%,
V:?0.09%, Mo:0.4%,
Cr:?0.65%, Al:?0.10%
All the other are Cu and impurity;
2) above-mentioned materials is placed melting in the 5t bell-type resistance furnace, degasification slagging-off in fusion process, thus carry out the high-cleanness, high refining;
3) cast the casting mold of housing;
4) handle through the homo genizing annelaing about 460 ° of C of 24 hours.
The radiating shell that makes carries out the test force performance on the CMT5105 electronic universal tester, and carries out the fracture toughness property experiment in MTS material experiment technology.Through test; The ys of having of adopting that the present invention the makes radiating shell that special heat radiation needs is processed by complicated copper-zinc alloy is 647MPa; Fracture toughness property be 867
Figure 321327DEST_PATH_IMAGE001
; Its grain size distribution is even, when possessing excellent heat dispersion performance, also has good mechanical property.

Claims (1)

1. the method for manufacture of a complicated copper-zinc alloy housing is characterized in that, comprises following steps:
1) draw materials, select the raw material of following chemical component weight per-cent:
Zn:?28~30%, C:0.02~0.03%;
Mn:2.1~2.3%; Si:0.15~0.20%,
Nb:0.04~0.06%, Ti:0.02~0.04%,
V:0.05~0.09%, Mo:0.1~0.4%,
Cr:0.55~0.65%, Al:0.06~0.10%
All the other are Cu and impurity;
2) above-mentioned materials is placed melting in the 5t bell-type resistance furnace, degasification slagging-off in fusion process, thus carry out the high-cleanness, high refining;
3) cast the casting mold of housing;
4) handle through the homo genizing annelaing of 440 ° of C~460 ° C of 24 hours.
CN201210082004XA 2012-03-26 2012-03-26 Manufacturing method of complex copper-zinc alloy shell Pending CN102628121A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210082004XA CN102628121A (en) 2012-03-26 2012-03-26 Manufacturing method of complex copper-zinc alloy shell

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210082004XA CN102628121A (en) 2012-03-26 2012-03-26 Manufacturing method of complex copper-zinc alloy shell

Publications (1)

Publication Number Publication Date
CN102628121A true CN102628121A (en) 2012-08-08

Family

ID=46586512

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210082004XA Pending CN102628121A (en) 2012-03-26 2012-03-26 Manufacturing method of complex copper-zinc alloy shell

Country Status (1)

Country Link
CN (1) CN102628121A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102676875A (en) * 2012-06-12 2012-09-19 杨晓锋 Shell with good heat dissipation performance made of complex copper-zinc alloy
CN115233031A (en) * 2021-09-07 2022-10-25 大连理工大学 High-performance copper alloy and preparation method thereof

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102796916A (en) * 2012-03-21 2012-11-28 朱湖泽 Method for manufacturing complex copper-zinc alloy shell

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102796916A (en) * 2012-03-21 2012-11-28 朱湖泽 Method for manufacturing complex copper-zinc alloy shell

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102676875A (en) * 2012-06-12 2012-09-19 杨晓锋 Shell with good heat dissipation performance made of complex copper-zinc alloy
CN115233031A (en) * 2021-09-07 2022-10-25 大连理工大学 High-performance copper alloy and preparation method thereof
CN115233031B (en) * 2021-09-07 2022-12-30 大连理工大学 High-performance copper alloy and preparation method thereof

Similar Documents

Publication Publication Date Title
CN101285137B (en) Leadless and free-cutting brass containing magnesium and manufacturing method for manufactures
WO2018161380A1 (en) Tellurium-beryllium-copper alloy and preparation method thereof
JP4134279B1 (en) Cu alloy material
CN105296818A (en) Aluminum alloy and preparation method and application thereof
CN106636734B (en) High-intensitive, highly conductive, high resistance to stress relaxation copper alloy elastic material and preparation method thereof
US8580191B2 (en) Brass alloys having superior stress corrosion resistance and manufacturing method thereof
CN108504910B (en) Aluminum alloy and preparation method thereof
CN101440443A (en) Dezincification corrosion resistant low-stibium aluminum yellow brass alloy and manufacturing method thereof
CN108130456B (en) High-thermal-conductivity die-casting aluminum alloy material and preparation method thereof
JP4620963B2 (en) Brass, manufacturing method thereof, and parts using the same
JP2007126739A (en) Copper alloy for electronic material
CN111979446A (en) Tellurium-beryllium-copper alloy for manufacturing rod and wire and preparation method thereof
CN102676875A (en) Shell with good heat dissipation performance made of complex copper-zinc alloy
CN102605210B (en) Method for manufacturing complex copper-zinc alloy
CN101619421A (en) High -toughness hot working die steel
CN104651685A (en) Aluminum magnesium alloy material and preparation method thereof
CN102628121A (en) Manufacturing method of complex copper-zinc alloy shell
CN101709444B (en) Thermal treatment method for lead-free aluminum alloy
KR20200087123A (en) Mold material for casting, and copper alloy material
CN102796916A (en) Method for manufacturing complex copper-zinc alloy shell
CN103882268B (en) A kind of triangle vavle aluminum alloy materials and preparation method thereof
CN106244848B (en) The copper-based glass mold material of microalloying non-ferrous metal and its manufacturing method
JP5713299B2 (en) Free-cutting stainless steel cast steel product and manufacturing method thereof
CN101921926B (en) Low-calcium and easy-cutting silicon brass alloy and preparation method thereof
CN106167863B (en) A kind of low beryllium alumin(i)um alloy and preparation method and application

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20120808