CN103757476A - Magnesium-bismuth brass alloy material and preparation method thereof - Google Patents

Magnesium-bismuth brass alloy material and preparation method thereof Download PDF

Info

Publication number
CN103757476A
CN103757476A CN201410011620.5A CN201410011620A CN103757476A CN 103757476 A CN103757476 A CN 103757476A CN 201410011620 A CN201410011620 A CN 201410011620A CN 103757476 A CN103757476 A CN 103757476A
Authority
CN
China
Prior art keywords
bismuth
magnesium
speed
hour
copper
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
CN201410011620.5A
Other languages
Chinese (zh)
Inventor
丁健
倪受春
林其斌
葛浩
夏岩磊
杨玭
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.)
Chuzhou University
Original Assignee
Chuzhou University
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 Chuzhou University filed Critical Chuzhou University
Priority to CN201410011620.5A priority Critical patent/CN103757476A/en
Publication of CN103757476A publication Critical patent/CN103757476A/en
Pending legal-status Critical Current

Links

Abstract

The invention relates to a magnesium-bismuth brass alloy material which contains the following chemical components in percentage by mass: 6.5-5.9% of magnesium, 0.25-0.29% of bismuth, 11.5-11.9% of zinc, 0.04-0.06% of Ta, 1.6-1.8% of Mn, 0.4-0.5% of Be and the balance of copper. The alloy has the characteristics of no toxicity, environment friendliness, free cutting, lower cost than bismuth brass, high-temperature oxidation resistance, higher strength and favorable cold/hot working properties, and can be forged and cast into wires, bars and many other parts; and by reasonably controlling the after-casting treatment temperature and using waste copper as the raw material, the core hardness is basically consistent with the surface hardness, and the alloy quality is uniform. When the refining agent is used for casting production, the porosity in the casting is lowered by 1-2 degrees, the oxide inclusion content is at level 2 or so, and the yield is obviously enhanced.

Description

A kind of magnesium-bismuth-brass alloys material and preparation method thereof
Technical field
The manufacture field that the present invention relates to metal alloy compositions, relates in particular to a kind of magnesium-bismuth-brass alloys material and preparation method thereof.
Background technology
Copper is because of its good electroconductibility, plasticity-, and erosion resistance, applies very extensive.In copper alloy, add Lv ﹑ Nie ﹑ Meng ﹑ Xi ﹑ Gui ﹑ lead and other elements, can improve the performance of copper, for different places.Still there are some problems in the existing copper alloy of China at present, and as alloy contains a large amount of impurity elements, high temperature fatigue is poor, hot strength is low; Hardness is low, wears no resistance, frictional coefficient is large, and work-ing life is short; Poorly conductive, waste electric energy; Bending machining performance is poor, easily fractures; Quality weight, constructional difficulties; Can't meet market demands.
Summary of the invention
The object of the present invention is to provide a kind of magnesium-bismuth-brass alloys material and preparation method thereof, this Cu alloy material has advantages of easy cutting, good processability, high temperature oxidation resisting.
Technical scheme of the present invention is as follows:
A kind of magnesium-bismuth-brass alloys material, is characterized in that: chemical element composition and mass percent thereof that it contains are: magnesium 6.5-6.9, bismuth 0.25-0.29, zinc 11.5-11.9, Ta0.04-0.06, Mn1.6-1.8, Be0.4-0.5, surplus are copper.
The production method of described magnesium-bismuth-brass alloys material, is characterized in that:
(1), preparing fine copper and copper scrap originates as copper matrix in 1:0.3-0.8 ratio, fine copper is added to drop in stove and melt, carry out removing impurities matter, deoxidation, employing refining agent initial refining, add alloying constituent and carry out alloying, then add copper scrap fusing, add refining agent secondary refining, detection and adjust chemical element component content to qualified, casting, casting postheat treatment etc.;
(2) in alloying process, to the lot sequence that drops into alloying element in stove, be: (1) zinc; (2) bismuth, manganese, Ta; (3) other remaining components; The each batch of timed interval of dropping into element is 20-24 minute, after feeding intake, stirs.
Described casting postheat treatment is: first by room temperature, with 250-260 ℃/h of speed, be warming up to 330-350 ℃, then be cooled to 280-290 ℃ with 200-210 ℃/h of speed, then be warming up to 550-570 ℃ with 250-260 ℃/h of speed, insulation 1-2 hour; With 270-280 ℃/h of speed, be cooled to 100-120 ℃ again, insulation 1-2 hour; With 250-260 ℃/h of speed, be warming up to 340-360 ℃ again, insulation 1-2 hour; With 250-260 ℃/h of speed, be cooled to 100-120 ℃ again, insulation 1-2 hour; With 200-210 ℃/h of speed, be warming up to 300-310 ℃ again, insulation 2-3 hour, takes out air cooling and get final product.
Described refining agent is made by the raw material of following weight part: Paris white 4-5, bauxitic clay 2.1-2.5, trees ashes 1-2, nano silicon 1-2, alum 2-3, jade powder 3-4, calcium carbide powder 4-5, potassium fluotitanate 2-3, sodium tetraborate 1-2, Bi 2o 32-3; Its preparation method is that Paris white, bauxitic clay, trees ashes, nano silicon, alum, jade powder, calcium carbide powder are mixed, be heated to 2600-3000 ℃, stir 1-2 hour, after cooling, be added in the hydrochloric acid soln of 10-15%, soak 1-2 hour, filter, filter residue is cleaned with clear water repeatedly, dries, and merges and mixes and get final product with other composition.
Beneficial effect of the present invention
Alloy of the present invention has the free machining feature of asepsis environment-protecting, and cost is low compared with bismuth brass, also has the feature of high-temperature oxidation resistant, and intensity is higher, and cold and hot working performance is good, can forge, be cast as the various parts such as wire rod, excellent class; By reasonable control casting post-processing temperature, use copper scrap as raw material, make core hardness and surface hardness basically identical, alloy quality homogeneous.Refining agent of the present invention, for Foundry Production, can make the degree of porosity in foundry goods reduce 1-2 degree, and oxide inclusion, 2 grades of left and right, obviously improves yield rate.
Embodiment
A kind of magnesium-bismuth-brass alloys material, chemical element composition and mass percent thereof that it contains are: magnesium 6.5-6.9, bismuth 0.25-0.29, zinc 11.5-11.9, Ta0.04-0.06, Mn1.6-1.8, Be0.4-0.5, surplus are copper.
The production method of described magnesium-bismuth-brass alloys material is as follows:
(1), preparing fine copper and copper scrap originates as copper matrix in 1:0.5 ratio, fine copper is added to drop in stove and melt, carry out removing impurities matter, deoxidation, employing refining agent initial refining, add alloying constituent and carry out alloying, then add copper scrap fusing, add refining agent secondary refining, detection and adjust chemical element component content to qualified, casting, casting postheat treatment etc.;
(2) in alloying process, to the lot sequence that drops into alloying element in stove, be: (1) zinc; (2) bismuth, manganese, Ta; (3) other remaining components; The each batch of timed interval of dropping into element is 22 minutes, after feeding intake, stirs.
Described casting postheat treatment is: first by room temperature, with 255 ℃/h of speed, be warming up to 340 ℃, then be cooled to 285 ℃ with 205 ℃/h of speed, then be warming up to 560 ℃ with 255 ℃/h of speed, be incubated 1.5 hours; With 2750 ℃/h of speed, be cooled to 110 ℃ again, be incubated 1.5 hours; With 255 ℃/h of speed, be warming up to 350 ℃ again, be incubated 1.5 hours; With 255 ℃/h of speed, be cooled to 110 ℃ again, be incubated 1.5 hours; With 205 ℃/h of speed, be warming up to 305 ℃ again, be incubated 2.5 hours, take out air cooling and get final product.
Described refining agent by following weight part (kilogram) raw material make: Paris white 5, bauxitic clay 2.1, trees ashes 1, nano silicon 2, alum 2, jade powder 4, calcium carbide powder 4, potassium fluotitanate 3, sodium tetraborate 2, Bi 2o 32; Its preparation method is that Paris white, bauxitic clay, trees ashes, nano silicon, alum, jade powder, calcium carbide powder are mixed, be heated to 2600-3000 ℃, stir 1-2 hour, after cooling, be added in the hydrochloric acid soln of 10-15%, soak 1-2 hour, filter, filter residue is cleaned with clear water repeatedly, dries, and merges and mixes and get final product with other composition.
The present embodiment magnesium-bismuth-brass alloys material, tensile strength б b is 510Mpa, yield strength 486MPa, hardness value HB is 134, electric conductivity %IACS54,602 ℃ of softening temperatures, 20 ℃ of unit elongation 16%.

Claims (4)

1. a magnesium-bismuth-brass alloys material, is characterized in that: chemical element composition and mass percent thereof that it contains are: magnesium 6.5-6.9, bismuth 0.25-0.29, zinc 11.5-11.9, Ta0.04-0.06, Mn1.6-1.8, Be0.4-0.5, surplus are copper.
2. the production method of magnesium-bismuth-brass alloys material according to claim 1, is characterized in that:
(1), preparing fine copper and copper scrap originates as copper matrix in 1:0.3-0.8 ratio, fine copper is added to drop in stove and melt, carry out removing impurities matter, deoxidation, employing refining agent initial refining, add alloying constituent and carry out alloying, then add copper scrap fusing, add refining agent secondary refining, detection and adjust chemical element component content to qualified, casting, casting postheat treatment etc.;
(2) in alloying process, to the lot sequence that drops into alloying element in stove, be: (1) zinc; (2) bismuth, manganese, Ta; (3) other remaining components; The each batch of timed interval of dropping into element is 20-24 minute, after feeding intake, stirs.
3. the production method of magnesium-bismuth-brass alloys material according to claim 2, it is characterized in that: described casting postheat treatment is: first by room temperature, with 250-260 ℃/h of speed, be warming up to 330-350 ℃, with 200-210 ℃/h of speed, be cooled to 280-290 ℃ again, with 250-260 ℃/h of speed, be warming up to 550-570 ℃ again, insulation 1-2 hour; With 270-280 ℃/h of speed, be cooled to 100-120 ℃ again, insulation 1-2 hour; With 250-260 ℃/h of speed, be warming up to 340-360 ℃ again, insulation 1-2 hour; With 250-260 ℃/h of speed, be cooled to 100-120 ℃ again, insulation 1-2 hour; With 200-210 ℃/h of speed, be warming up to 300-310 ℃ again, insulation 2-3 hour, takes out air cooling and get final product.
4. the production method of magnesium-bismuth-brass alloys material according to claim 2, is characterized in that: described refining agent is made by the raw material of following weight part: Paris white 4-5, bauxitic clay 2.1-2.5, trees ashes 1-2, nano silicon 1-2, alum 2-3, jade powder 3-4, calcium carbide powder 4-5, potassium fluotitanate 2-3, sodium tetraborate 1-2, Bi 2o 32-3; Its preparation method is that Paris white, bauxitic clay, trees ashes, nano silicon, alum, jade powder, calcium carbide powder are mixed, be heated to 2600-3000 ℃, stir 1-2 hour, after cooling, be added in the hydrochloric acid soln of 10-15%, soak 1-2 hour, filter, filter residue is cleaned with clear water repeatedly, dries, and merges and mixes and get final product with other composition.
CN201410011620.5A 2014-01-10 2014-01-10 Magnesium-bismuth brass alloy material and preparation method thereof Pending CN103757476A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410011620.5A CN103757476A (en) 2014-01-10 2014-01-10 Magnesium-bismuth brass alloy material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410011620.5A CN103757476A (en) 2014-01-10 2014-01-10 Magnesium-bismuth brass alloy material and preparation method thereof

Publications (1)

Publication Number Publication Date
CN103757476A true CN103757476A (en) 2014-04-30

Family

ID=50524790

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410011620.5A Pending CN103757476A (en) 2014-01-10 2014-01-10 Magnesium-bismuth brass alloy material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN103757476A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104032163A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Free-cutting brass alloy material and preparation method thereof
CN104032170A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Free-cutting brass alloy material and preparation method thereof
CN104032175A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Lanthanum-containing brass alloy material and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002266042A (en) * 2001-03-09 2002-09-18 Kobe Steel Ltd Copper alloy sheet having excellent bending workability
CN1517446A (en) * 2003-01-22 2004-08-04 ͬ�Ϳ�ҵ��ʽ���� Copper-based alloy and its manufacturing method
CN101161836A (en) * 2007-10-16 2008-04-16 中南大学 Leadless easy-cutting magnesium brass alloy and method for preparing same
CN101289714A (en) * 2007-04-18 2008-10-22 北京有色金属研究总院 Lead-free and easy-cutting magnesium-bismuth-brass alloys
CN103397221A (en) * 2013-07-01 2013-11-20 安徽三联泵业股份有限公司 Copper alloy for drawing mould and preparation method thereof

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002266042A (en) * 2001-03-09 2002-09-18 Kobe Steel Ltd Copper alloy sheet having excellent bending workability
CN1517446A (en) * 2003-01-22 2004-08-04 ͬ�Ϳ�ҵ��ʽ���� Copper-based alloy and its manufacturing method
CN101289714A (en) * 2007-04-18 2008-10-22 北京有色金属研究总院 Lead-free and easy-cutting magnesium-bismuth-brass alloys
CN101161836A (en) * 2007-10-16 2008-04-16 中南大学 Leadless easy-cutting magnesium brass alloy and method for preparing same
CN103397221A (en) * 2013-07-01 2013-11-20 安徽三联泵业股份有限公司 Copper alloy for drawing mould and preparation method thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104032163A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Free-cutting brass alloy material and preparation method thereof
CN104032170A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Free-cutting brass alloy material and preparation method thereof
CN104032175A (en) * 2014-05-12 2014-09-10 蚌埠市宏威滤清器有限公司 Lanthanum-containing brass alloy material and preparation method thereof

Similar Documents

Publication Publication Date Title
CN103757475B (en) A kind of production method of high-strength simple-cutting tin-brass alloy material
CN103757479B (en) A kind of Lead-free environment-friendlycopper-nickel-zinc copper-nickel-zinc alloy material and preparation method thereof
CN103882270A (en) Aluminum alloy material for special-type high pressure oil pump cases and preparation method thereof
CN103757481A (en) Free-cutting bismuth-nickel copper alloy material and preparation method thereof
CN103757476A (en) Magnesium-bismuth brass alloy material and preparation method thereof
CN103882267A (en) High-strength cast aluminum alloy material and preparation method thereof
CN104032173A (en) High-strength tin-brass alloy material and preparation method thereof
CN103882268A (en) Aluminum alloy material for triangular valves and preparation method thereof
CN103773993B (en) A kind of zinc electroplating bath cupronickel alloy material and preparation method thereof
CN104032169A (en) Cerium-containing leadless free-cutting zinc-copper-nickel alloy material and preparation method thereof
CN104032183B (en) A kind of free machining environmental protection cupronickel alloy material and preparation method thereof
CN103757472B (en) A kind of containing cerium cutting brass alloy material and preparation method thereof
CN103757480B (en) Complicated cupronickel alloy material of a kind of seawater corrosion resistance and preparation method thereof
CN104032170A (en) Free-cutting brass alloy material and preparation method thereof
CN103757473B (en) A kind of environment-protective free-cutting nickel silver alloy material and preparation method thereof
CN103757474A (en) High-manganese free-cutting brass alloy material and preparation method thereof
CN104032164A (en) Leadless free-cutting silicon brass alloy material and preparation method thereof
CN103757465A (en) Corrosion-resistant free-cutting copper alloy material and preparation method thereof
CN104032174A (en) Leadless free-cutting zinc-copper-nickel alloy material and preparation method thereof
CN104032175B (en) A kind of containing lanthanum brass alloy material and preparation method thereof
CN103882258A (en) Zinc alloy material for valve seats and preparation method thereof
CN103757471B (en) A kind of leadless easy-cutting magnesium brass alloy material and preparation method thereof
CN104032165B (en) A kind of antifouling and seawater corrosion resistance Cu alloy material and preparation method thereof
CN104032200B (en) A kind of resistance to high temperature oxidation brass alloy material and preparation method thereof
CN104032179A (en) Leadless environment-friendly copper alloy material and preparation method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20140430

RJ01 Rejection of invention patent application after publication