CN1223306A - High-strength high softening temp. copper based elastic material - Google Patents
High-strength high softening temp. copper based elastic material Download PDFInfo
- Publication number
- CN1223306A CN1223306A CN 98104639 CN98104639A CN1223306A CN 1223306 A CN1223306 A CN 1223306A CN 98104639 CN98104639 CN 98104639 CN 98104639 A CN98104639 A CN 98104639A CN 1223306 A CN1223306 A CN 1223306A
- Authority
- CN
- China
- Prior art keywords
- alloy
- copper
- elastic material
- elastic
- based elastic
- 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.)
- Granted
Links
Abstract
The present invention relates to a kind of copper-base alloy. It is a good elastic material, can be used for making precision elastic elements in the instruments, meters and electronic communication devices, and possesses good conductivity, higher tensile strength, high elastic limit and toughness, high softening temp., strong resistance to stress relaxation, good machining property, weldability and electroplating property, and high corrosion-proofing and antioxidation properties. Its material component composition includes: 4.6-6.8% of Ni, 1.1-2.6% of Si, 0.8-2.1% of Al, 0.21-0.52% of Fe, 0.14-0.43% of Cr, 0.08-0.19 of Ce, 0.04-0.12% of Mg and the rest is Cu. Said invention is rich in raw material source, non-toxic and low in cost, and can be partially substituted for beryllium bronze material.
Description
The invention belongs to copper base alloy.
Conduction contact spring, connector and elastic sensing element in current precision instrumentation, the electronic communication device extensively adopts berylliumbronze or tin-phosphor bronze elastic alloy, but the rare costliness of berylliumbronze raw material, toxic in the production, alloy property is to the thermal treatment process sensitivity when producing and use, the mechanical property instability: and the poor processability in the tin-phosphor bronze, production cycle is long, elastic performance and electric conductivity are on the low side, precision and poor reliability, the thermostability of two kinds of alloys is all lower, and maximum operation temperature is less than 100 ℃.At present both at home and abroad energetically research and development replace the novel copper-based elastic alloy of berylliumbronze, developed titanium bronze, copper-nickel-Xi is alloy, copper-nickel-Mn series alloy, 156 complex brass alloys etc.At present dropped into the titanium bronze of suitability for industrialized production, as (or tensile strength is 980~1280MPa, unit elongation 4.0~8.0%, electric conductivity 13~18%IACS after 0.5~1.0%Cr) the copper alloy cold working timeliness to contain 3.5~6%Ti, 0.15~0.25.Cu-9Ni-6Sn, the Cu-15Ni-8Sn of U.S.'s Bell Laboratory exploitation since the sixties (0.2Nb) alloy, by its intensity of thermomechanical treatment near in addition surpass berylliumbronze; The tensile strength of copper-nickel-Mn series alloy, 156 complex brass alloys and elastic limit are also near berylliumbronze.But titanium bronze melting technology complexity, castability is poor, metallurgical quality control difficulty; Copper-nickel-Xi is that discontinuous precipitation easily takes place in ag(e)ing process alloy prematurely, and makes alloy that brittle rupture easily take place: the electric conductivity of alloys such as copper-nickel-Xi system, copper-nickel-Mn series alloy, 156 complex brass is generally on the low side.
The object of the invention provides that a kind of electric conductivity and elastic performance approach that berylliumbronze, toughness are higher than berylliumbronze, anti-stress relaxation ability is strong, use temperature is higher, anti-corrosion and high strength high softening temperature copper based elastic material that oxidation-resistance is strong, and raw material sources are abundant, cost is lower, easy to process.
Material provided by the invention contains (by weight) 4.6~6.8%Ni, 1.1~2.6%Si, 0.8~2.1%Al, 0.21~0.52%Fe, 0.14~0.43%Cr, 0.08~0.19%Ce, 0.04~0.12%Mg, surplus Cu.
Embodiment:
This alloy material of the present invention is a basic raw material with industrial pure copper, electrolytic nickel, industrial pure silicon, commercial-purity aluminium, technically pure iron, extra low carbon ferrochromium, cerium-rich mischmetal and pure magnesium.Alloying constituent is for containing (by weight) 5.4%Ni, 1.6%Si, 1.3%Al, 0.32%Fe, 0.28%Cr, 0.12%Ce, 0.09%Mg, surplus Cu.In advance technically pure iron, commercial-purity aluminium and extra low carbon ferrochromium are smelted into by weight proportion the lower master alloy of relative fusing point.Preparing burden by this alloying constituent is smelted into ingot casting (slab) in medium-frequency induction furnace, ingot mill surface, and hot rolling cogging, cold rolling behind the homogenizing annealing carries out process annealing and handles, and is cold rolling again, and it is rolling to carry out finished product after the solution treatment again, carries out the finished product ageing treatment at last.
Alloy material of the present invention improves alloy substrate intensity by adopting an amount of alloying element solid solution in matrix, multiple alloying element is separated out the complicated intermetallic compound of multicomponent and disperse through timeliness and is distributed in the alloy substrate and reaches and strengthen and keep hot strength, a small amount of alloying element crystal grain thinning and improve the thermoplasticity purpose of alloy.It is little that nickel, chromium solid solution strengthening effect reduce copper matrix electric conductivity greatly, improved the recrystallization temperature of alloy; Nickel, aluminium, silicon etc. have improved the solidity to corrosion and the oxidation-resistance of alloy, and separate out the Ni of small and dispersed in ag(e)ing process
3Intermetallic compound such as Al, NiSi, and obtain higher intensity, thermostability and electric conductivity.Iron is crystal grain thinning significantly, improves intensity, toughness and the thermoplasticity of alloy, has improved the hot-work ability of alloy.Magnesium has promoted the even dispersion degree that intermetallic compound is separated out at alloy substrate in the ag(e)ing process.Silicon, rare earth cerium have improved the casting technique performance of alloy, prevent segregation, have improved the yield rate of alloy, and rare-earth element cerium can purify alloy simultaneously, improve the hot and cold processing characteristics of copper alloy, improve corrosion resistance nature, mechanical property and the high-temperature stability of alloy.
Table 1 shows alloy material of the present invention after solution treatment → cold working (30% working modulus) → ageing treatment, with the performance comparison of cold working aging state beraloy.
By table 1 as seen, the electric conductivity and the elastic performance of material of the present invention approach berylliumbronze, toughness is higher than berylliumbronze, because this alloy material recrystallization temperature is high and the dispersion-strengthened action of intermetallic compound, so have better high-temperature behavior than berylliumbronze, anti-stress relaxation performance at 20~400 ℃ of invention materials all is higher than berylliumbronze, improved product reliability, so can use down at 100 ℃~250 ℃, (thick 0.15~0.6mm) bending property is higher than cold working aging state beraloy to band.The present invention is at 1%H
2SO
4In 0.0008 millimeter/year of the erosion rate of (20 ℃), erosion rate (0.11 millimeter/year) much smaller than cold working aging state beraloy, in media such as room temperature 10%NaCl, 10%HCl and 250 ℃~700 ℃ high temperature oxidation atmosphere, its erosion rate, oxidation weight gain all are lower than beraloy.So the invention material also has strong anti-corrosion and oxidation-resistance, in addition, because invention material recrystallization temperature is high and superheated susceptivity is low, so production technique is easy to control, processing, welding, electroplate functionally, raw material sources of the present invention are abundant, and raw materials cost can reduce by 60% than berylliumbronze.
Table 1:
Copper based elastic material of the present invention | Berylliumbronze (QBe2) | Berylliumbronze (QBe1.7) | ||
Tensile strength (6b) | Room temperature | 1090~1170MPa | ?????1320MPa | ??1080MPa |
300 ℃ (being incubated 1 hour) | 1010~1110MPa | ?????550MPa | ||
400 ℃ (being incubated 1 hour) | 680~740MPa | ?????500MPa | ||
Yield strength (60.01) | ????890~970MPa | ?????1120MPa | ??860MPa | |
Unit elongation (δ) | ????2.3~3.4% | ?????2% | ||
Young's modulus (E) | ????13200~13500MPa | ?13200~13500MPa | ||
Electric conductivity (LACS) | ????14.8~18.3% | ?????21~23% |
Claims (2)
1. a high strength high softening temperature copper based elastic material is characterized in that containing (by weight) 4.6~6.8%Ni, 1.1~2.6%Si, 0.8~2.1%Al, 0.21~0.52%Fe, 0.14~0.43%Cr, 0.08~0.19%Ce, 0.04~0.12%Mg, surplus Cu.
2. resilient material according to claim 1 is characterized in that containing (by weight) 5.4%Ni, 1.6%Si, 1.3%Al, 0.32%Fe, 0.28%Cr, 0.12%Ce, 0.09%Mg, surplus Cu.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN98104639A CN1063801C (en) | 1998-01-14 | 1998-01-14 | High-strength high softening temp. copper based elastic material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN98104639A CN1063801C (en) | 1998-01-14 | 1998-01-14 | High-strength high softening temp. copper based elastic material |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1223306A true CN1223306A (en) | 1999-07-21 |
CN1063801C CN1063801C (en) | 2001-03-28 |
Family
ID=5218354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN98104639A Expired - Fee Related CN1063801C (en) | 1998-01-14 | 1998-01-14 | High-strength high softening temp. copper based elastic material |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1063801C (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101984107A (en) * | 2010-12-03 | 2011-03-09 | 中南大学 | Method for preparing CuNiSiAl elastic copper alloy |
CN104532055A (en) * | 2014-11-21 | 2015-04-22 | 华南理工大学 | High nickel-content deformable aluminum white copper alloy material, and preparation method thereof |
CN107201462A (en) * | 2017-06-29 | 2017-09-26 | 大连理工大学 | A kind of Cu Ni Fe alloys with high softening temperature and preparation method thereof |
CN112708799A (en) * | 2020-12-21 | 2021-04-27 | 江西理工大学 | High-strength conductive softening-resistant copper alloy and preparation method thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3725830C2 (en) * | 1986-09-30 | 2000-03-30 | Furukawa Electric Co Ltd | Copper-tin alloy for electronic instruments |
JPS6425929A (en) * | 1987-07-20 | 1989-01-27 | Furukawa Electric Co Ltd | Copper alloy for electronic equipment |
-
1998
- 1998-01-14 CN CN98104639A patent/CN1063801C/en not_active Expired - Fee Related
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101984107A (en) * | 2010-12-03 | 2011-03-09 | 中南大学 | Method for preparing CuNiSiAl elastic copper alloy |
CN104532055A (en) * | 2014-11-21 | 2015-04-22 | 华南理工大学 | High nickel-content deformable aluminum white copper alloy material, and preparation method thereof |
CN107201462A (en) * | 2017-06-29 | 2017-09-26 | 大连理工大学 | A kind of Cu Ni Fe alloys with high softening temperature and preparation method thereof |
CN107201462B (en) * | 2017-06-29 | 2018-08-14 | 大连理工大学 | A kind of Cu-Ni-Fe alloys and preparation method thereof with high softening temperature |
CN112708799A (en) * | 2020-12-21 | 2021-04-27 | 江西理工大学 | High-strength conductive softening-resistant copper alloy and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN1063801C (en) | 2001-03-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104073686B (en) | A kind of deformation dilute copper alloy material riveted and application thereof | |
CN109609801A (en) | High property copper alloy and preparation method thereof | |
CN102560191A (en) | High-performance elastic copper alloy and preparation and processing method thereof | |
EP0189637B1 (en) | Copper alloy and production of the same | |
CN101225488A (en) | Copper alloy material for lead frame and preparation method thereof | |
CN106636734A (en) | High-strength, high-electric-conductivity and high-stress relaxation-resistance copper alloy elastic material and preparation method thereof | |
CN109930026B (en) | High-strength high-conductivity stress relaxation-resistant copper alloy lead frame material and preparation method thereof | |
CN106399748A (en) | Novel copper-nickel-silicon system alloy material for lead frame and preparation method of novel copper-nickel-silicon system alloy material | |
JPS5816044A (en) | Copper alloy | |
CN103898353A (en) | Copper alloy with high strength and high conductivity and preparation method thereof | |
JP5297855B2 (en) | Copper alloy sheet and manufacturing method thereof | |
CN100491558C (en) | High-performance yttrium-base heavy rare earth copper alloy die material and preparation method thereof | |
WO1998048068A1 (en) | Grain refined tin brass | |
US5882442A (en) | Iron modified phosphor-bronze | |
CN103502485A (en) | Copper alloy and method for producing copper alloy | |
US4147568A (en) | Copper-zinc-nickel-manganese alloys | |
CN105369077A (en) | Aluminum alloy conductor material and preparation method thereof | |
US3297497A (en) | Copper base alloy | |
US6379478B1 (en) | Copper based alloy featuring precipitation hardening and solid-solution hardening | |
US2126827A (en) | Copper-cobalt-zinc alloy | |
CN1063801C (en) | High-strength high softening temp. copper based elastic material | |
EP1021575B1 (en) | Copper based alloy featuring precipitation hardening and solid-solution hardening | |
JPS6132386B2 (en) | ||
CN101250644A (en) | Copper-base alloy capable of being used for lead frame material and manufacture method thereof | |
CN108929968A (en) | A kind of production technology of high conductivity copper alloy wire |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C06 | Publication | ||
PB01 | Publication | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |