CN102978430B - Method for manufacturing lead frame - Google Patents

Method for manufacturing lead frame Download PDF

Info

Publication number
CN102978430B
CN102978430B CN201210441508.6A CN201210441508A CN102978430B CN 102978430 B CN102978430 B CN 102978430B CN 201210441508 A CN201210441508 A CN 201210441508A CN 102978430 B CN102978430 B CN 102978430B
Authority
CN
China
Prior art keywords
copper
manufacture method
lead frame
iron alloy
alloy
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.)
Active
Application number
CN201210441508.6A
Other languages
Chinese (zh)
Other versions
CN102978430A (en
Inventor
葛艳明
袁志伟
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.)
Jiangsu Jinyuan High-end Equipment Co., Ltd.
Original Assignee
Jiangsu Jinyuan Forging Co Ltd
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 Jiangsu Jinyuan Forging Co Ltd filed Critical Jiangsu Jinyuan Forging Co Ltd
Priority to CN201210441508.6A priority Critical patent/CN102978430B/en
Publication of CN102978430A publication Critical patent/CN102978430A/en
Application granted granted Critical
Publication of CN102978430B publication Critical patent/CN102978430B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001Technical content checked by a classifier
    • H01L2924/0002Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00

Abstract

The present invention discloses a method for manufacturing a lead frame, comprising the following steps: melting, injecting into a blank mold, cooling; hot rolling and calendaring the casting blank; repeatedly cold rolling and calendaring, and two-stage continuous annealing hot rolled strips; cold rolling processing to make the variation of thickness be above 40%, and then low-temperature annealing to obtain the finished strips. In the manufacturing process, the component content is controlled including 2.0-2.6 wt% of Fe, 0.05-0.1 wt% of Ti, 0.01-0.03 wt% of B, 0-0.05 wt% of Na, 0.01-1.5 wt% of Mo, the balance being Cu and impurities. The strip is used to manufacture the lead frame. According to the present invention, the copper iron alloy structure is homogeneous, and precipitated phase is fine and dispersed. The finished product is high in tensile strength, hardness, conductivity, and elongation, and can meet the demands of the electronics industry on the performance of the lead frame material. The lead frame of the invention uses copper iron alloy, thereby also having excellent hot workability.

Description

A kind of manufacture method of down-lead bracket
Technical field
The present invention relates to a kind of manufacture method of down-lead bracket, relate in particular to a kind of manufacture method of the down-lead bracket for semiconducter device.
Background technology
At present, electronics and information industry has become a mainstay industry of China, and semiconducter device is as the foundation stone of this mainstay industry, and it comprises outer enclosure and internal integrated circuit; Unicircuit (IC) comprises chip, lead-in wire and down-lead bracket, adhesives, packaged material etc.Wherein, the major function of down-lead bracket is for chip provides mechanical support carrier, also has the external circuit of connection simultaneously, transmits the functions such as electrical signal and heat radiation.Therefore IC encapsulation need to possess the over-all propertieies such as high strength, high conduction, high thermal conductivity and good weldability, solidity to corrosion, plastic packaging, oxidation-resistance.
Research, trial-production, the production of China's down-lead bracket material are started late, down-lead bracket copper strips industrial scale is little, description is few, only have at present minority enterprise can produce the alloy of little model in batches, and there is quality low precision, quality is unstable, softening temperature is low, internal stress is inhomogeneous, width and the problem such as thickness deviation is overproof, appearance requirement is defective.Copper-iron alloy, as the main raw of manufacturing down-lead bracket, has accounted for 80% of market total value at present, and alloy designations has kind more than 100.
The C194 alloy that wherein China produces is wherein representative one.But the quality of the C194 down-lead bracket copper-iron alloy of producing at present can't meet the demands, low precision, description is few, unstable properties, copper strips yield rate, less than 50%, has larger defect at aspects such as template situation, residualinternal stress, surface smoothness, limit portion burrs.
Summary of the invention
The invention provides a kind of manufacture method of down-lead bracket, especially the manufacture method of copper-iron alloy for down-lead bracket, the method can effectively solve down-lead bracket copper-iron alloy over-all properties and not meet the problems such as production requirement, alloy structure are inhomogeneous, precipitated phase small and dispersed, adopts the characteristics such as tensile strength, hardness, unit elongation, specific conductivity and the softening temperature of copper-iron alloy prepared by manufacture method of the present invention all can meet preferably the many requirement of electronics industry to down-lead bracket material property.
The manufacture method of down-lead bracket of the present invention comprises the following steps:
(1) first major ingredient and auxiliary material are injected to mold after 1250~1350 DEG C of meltings, in the temperature range of liquidus temperature to 380 DEG C, carry out coolingly with 80 DEG C/more than min speed of cooling, in manufacturing processed, control alloying constituent and content F e and be 2.0~2.6wt%, Ti and be 0.05~0.1wt%, B and be 0.01~0.03wt%, Na and be 0~0.05wt%, Mo and be 0.01~1.5wt%, all the other components and be Cu and inevitable impurity;
(2) by the strand obtaining, the Heating temperature below 1000 DEG C is carried out hot rolling calendering, and in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity;
(3) hot rolled band is carried out repeatedly to cold rolling calendering and 300 DEG C~600 DEG C twin-stage continuous annealings, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity;
(4) carrying out cold rolling rolling processing reaches more than 40% its amounts of thickness variation, carry out again 420 DEG C of following low-temperature annealings, obtain band finished product, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity.
(5) adopt above-mentioned band to make down-lead bracket.
Preferably, the major ingredient in step (1) is No. 1 electrolytic copper, and auxiliary material is copper iron master alloy, copper boron master alloy, simple substance titanium, SODIUM METAL and mishmetal.
Preferably, the crystal grain diameter of controlling band in step (2) the hot rolling calendering course of processing is less than 50 μ m;
Preferably, the crystal grain diameter of controlling band in the cold rolled annealed course of processing in step (3) is less than 50 μ m.
Preferably, the copper-iron alloy making through step (4) also contains element and the total amount more than at least one in As, Sb, Bi, Bb, Co, Ni element and is less than 0.05wt%.
Preferably, the tensile strength of described copper alloy is that 600MBa is above, hardness 180Hv above, specific conductivity 66%IACS is above, unit elongation is more than 7.0%.
The preparation method's of down-lead bracket copper-iron alloy of the present invention beneficial effect is:
(1) copper-iron alloy over-all properties of the present invention is superior, alloy structure even, precipitated phase small and dispersed, and alloy price is relatively low, and production efficiency is high;
(2) tensile strength of finished product reaches that 600MBa is above, hardness 180Hv above, specific conductivity 66%IACS is above, unit elongation is more than 7.0%, can meet preferably the many requirement of electronics industry to blaster fuse frame material performance;
(3) down-lead bracket of the present invention also has good hot workability with copper-iron alloy, is conducive to manufacture, and is the best materials of producing the electrical and electronic parts such as down-lead bracket.
Embodiment
In order to make those skilled in the art more clearly understand the manufacture method of down-lead bracket of the present invention, describe its technical scheme in detail below by embodiment.
For meeting desired kind of specific character of the material for electrical/electronic components such as down-lead bracket, the invention provides a kind of manufacture method of down-lead bracket, the copper-iron alloy of wherein manufacturing down-lead bracket is selected the component concentration of best Ti, B, Na, Mo, manufactures with the advanced person's such as rolling processing conditions and heat-treat condition of most suitable slab cooling condition, strand process means.
In the present invention, all content, proportioning or per-cent are mass ratio.
Down-lead bracket copper-iron alloy, Fe:2.0~2.6wt%, Ti:0.05~0.1wt% in this copper-iron alloy, B:0.01~0.03wt%, Na:0~0.05wt%, Mo:0.01~1.5wt%, in copper alloy, also contain at least one above element and total amount in As, Sb, Bi, Bb, Co, Ni element and be less than 0.05wt%, and S content is below 25BBm; The tensile strength 600MBa of this copper-iron alloy is above, hardness 180Hv is above, specific conductivity 66%IACS is above, unit elongation is more than 7.0%.
Each component content of copper-iron alloy of the present invention: Fe is the main strengthening element in alloy, and alloy is after suitable ageing treatment, and the particle formal distribution that Fe element distributes with disperse is in copper matrix and play ageing strengthening effect.Due to the saturation solubility of Fe under normal temperature in Cu minimum (being only 0.0004% below at 300 DEG C), alloy can be realized higher specific conductivity; Can crystal grain thinning by adding a small amount of Fe, postpone the recrystallization process of copper, improve its intensity and hardness, but excessive plasticity, specific conductivity and the thermal conductivity that can reduce copper of Fe element, the addition of Fe element is controlled at 2.0~2.6 scope.
Adding of Ti can prevent from equating effect at metallic matrix with there is fragility second in the middle of coating, can improve the welding property of alloy, but low-alloyed conductivity can fall in excessive interpolation Ti element, the content of Ti element is limited in to 0.05~0.1 scope.
In the time of room temperature, the solubleness of B in copper is almost nil, can reduce specific conductivity and the thermal conductivity of copper, but its mechanical property and welding property to copper has desirable influence, B can also improve the mobility of copper-iron alloy melt, B is to add with the form of reductor in the time of copper smelting iron alloy, and unnecessary B is solid-solubilized in copper matrix can prevent hydrogen embrittlement; In the ag(e)ing process of alloy, B is also combined with Fe, form Fe3B precipitate and play certain ageing strengthening effect.Adding of B is for deoxidation, is solid-solubilized in copper matrix and prevents hydrogen embrittlement, instead of strengthen by separating out Fe3B.In giving full play to the advantageous effect of B element, should reduce B content as far as possible, to ensure the high conduction performance of alloy, the content of B element is limited to 0.01~0.03 scope.
Add micro-Na that the specific conductivity of copper is declined, but can improve the oxidation-resistance property of copper, and copper is had to desoxydatoin.Identical with the principle that limits B element, the content of Na element is limited in 0~0.05 scope.
The effect of mixed rare-earth elements Mo is mainly:
(1) deoxidation dehydrogenation: the chemically reactive of rare earth is very strong, with the avidity of the oxygen avidity much larger than copper and oxygen, and generates the rare earth oxide that fusing point is higher than copper, density ratio copper is little, receives good desoxydatoin; Rare earth and hydrogen are combined into the hydride that density is little, float up to copper liquid surface, at high temperature again decompose, and discharge hydrogen, or oxidizedly enter slag and be removed;
(2) cleaning molten: rare earth to the effect that removes of other harmful element also clearly, these dystectic rare earth compounds will keep solid state from liquid copper, to discharge together with slag, thereby reach the effect that removes detrimental impurity, rare earth especially can be removed crystal boundary impurity element significantly, impurity element has increased the significant quantity of the element such as Fe, B after removing, can increase substantially the intensity of alloy;
(3) crystal grain thinning: add Mo in alloy, obvious crystal grain thinning in fusion-casting process, improves alloy alloy plasticity after follow-up thermomechanical treatment;
(4) promote second phase particles to separate out: in alloy, add after Mo, the second phase particles (fe) of separating out in band is tiny, disperse, and size is probably at 5~20nm; In addition, can put forward heavy alloyed recrystallization temperature, thereby improve the high temperature resistance softening performance of alloy after interpolation Mo, the softening temperature of interalloy of the present invention all, more than 480 DEG C, adds appropriate mishmetal Mo, and composition range is controlled at 0.01~1.5.
In technical solution of the present invention, based on the impact of sulphur on technique and product in major ingredient impurity, its major ingredient is selected electrolytic copper No. 1, sulfur-bearing as few as possible in impurity, and will prevent punch process time because oil pollution is sneaked into S, even if deformation performance when a small amount of S also can make hot rolling sharply declines, control the content of S, workpiece cracking when hot rolling can be avoided.Conventionally, the content of S must be less than 0.0025wt%, and ideal value is to be less than 0.0015wt%.
Alloy manufacture method for down-lead bracket of the present invention comprises the steps:
(1) first by No. 1 electrolytic copper 1250~1350 DEG C of fusings, after adding the meltings such as copper iron master alloy, copper boron master alloy, sodium simple substance, titanium simple substance and mishmetal, carry out minitype vertical type semicontinuous casting, utilize mold carry out once cooling and utilize water to drench to carry out secondary cooling, make speed of cooling in the temperature range of liquidus line to 380 DEG C 80 DEG C/more than min, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are 0.01~1.5wt%;
(2) after strand heats in the temperature range of 900~1000 DEG C, make its thickness reach 6mm through hot rolling calendering, the end temp of hot rolling calendering is 700 DEG C, make grain-size be less than 50 μ m by chilling, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are 0.01~1.5wt%;
(3) hot rolled band being carried out repeatedly to cold rolling calendering, to make its thickness be 1mm, in the temperature range of 300 DEG C~600 DEG C, carry out twin-stage annealing, make the crystal grain diameter of the calendering band after annealing be less than 50 μ m, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are 0.01~1.5wt%;
(4) cold rolling calendering makes thickness reach 0.5mm, then carries out low-temperature annealing, obtains band finished product; In manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are 0.01~1.5wt%.
(5) adopt above-mentioned band to make down-lead bracket.
In manufacturing process of the present invention: alloy raw material is No. 1 electrolytic copper, copper iron master alloy, copper boron master alloy, sodium simple substance, titanium simple substance and mishmetal, adopt medium-frequency induction furnace melting.
Casting technique after raw material fusing is taking continuous casting as best, and semicontinuous casting also can.In castingprocesses in the temperature range of liquidus line to 380 DEG C, carrying out coolingly with 80 DEG C/more than min speed of cooling, during lower than 80 DEG C/min, will there is the segregation of element in speed of cooling, later hot rolling is brought to adverse influence, and cause the reduction of production efficiency; Control speed of cooling, the temperature range of preferred liquid phase line temperature to 380 DEG C; Below 380 DEG C, when casting, the length of cooling time changes the excessive segregation that alloying element can not occur.
After melt-casting, carry out hot-work.Hot worked Heating temperature should be the scope of 900~1000 DEG C, if temperature exceedes ceiling temperature, it is overheated to occur, and causes hot rolling cracking, reduces production efficiency.Carry out hot rolling in the temperature range of 900~1000 DEG C time, small segregation and cast structure will disappear, within the scope of the constituent contents such as Fe of the present invention, Ti, B, can obtain the rolled strip of homogeneous microstructure, more preferably hot rolling temperature is 950 DEG C of left and right.After hot rolling, crystal grain diameter is below 50 μ m, and crystal grain diameter is greater than 50 μ m, and cold processing ratio thereafter, the condition and range of annealing will narrow, and make deterioration in characteristics.
After hot rolling, carry out as required surfacing cut, repeatedly carry out thereafter the annealing in the temperature range of cold rolling processing and 300~600 DEG C.Adopt the twin-stage continuous annealing of low temperature after first high temperature, reach and control the object of grain-size and precipitated phase (crystal grain diameter is less than 50 μ m).Temperature is during lower than 300 DEG C, carries out the required time of structure property control longer; Exceed 600 DEG C, in the short period of time, crystal grain will become thick.If the crystallization crystal grain after annealing is greater than 50 μ m, can make the mechanical characteristicies such as tensile strength and processing characteristics reduce.Therefore make crystal grain diameter be less than 50 μ m, better crystal grain diameter is less than 25 μ m.
The annealed material obtaining, carrying out cold rolling rolling processing reaches more than 40% its amounts of thickness variation, also carry out 420 DEG C of following low-temperature annealings, obtain that tensile strength 600MBa is above, hardness 180Hv is above, specific conductivity 66%IACS is above, more than 7.0% copper-iron alloy of unit elongation.When cold processing ratio is discontented with 40%, because of the insufficient strength that work hardening produces, can not improve mechanical characteristics completely.Therefore desirable working modulus is more than 50%.In order further to carry heavy alloyed tensile strength, hardness, unit elongation, especially the characteristic such as specific conductivity, low temperature annealing process is very necessary, at the temperature of 420 DEG C, because of thermal capacity excessive, material is softened at short notice, and no matter adopt intermittent type or continous way, all easily produce the characteristic inequality of material internal.Therefore, stress relief annealed condition should be below 420 DEG C.
Embodiment:
The copper-iron alloy № 1~6 of composition as shown in table 1 (wt%),
Table 1
It should be noted that, in the fusion process of alloy, each element all has scaling loss in various degree, its burn out rate Fe:1~2%, Ti:1~3%, B:2~5%, Na:20~30%, Mo:30~50%; In the process of batching, should supply.When melting starts, first add electrolytic copper and copper iron master alloy, start heating, after its fusing, first add 1/3 copper boron master alloy, insulation 1~3min; Add afterwards titanium, sodium and rare earth, after its fusing, be incubated 3~5min, then add the copper boron master alloy of residue 2/3, after fine melt, be incubated 10min casting; Use the strand of minitype vertical type semicontinuous caster casting 70 × 180 × 1000 (mm), utilize mold carry out once cooling and utilize water to drench to carry out secondary cooling, make speed of cooling in the temperature range of liquidus line to 380 DEG C 80 DEG C/more than min., after each strand heats in the temperature range of 900~1000 DEG C, roll so that its thickness is 6mm through hot rolling thereafter, from surface and the crackle at edge evaluate hot rolling.After overpickling, the experiment material that does not observe crackle under the opticmicroscope of 50 times is evaluated as, and it is poor that the experiment material that can observe crackle is evaluated as.The end temp of hot rolling calendering is 700 DEG C, makes grain-size be controlled at 50 μ m left and right by chilling.Then carrying out cold rolling calendering, to make its thickness be 1mm, carries out twin-stage anneal in the temperature range of 300~600 DEG C, impels second phase particles to separate out raising performance, and carrying out afterwards cold rolling calendering, to make its thickness be 0.5mm again, finally carries out low-temperature annealing.
Clip test film from above obtained band, carries out the mensuration of tensile strength, hardness, unit elongation and specific conductivity, and property indices is all measured according to GB.Above obtained outcome record is in table 2.
Table 2
Obviously, this copper-iron alloy has good hot workability, is conducive to manufacture, and especially has the characteristics such as good tensile strength, hardness, unit elongation and specific conductivity, is the best materials of producing the electrical and electronic parts such as down-lead bracket; This copper-iron alloy belongs to Cu-Fe and is associated the row of golden C194.
By specific embodiment, technical solution of the present invention has been done to further illustrate above, the example providing is only exemplary applications, can not be interpreted as the one restriction to the claims in the present invention protection domain.

Claims (5)

1. a manufacture method for down-lead bracket, is characterized in that, described manufacture method comprises the following steps:
(1) first major ingredient and auxiliary material are injected to mold after 1250~1350 DEG C of meltings, in the temperature range of liquidus temperature to 380 DEG C, carry out coolingly with 80 DEG C/more than min speed of cooling, in manufacturing processed, control alloying constituent and content F e and be 2.0~2.6wt%, Ti and be 0.05~0.1wt%, B and be 0.01~0.03wt%, Na and be 0~0.05wt%, Mo and be 0.01~1.5wt%, all the other components and be Cu and inevitable impurity;
(2) by the strand obtaining, the Heating temperature below 1000 DEG C is carried out hot rolling calendering, and in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity;
(3) hot rolled band is carried out repeatedly to cold rolling calendering and 300 DEG C~600 DEG C twin-stage continuous annealings, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity;
(4) carrying out cold rolling rolling processing reaches more than 40% its amounts of thickness variation, carry out again 420 DEG C of following low-temperature annealings, obtain band finished product, in manufacturing processed, control composition content F e is that 2.0~2.6wt%, Ti are that 0.05~0.1wt%, B are that 0.01~0.03wt%, Na are that 0~0.05wt%, Mo are that 0.01~1.5wt%, all the other components are Cu and inevitable impurity;
(5) adopt above-mentioned band to make down-lead bracket.
2. manufacture method as claimed in claim 1, is characterized in that, the crystal grain diameter of controlling band in step (2) the hot rolling calendering course of processing is less than 50 μ m.
3. manufacture method as claimed in claim 1, is characterized in that, the crystal grain diameter of controlling band in step (3) in the cold rolled annealed course of processing is less than 50 μ m.
4. manufacture method as claimed in claim 1, is characterized in that, the copper-iron alloy making through step (4) also contains element and the total amount more than at least one in As, Sb, Bi, Co, Ni element and is less than 0.05wt%.
5. manufacture method as claimed in claim 4, is characterized in that, the tensile strength of described copper-iron alloy is that 600MPa is above, hardness 180HV above, specific conductivity 66%IACS is above, unit elongation is more than 7.0%.
CN201210441508.6A 2012-11-07 2012-11-07 Method for manufacturing lead frame Active CN102978430B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210441508.6A CN102978430B (en) 2012-11-07 2012-11-07 Method for manufacturing lead frame

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210441508.6A CN102978430B (en) 2012-11-07 2012-11-07 Method for manufacturing lead frame

Publications (2)

Publication Number Publication Date
CN102978430A CN102978430A (en) 2013-03-20
CN102978430B true CN102978430B (en) 2014-07-30

Family

ID=47852764

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210441508.6A Active CN102978430B (en) 2012-11-07 2012-11-07 Method for manufacturing lead frame

Country Status (1)

Country Link
CN (1) CN102978430B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107282631B (en) * 2017-07-10 2019-03-08 东北大学 A method of in specific temperature area, forced plasticity deforming prepares copper alloy with high strength and high conductivity

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1678762A (en) * 2002-05-15 2005-10-05 蒂森克鲁伯钢铁股份公司 Non-grain oriented electrical steel strip or electrical steel sheet and method for producing the same
CN101914701A (en) * 2010-08-26 2010-12-15 中铝华中铜业有限公司 Lead frame material and method for processing strip made of same

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1678762A (en) * 2002-05-15 2005-10-05 蒂森克鲁伯钢铁股份公司 Non-grain oriented electrical steel strip or electrical steel sheet and method for producing the same
CN101914701A (en) * 2010-08-26 2010-12-15 中铝华中铜业有限公司 Lead frame material and method for processing strip made of same

Also Published As

Publication number Publication date
CN102978430A (en) 2013-03-20

Similar Documents

Publication Publication Date Title
CN100425717C (en) Copper alloy for lead-wire frame and its production
CN100469923C (en) High temperature copper alloy for lead frame and its making process
CN101531149B (en) Preparation method of overlength Cu-Cr-Zr alloyed contact line
CN100587091C (en) Cu-Cr-Zr alloy preparation technology for contact wire
CN104178660B (en) A kind of high intensity Cu-Ni-Si alloy and preparation method thereof
CN107988512A (en) A kind of high strength and high flexibility cupro-nickel silicon cobalt system lead frame processing technology
CN105274386B (en) High-performance complex multi-element phosphor bronze alloy material and preparation method thereof
CN106756202A (en) A kind of blaster fuse frame material complicated pluralism Cu alloy material and preparation method thereof
CN108588467A (en) A kind of auri yellow gold material
CN108315581A (en) A kind of low beryllium content copper alloy and preparation method thereof of high intensity high softening temperature
CN103624415A (en) Boron-containing stannum-based lead-free solder and manufacturing method thereof
CN102978431B (en) Method for manufacturing copper-iron alloy used for lead frame
CN102978429B (en) Copper alloy for manufacturing frame
CN103421980B (en) A kind of high-strength elastic brass and preparation method thereof
CN102978430B (en) Method for manufacturing lead frame
CN104233031A (en) Microalloying AZ91 magnesium alloy with high strength and proper solderability and preparation method thereof
CN114277280B (en) Precipitation strengthening type tin brass alloy and preparation method thereof
CN113502408B (en) High-conductivity copper alloy containing tellurium and nickel and preparation method thereof
CN113969364B (en) High-strength high-conductivity copper-niobium alloy and preparation method thereof
CN102690971A (en) High-strength copper alloy strip and preparation method thereof
CN102978432B (en) Lead support used for semiconductor devices
CN101768680B (en) Composite modifier for copper alloy of lead frame
CN102983081B (en) Manufacturing method of semiconductor device composed of integrated circuit
JP2008095125A (en) Copper-alloy sheet with excellent platability for electrical and electronic parts
CN102983082B (en) Method of manufacturing integrated circuit

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP03 Change of name, title or address

Address after: 213376, No. 8, Zhongguancun Avenue, Liyang, Jiangsu, Changzhou

Patentee after: Jiangsu Jinyuan High-end Equipment Co., Ltd.

Address before: 213376, No. 2008 Ling Ling West Road, Changzhou, Jiangsu, Liyang

Patentee before: Jiangsu Jinyuan Forging Co., Ltd.