JPH03219051A - Fe-ni alloy for lead frame and its manufacture - Google Patents
Fe-ni alloy for lead frame and its manufactureInfo
- Publication number
- JPH03219051A JPH03219051A JP1408090A JP1408090A JPH03219051A JP H03219051 A JPH03219051 A JP H03219051A JP 1408090 A JP1408090 A JP 1408090A JP 1408090 A JP1408090 A JP 1408090A JP H03219051 A JPH03219051 A JP H03219051A
- Authority
- JP
- Japan
- Prior art keywords
- less
- alloy
- lead frame
- composition
- tensile strength
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 8
- 229910000990 Ni alloy Inorganic materials 0.000 title description 2
- 239000000956 alloy Substances 0.000 claims abstract description 33
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 32
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 13
- 229910052796 boron Inorganic materials 0.000 claims abstract description 10
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 10
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 10
- 229910052802 copper Inorganic materials 0.000 claims abstract description 9
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 9
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 claims abstract description 8
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 8
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 8
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 8
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 7
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 7
- 229910001122 Mischmetal Inorganic materials 0.000 claims abstract description 6
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 4
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 3
- 239000000203 mixture Substances 0.000 claims description 20
- 239000012535 impurity Substances 0.000 claims description 7
- 239000002994 raw material Substances 0.000 claims description 4
- 238000000137 annealing Methods 0.000 claims description 3
- 238000002844 melting Methods 0.000 claims description 3
- 230000008018 melting Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 11
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract description 6
- 239000010703 silicon Substances 0.000 abstract description 6
- 239000000919 ceramic Substances 0.000 abstract description 4
- 229910052759 nickel Inorganic materials 0.000 abstract description 4
- 238000007789 sealing Methods 0.000 abstract description 3
- 238000010348 incorporation Methods 0.000 abstract 1
- 230000032683 aging Effects 0.000 description 8
- 239000010955 niobium Substances 0.000 description 8
- 239000010949 copper Substances 0.000 description 7
- 239000011651 chromium Substances 0.000 description 6
- 239000010936 titanium Substances 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000004881 precipitation hardening Methods 0.000 description 3
- 230000008646 thermal stress Effects 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- -1 Z r Inorganic materials 0.000 description 2
- 238000003483 aging Methods 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229910000833 kovar Inorganic materials 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- JUWSSMXCCAMYGX-UHFFFAOYSA-N gold platinum Chemical compound [Pt].[Au] JUWSSMXCCAMYGX-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 239000003566 sealing material Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Heat Treatment Of Steel (AREA)
Abstract
Description
【発明の詳細な説明】
「産業上の利用分野」
本願発明は、多ピンIC用リードフレーム材料なととし
て好適なFe−Ni合金およびその製法に関し、特定の
元素を特定量添加ずろことにより、従来の合金よりも優
れた変形抵抗を示し、従来の合金と同等の低熱膨張性を
確保したもの、および、その製法に関するらのである。Detailed Description of the Invention "Field of Industrial Application" The present invention relates to a Fe-Ni alloy suitable as a lead frame material for multi-pin ICs and a method for producing the same, by adding a specific element in a specific amount. The present invention relates to a material that exhibits better deformation resistance than conventional alloys and has low thermal expansion comparable to that of conventional alloys, and a method for producing the same.
「従来の技術」
近年、集積度の高い大規模集積回路(LSI)や超人規
模集積回路(超L S I )なとの開発か盛んとなっ
てきているが、このようなLSIや超L S Iにおい
ては、シリコン素子が大型化し、発熱令ら多くなってき
ている。従ってノリコン素子とリードフレームとの間の
熱膨張率の差異か大きい場合は、通電発熱によるリード
フレームの膨張と収縮によりシリコン素子が熱ストレス
を受けて割れたり、亀裂を生じたりするおそれがある。"Conventional technology" In recent years, the development of highly integrated large-scale integrated circuits (LSI) and superhuman-scale integrated circuits (ultra-LSI) has become active. In I, silicon elements have become larger and generate more heat. Therefore, if the difference in thermal expansion coefficient between the silicone element and the lead frame is large, the silicon element may be subject to thermal stress due to expansion and contraction of the lead frame due to heat generated by electricity, and may break or crack.
そこでLSIや超LSI用なとのリードフレーム材料に
あっては、特にその熱膨張率をシリコン素子の熱膨張率
に近付ける必要がある。Therefore, in the case of lead frame materials for LSIs and VLSIs, it is particularly necessary to bring the coefficient of thermal expansion close to that of silicon elements.
このため従来から、リードフレーム用の材料においては
、ソリコン素子なとに作用する熱応力を緩和することを
目的とした低膨張のFe−Ni合金として、42 A
1loy(42%N1−Fe)(特開昭5511915
6号など)、コバール(29%Ni−17%co−Fe
)、および、低膨張コバール(29%Ni−13%Co
−FeX特開昭59−198741号)などが知られて
いる。For this reason, 42A has traditionally been used as a material for lead frames as a low-expansion Fe-Ni alloy for the purpose of alleviating thermal stress that acts on solicon elements.
1loy (42%N1-Fe) (JP-A-5511915
No. 6), Kovar (29%Ni-17%co-Fe)
), and low expansion Kovar (29%Ni-13%Co
-FeX JP-A-59-198741) and the like are known.
「発明が解決しようとする課題 1
ところが、最近、リードフレームの多ピン化に伴い、以
萌はインナーリートの幅か0.3〜05+++m程度で
あったものが、0.1〜0 、2 mm程度の幅になる
場合が生じてきているとと乙に、外部リードについても
細くなる傾向にある。``Problems to be solved by the invention 1 However, recently, with the increase in the number of pins in lead frames, the inner lead width has changed from 0.3 to 0.5 +++ m to 0.1 to 0.2 mm. In addition to this, there is also a tendency for external leads to become narrower.
このため、リードの材料強度か不足することから、製造
工程途中なとにおいて、運搬時やセパレータのテーピン
グ時に、あるいは、基板への接続時に、リーI・か外力
による変形を起こすごとがあり、このことが重大な問題
となりつつある。For this reason, the material strength of the lead is insufficient, and the lead may be deformed due to external force during the manufacturing process, during transportation, taping the separator, or when connecting to the board. This is becoming a serious problem.
そこで本願発明前らは、先に、特願昭63−315 G
46号明細7jF、特願甲1−164582号明細1
1F、特願平1−、172509号明細1ケなとにおい
て、Fe−N1−Go系合金に特定量のBeあるいはそ
の池の元素を添加することで高強度と低熱膨張性を確保
した合金について特許出願している。Therefore, the inventors of the present application first filed the patent application No. 63-315 G.
No. 46 Specification 7jF, Patent Application No. A1-164582 Specification 1
1F, Japanese Patent Application No. 172509 No. 1, describes an alloy in which high strength and low thermal expansion are ensured by adding a specific amount of Be or other elements thereof to a Fe-N1-Go alloy. A patent application has been filed.
これらの特許出願においては、Ni30〜55%、00
2%以下、f3c0.01−2%、M n 1%以下、
S i0.5%以下、Cu5%以1ζ、C0.1%以下
を上体と4−る組成を(fし、更に、必要に応してSや
Nを特定頃合f了することで目的を達成している。In these patent applications, Ni30-55%, 00
2% or less, f3c 0.01-2%, M n 1% or less,
The composition of Si is 0.5% or less, Cu is 5% or more, and C is 0.1% or less. Achieved.
本願発明は、先に本願発明前らが特許出願している技術
を更に発展させて前記課題を解決するためになされたら
ので、従来合金よりも硬度と引張強度に1斬れ、しかも
ノリコン素子に近い低熱膨張率を示tリードフレーム用
Fe−Ni合金およびその製法を提供することを目的と
4−る。The present invention was made in order to solve the above problems by further developing the technology for which the inventors of the present invention have previously applied for a patent, so it has better hardness and tensile strength than conventional alloys, and is close to Noricon elements. The object of the present invention is to provide a Fe--Ni alloy for lead frames that exhibits a low coefficient of thermal expansion and a method for producing the same.
「課題を解決するための手段」
請求項1に記載した発明はn記課題を解決するために、
N130−55%、Co 2%以下、B c0.01〜
2%、M n I%以ド、Si0.5%以下、Cu5%
以下、C0.1%以下を含み、0.01〜2%のA1と
0.01〜2%の’I’ iのうち、少なくと(J1種
を含み、Fe残部及び不可避不純物の組成にしたもので
ある。"Means for solving the problem" The invention stated in claim 1 solves the problem n.
N130-55%, Co 2% or less, B c0.01~
2%, M n I% or more, Si 0.5% or less, Cu 5%
Below, the composition contains 0.1% or less of C, 0.01 to 2% of A1 and 0.01 to 2% of 'I' i, including at least (J1 type), and the composition of the remaining Fe and unavoidable impurities. It is something.
請求項2に記載した発明は前記課題を解決4゛るために
、Ni30〜55%、Co2%以ド、[3eo、01〜
2%、M n 1%以下、Si 0.5%以ド、Cu5
%以下、C0.1%以下を含み、0.01〜1%のNb
と0.01−1%のMoと001〜/I%のWと0.0
1〜1%のVと0.01〜3%のCrと0.001〜0
.5%の13と0001〜1%のZrと0.001−]
%のミソツユメタルのうち、少なくとも1種以上を含み
、Fe残部及び不可避不純物の組成にしたしのである。In order to solve the above-mentioned problem, the invention as set forth in claim 2 uses Ni30 to 55%, Co2% or more, [3eo, 01 to
2%, Mn 1% or less, Si 0.5% or more, Cu5
% or less, including C0.1% or less, and 0.01 to 1% Nb
and 0.01-1% Mo and 001~/I% W and 0.0
1-1% V and 0.01-3% Cr and 0.001-0
.. 5% 13 and 0001~1% Zr and 0.001-]
% of MiSotsuyu metal, and has a composition of Fe remainder and unavoidable impurities.
請求項3に記載した発明は前記課題を解決するために、
Ni30〜55%、Co2%以下、r3e0.01〜2
%、Mn1%以下、Si 0.5%以下、(305%以
下、C0.1%以下を含み、0.01〜2%のA1と0
.01〜2%の′■゛]のうち、少なくとし1種を含み
、0.01〜1%のNbと0.01〜4%のMoと0.
01〜4%のWと0.01〜1%のVと0.01〜3%
のCrと0.001〜0.5%の13と0.001〜1
%のZrと0.001〜1%のミソツユメタルのうち、
少なくとし1種以上を含み、F e残部及び不可避不純
物の組成にしたしのである。In order to solve the above problem, the invention described in claim 3 has the following features:
Ni30-55%, Co2% or less, r3e0.01-2
%, Mn 1% or less, Si 0.5% or less, (including 305% or less, C 0.1% or less, 0.01 to 2% A1 and 0
.. 0.01 to 2% of Nb, 0.01 to 1% of Mo, and 0.01 to 1% of Mo.
01-4% W, 0.01-1% V and 0.01-3%
of Cr and 0.001-0.5% of 13 and 0.001-1
% of Zr and 0.001~1% of Misotsuyu metal,
The composition contains at least one or more kinds of Fe, the remainder of Fe, and unavoidable impurities.
請求項4に記載した発明は前記課題を解決するために、
請求項1又は請求項2又は請求項3に記載した組成を満
たすように原材料を配合し、溶解して得たインゴットを
目的の形状になるまで塑性加圧と焼鈍処理を施し、最終
塑性加工後に300〜700℃の温度域において時効す
るものである。In order to solve the above problem, the invention described in claim 4 has the following features:
The raw materials are blended to satisfy the composition described in claim 1, claim 2, or claim 3, and the ingot obtained by melting is subjected to plastic pressing and annealing treatment until the desired shape is obtained, and after final plastic working. It is aged in a temperature range of 300 to 700°C.
]−作用 」
F eとNiとCo&MnとSiとCuとCを所定置き
(fする低膨張率の合金に、13 eを少9添加するこ
とで高強度になるとともに、[(eの添加噴か少量て済
むのて、合金の主成分は低膨張率の合金であり、このた
め、リードフレーム用の材料として好適な熱膨張率が確
保される。更に、前記組成に、A1とT iの少なくと
も一方を所定量添加することで析出硬化による強化がな
され、次いてNbとM。]-Effect By placing Fe, Ni, Co&Mn, Si, Cu, and C (f) into an alloy with a low expansion coefficient, adding a small amount of 13e increases its strength. Since only a small amount is required, the main component of the alloy is an alloy with a low coefficient of expansion, which ensures a suitable coefficient of thermal expansion as a material for a lead frame.Furthermore, in the above composition, at least one of A1 and Ti is added. Strengthening by precipitation hardening is achieved by adding a predetermined amount of one of them, followed by Nb and M.
と〜■とVとCrと13とZrとミソツユメタルの少な
くとし1種を特定n1添加することで固溶強化かなされ
て強化される。By adding specific n1 of at least one of the following: and~■, V, Cr, 13, Zr, and misotsuyu metal, it is strengthened by solid solution strengthening.
また、萌記谷組成とした合金に300〜700℃て熱処
理を施すと、引張り強さの制御が可能になり、時効硬化
する。Further, when an alloy having a Moekiya composition is heat treated at 300 to 700°C, the tensile strength can be controlled and age hardening occurs.
以下に本願発明を更に詳細に説明する。The present invention will be explained in more detail below.
本願発明の合金においては、Niにメタル)を30−5
5%、(10(コバルト)を2%以下、[3e(ヘリリ
ウ1. )を0.01〜2%、M II(7ンガン)を
1%以下、Si(ケイ素)を0.5%以下、Cu(銅)
を5%以下、C(炭素)を0.1%以下含Hしている合
金か主体となっている。In the alloy of the present invention, Ni is added to 30-5
5%, (10 (cobalt) 2% or less, 3e (Heliru 1.) 0.01 to 2%, M II (7 ngan) 1% or less, Si (silicon) 0.5% or less, Cu (copper)
It is mainly an alloy containing H of 5% or less and C (carbon) of 0.1% or less.
そして前記組成を主体とする合金に、0.01〜2%の
Al(アルミニウム)と0.01〜2%の’I”i(チ
タン)とを添加している。0.01 to 2% of Al (aluminum) and 0.01 to 2% of 'I''i (titanium) are added to the alloy mainly having the above composition.
また、1ji7記組成を主体とする合金に、0.0I〜
1%のNb(ニオブ)と001〜4%のMo(モリブデ
ン)と0.01〜4%のW(タングステン)と0.01
−1%のv(バナジウム)と0.01〜3%v)cr(
クロム)と0.001〜0.5%のB(ホウ素)と0.
001−1%のZr(ジルコニウム)と0.001〜1
%のミソツユメタル(混合希土類金属)のう1″)、少
なくとも1種以上を独自に、あるいは、+”+:i記A
1とTiの少なくともIIと共に添加している。In addition, in alloys mainly having the composition 1ji7, 0.0I~
1% Nb (niobium), 001~4% Mo (molybdenum), 0.01~4% W (tungsten), and 0.01
-1% v(vanadium) and 0.01-3% v)cr(
chromium), 0.001 to 0.5% B (boron), and 0.001 to 0.5% B (boron).
001-1% Zr (zirconium) and 0.001-1
% Misotsuyu metal (mixed rare earth metal) 1"), at least one or more independently, or +"+: i A
1 and Ti together with at least II.
前記組成において、NiとCoとCuの含?Tffiを
前記範囲外にすると、リードフレーム材料が適用される
シリコン素子等の熱膨張率に適応した熱膨張率か得られ
なくなるために好ましくない。In the above composition, does it contain Ni, Co, and Cu? If Tffi is outside the above range, it is not preferable because the lead frame material will not be able to obtain a coefficient of thermal expansion that is compatible with the coefficient of thermal expansion of the silicon element, etc. to which it is applied.
r3cの含有量を0.01%未満とすると、他の添加元
素の協力を得ても目的とする強度は得られず不都合であ
り、Beの含14 FBが2.0%を越える場合、強度
向上の割に高価なりeの使用量か多くなってコストが高
くなり、不適当である。If the r3c content is less than 0.01%, it is inconvenient that the desired strength cannot be obtained even with the cooperation of other additive elements, and if the Be content exceeds 2.0%, the strength will decrease. Despite the improvements, it is expensive and the amount of e used increases, resulting in high costs, making it unsuitable.
Siは脱酸剤として用いるが、含ffff1が0.5%
を越えると合金を脆化させるので不都合であり、Mnは
鍛造性を向上させるとともに脱酸剤として用いるが、含
有量が1%を越えると加工性を悪化させるので好ましく
ない。Si is used as a deoxidizing agent, but the ffff1 content is 0.5%.
If the content exceeds 1%, the alloy becomes brittle, which is disadvantageous. Mn improves forgeability and is used as a deoxidizing agent, but if the content exceeds 1%, it deteriorates workability, which is not preferable.
Cは0.1%を越えると加工性を悪化させる。When C exceeds 0.1%, workability deteriorates.
A1とT iの各含有量は下限値より少なくては目的と
する強度が得られず、」二限値を越えろ場合は強度向上
の割にコスト高となり、好ましい熱膨張係数ら得られな
い。If the content of each of A1 and Ti is less than the lower limit value, the desired strength cannot be obtained, and if it exceeds the lower limit value, the cost becomes high despite the improvement in strength, and a preferable coefficient of thermal expansion cannot be obtained.
NbとMoとWとVとCrとBとZ rとミッシュメタ
ルの各含有量は下限値より少なくては目的とする強度が
得られず、上限値を越える場合は強度向上の割にコスト
高となり、好ましい熱膨張係数ら得られない。If the content of Nb, Mo, W, V, Cr, B, Z r, and misch metal is less than the lower limit, the desired strength cannot be obtained, and if it exceeds the upper limit, the cost will be high despite the strength improvement. Therefore, a preferable coefficient of thermal expansion cannot be obtained.
前記合金を製造するには、まず、前記の組成になるよう
に原材料を配合した後に、不純物の混入を避ける目的で
Arガスなどの雰囲気中で真空溶解を行−)で前記組成
のインゴットを得る。To produce the alloy, first, raw materials are blended to have the above composition, and then vacuum melting is performed in an atmosphere such as Ar gas to avoid contamination with impurities to obtain an ingot with the above composition. .
次いでこのインゴットを+ 200〜1400°C−ご
鍛造加I L、目的の形状、例えば目的の板厚になるま
で、好ましくは加工率70%以下で行う圧延加Tと、8
00〜1100°Cで行う焼鈍処理を必要回数繰り返し
施す。そして、最終圧延加工時に加工率を好ましくは5
0%以下程度に設定し、最終圧延後に時効硬化処理を目
的として、300〜700℃の温度域において、望まし
くは5時間以内の熱処理を行い、所望の厚さの板材を得
る。Next, this ingot is forged at +200 to 1400°C, rolled to the desired shape, for example, to the desired thickness, preferably at a processing rate of 70% or less, and then
The annealing treatment at 00 to 1100°C is repeated as many times as necessary. Then, the processing rate is preferably set to 5 during the final rolling process.
0% or less, and after the final rolling, a heat treatment is performed in a temperature range of 300 to 700° C., preferably within 5 hours, for the purpose of age hardening treatment, to obtain a plate material with a desired thickness.
前記時効処理温度において300℃以下では、析出粒子
が小さtぎて析出硬化が進まずに未時効となり、700
℃以上では時効により強度がピークになるまでの熱処理
時間が短かすぎて温度コント〔1−ルが困難であり、そ
れを越えると析出粒子か人きくなりすぎて十分な析出硬
化か期待でき4゛に強度を落としてしまう可能生らある
。If the aging treatment temperature is below 300°C, the precipitated particles will be too small and precipitation hardening will not proceed, resulting in unaged 700°C.
At temperatures above ℃, the heat treatment time until the strength reaches its peak due to aging is too short, making temperature control difficult; above this temperature, the precipitate particles become too sensitive and sufficient precipitation hardening cannot be expected. There is a possibility that the strength will be reduced.
以上説明したような製造方法で前記組成の合金を製造す
るならば、従来の合金よりも強度が高く変形抵抗が高い
とと乙に、ノリコン素子やセラミック封止材料の熱膨張
率に近い熱膨張率のリードフレーム用材料を得ることが
できる。しかし前記合金は時効処理の温度と時間を調節
することにより引張強さを調節できるので、所望の強さ
のり一トフレーム材料を得ることができる。更に、Be
の添加量が少量でら引張強度の向上効果が得られるので
、高価なりeの使用量が少なくて済み、低コストで製造
できる効果がある。If an alloy with the above composition is manufactured using the manufacturing method described above, it will have higher strength and deformation resistance than conventional alloys, and will also have a thermal expansion coefficient close to that of Noricon elements and ceramic sealing materials. It is possible to obtain materials for lead frames with high yields. However, since the tensile strength of the alloy can be adjusted by adjusting the temperature and time of the aging treatment, it is possible to obtain a glued frame material with a desired strength. Furthermore, Be
Since the effect of improving the tensile strength can be obtained with a small amount of addition, the amount of expensive e used can be reduced, resulting in an effect that production can be carried out at low cost.
「実施例」
以Fに示す第1表〜第4表の組成になるように各々原材
料を配合し、谷間合物をArガスを含む80Torrの
真空雰囲気において溶解してインゴットを作成し、次い
てこのインゴットに+ 200〜1400℃で熱間鍛造
加工を施し、次いて、加工率70%以下で行う圧延加工
と800〜1100℃に加熱後に徐冷する焼鈍処理とを
繰り返し行い、最終圧延加工を加工率50%以下で行っ
て圧延加工を終了し、次いで、500℃に2時j111
加熱する時効処理を行って試料No1〜92の板状の試
験片を得た。"Example" Raw materials were blended to have the compositions shown in Tables 1 to 4 below, and the valley compound was melted in a vacuum atmosphere of 80 Torr containing Ar gas to create an ingot. This ingot was subjected to hot forging at +200 to 1400°C, then rolled at a processing rate of 70% or less, and annealed by heating to 800 to 1100°C and then gradually cooled, followed by final rolling. The rolling process was completed at a processing rate of 50% or less, and then heated to 500°C for 2 hours.
A heating treatment was performed to obtain plate-shaped test pieces of samples Nos. 1 to 92.
h試験片の引張強度(kg/ mm2)と硬度(Ilv
)と・ト均熱膨張係数(30〜300℃、x I O−
8/’C)をdlす定し、その結果を第1表〜第4表に
示す。h Tensile strength (kg/mm2) and hardness (Ilv) of test piece
) and ・T uniform thermal expansion coefficient (30-300℃, x I O-
8/'C) was determined as dl, and the results are shown in Tables 1 to 4.
(以下、余白)
第1表ないし第・1表に示す結果から、A1とTiの金
白−’+tに関し、本願発明で限定した範囲か適切であ
ることか明らかになるととらに、NbとMOとWとVと
Crと+3とZrとミッシュメタルの含UNに関し、本
願発明で限定した範囲か適切であることか明らかとなっ
た。(Hereinafter, blank space) From the results shown in Tables 1 and 1, it becomes clear whether the range limited by the present invention is appropriate for A1 and Ti gold platinum-'+t, and it is also clear that Nb and MO It has become clear that the ranges limited by the present invention are appropriate with respect to the UN containing W, V, Cr, +3, Zr, and misch metal.
方、前記の手順で製造した発明品の試料について、時効
処理時間と引張り強さの関係を求めた。On the other hand, the relationship between the aging treatment time and the tensile strength was determined for the samples of the invention products manufactured by the above procedure.
その結果を第1図に示す。The results are shown in FIG.
第1図から明らかなように、時効処理の温度が300℃
の場合、処理時間の経過とともに引張強度は援やかなカ
ーブで一ト昇し、処理時間5時間程度でピークに向かい
、500℃の場合、引張強さのピークは2時間程度に短
縮され、700°Cの場合、ピークは1時間程度に短縮
されるが1時間経過後の引張強度は減少している。As is clear from Figure 1, the aging treatment temperature was 300°C.
In the case of 500°C, the tensile strength increases in a gentle curve as the processing time progresses, reaching a peak after about 5 hours of processing time, and in the case of 500°C, the peak tensile strength is shortened to about 2 hours, In the case of °C, the peak is shortened to about 1 hour, but the tensile strength after 1 hour has decreased.
第1図に示4゛結果から鑑みて本願発明方法では時効処
理温度を300〜700℃の範囲に限定しノこ。In view of the results shown in FIG. 1, in the method of the present invention, the aging treatment temperature is limited to a range of 300 to 700°C.
1発明の効果j
以上説明したように本願発明によれば、F cとNiと
co、l!:MnとSiとCuとCを所定令含存する低
熱膨張率の合金に、Beを少量添加し、更に、AlとT
iの少なくとも1種、または、NbとMoとWとVとC
rとBとZrとミッシュメタルの少なくとも1種を添加
することで高強度にしたので、ノリコン素子や封着用セ
ラミックなどに近い熱膨張率を維持した上に、従来より
6硬度と引張強度に優れた変形抵抗の大きな合金を提供
することができる。1 Effects of the Invention j As explained above, according to the present invention, F c, Ni, co, l! : A small amount of Be is added to an alloy with a low thermal expansion coefficient containing Mn, Si, Cu, and C in a predetermined age, and further Al and T are added.
At least one of i, or Nb, Mo, W, V, and C
It has high strength by adding at least one of r, B, Zr, and misch metal, so it maintains a thermal expansion coefficient close to that of Noricon elements and sealing ceramics, and has superior 6 hardness and tensile strength than conventional products. It is possible to provide an alloy with high deformation resistance.
従って本願発明によれば、ソリコン素子や封着用セラミ
ックに熱履歴による熱ストレスをかけることがないとと
もに、リードが外力による変形を起こしにくい優れたリ
ードフレーム用合金を提供することができる。Therefore, according to the present invention, it is possible to provide an excellent alloy for lead frames that does not apply thermal stress due to thermal history to the solicon elements or sealing ceramics, and whose leads are less susceptible to deformation due to external forces.
一方、前記組成とした合金に、300〜700℃で熱処
理を施すと、時効硬化させることができるので、時効条
件の選定により引張り強さなどの値の制御が可能になり
、所望の引張強さと硬度とを有するリードフレーム用に
好適な合金を得ることかてきる。On the other hand, if the alloy with the above composition is heat treated at 300 to 700°C, it can be age hardened, so it is possible to control values such as tensile strength by selecting aging conditions, and achieve the desired tensile strength and It is possible to obtain an alloy suitable for lead frames having hardness.
第1図は試験片の引張強さと時効処理時間の関係を示・
1−グラフである。Figure 1 shows the relationship between the tensile strength of the test piece and the aging treatment time.
1- It is a graph.
Claims (1)
以下 Be0.01〜2% Mn1%以下 Si0.5%以下 Cu5%以下 C0.1%以下を含み、 0.01〜2%のAlと 0.01〜2%のTiのうち、少なくとも1種を含み、 Fe残部及び不可避不純物 の組成を有するリードフレーム用Fe−Ni合金。 (2)Ni30〜55% Co2%以下 Be0.01〜2% Mn1%以下 Si0.5%以下 Cu5%以下 C0.1%以下を含み、 0.01〜1%のNbと 0.01〜4%のMoと 0.01〜4%のWと 0.01〜1%のVと 0.01〜3%のCrと 0.001〜0.5%のBと 0.001〜1%のZrと 0.001〜1%のミッシュメタルのうち、少なくとも
1種以上を含み、 Fe残部及び不可避不純物 の組成を有するリードフレーム用Fe−Ni合金。 (3)Ni30〜55% Co2%以下 Be0.01〜2% Mn1%以下 Si0.5%以下 Cu5%以下 C0.1%以下を含み、 0.01〜2%のAlと 0.01〜2%のTiのうち、少なくとも1種を含み、 0.01〜1%のNbと 0.01〜4%のMoと 0.01〜4%のWと 0.01〜1%のVと 0.01〜3%のCrと 0.001〜0.5%のBと 0.001〜1%のZrと 0.001〜1%のミッシュメタルのうち、少なくとも
1種以上を含み、 Fe残部及び不可避不純物 の組成を有するリードフレーム用Fe−Ni合金。 (4)請求項1又は請求項2又は請求項3に記載した組
成を満たすように原材料を配合し、溶解して得たインゴ
ットを目的の形状になるまで塑性加工と焼鈍処理を施し
、最終塑性加工後に、300〜700℃の温度域におい
て時効することを特徴とするリードフレーム用Fe−N
i合金の製法。[Claims] (1) Ni 30-55% (weight %, the same applies hereinafter) Co 2%
Below Be 0.01-2% Mn 1% Si 0.5% Cu 5% C 0.1% or less, At least one of 0.01-2% Al and 0.01-2% Ti An Fe-Ni alloy for lead frames having a composition including: Fe balance and unavoidable impurities. (2) Ni 30-55% Co 2% or less Be 0.01-2% Mn 1% or less Si 0.5% or less Cu 5% or less C 0.1% or less, including 0.01-1% Nb and 0.01-4% Mo, 0.01~4% W, 0.01~1% V, 0.01~3% Cr, 0.001~0.5% B, and 0.001~1% Zr. An Fe-Ni alloy for a lead frame, which contains at least one kind of misch metal in an amount of 0.001 to 1%, and has a composition of Fe balance and unavoidable impurities. (3) Ni 30-55% Co 2% or less Be 0.01-2% Mn 1% or less Si 0.5% or less Cu 5% or less C 0.1% or less, 0.01-2% Al and 0.01-2% Contains at least one of Ti, 0.01-1% Nb, 0.01-4% Mo, 0.01-4% W, 0.01-1% V and 0.01 Contains at least one of ~3% Cr, 0.001~0.5% B, 0.001~1% Zr, and 0.001~1% misch metal, with the remainder of Fe and unavoidable impurities An Fe-Ni alloy for lead frames having the composition. (4) The raw materials are blended to satisfy the composition described in claim 1, claim 2, or claim 3, and the ingot obtained by melting is subjected to plastic working and annealing treatment until the desired shape is obtained, and the final plastic Fe-N for lead frames that is aged in a temperature range of 300 to 700°C after processing
Production method of i-alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1408090A JPH03219051A (en) | 1990-01-24 | 1990-01-24 | Fe-ni alloy for lead frame and its manufacture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1408090A JPH03219051A (en) | 1990-01-24 | 1990-01-24 | Fe-ni alloy for lead frame and its manufacture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03219051A true JPH03219051A (en) | 1991-09-26 |
Family
ID=11851129
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1408090A Pending JPH03219051A (en) | 1990-01-24 | 1990-01-24 | Fe-ni alloy for lead frame and its manufacture |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03219051A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1063304A1 (en) * | 1999-06-22 | 2000-12-27 | Imphy Ugine Precision | Masking device for a colour flat screen cathode ray tube comprising a supporting frame for planar mask and planar mask |
-
1990
- 1990-01-24 JP JP1408090A patent/JPH03219051A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1063304A1 (en) * | 1999-06-22 | 2000-12-27 | Imphy Ugine Precision | Masking device for a colour flat screen cathode ray tube comprising a supporting frame for planar mask and planar mask |
| FR2795431A1 (en) * | 1999-06-22 | 2000-12-29 | Imphy Ugine Precision | FLAT SCREEN COLOR VIEWING CATHODIC TUBE MASKING DEVICE, OF THE TYPE INCLUDING A SUPPORT FRAME FOR TENDERED SHADOW MASK AND TENDER SHADOW MASK |
| US6420054B1 (en) | 1999-06-22 | 2002-07-16 | Imphy Ugine Precision | Masking device for a color cathode-ray display tube with a flat screen, of the type comprising a support frame for a tensioned shadowmask, and tensioned shadowmask |
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