JPH0133943B2 - - Google Patents
Info
- Publication number
- JPH0133943B2 JPH0133943B2 JP58139492A JP13949283A JPH0133943B2 JP H0133943 B2 JPH0133943 B2 JP H0133943B2 JP 58139492 A JP58139492 A JP 58139492A JP 13949283 A JP13949283 A JP 13949283A JP H0133943 B2 JPH0133943 B2 JP H0133943B2
- Authority
- JP
- Japan
- Prior art keywords
- cover
- case
- welding
- aluminum
- filler metal
- 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.)
- Expired
Links
- 238000005219 brazing Methods 0.000 claims description 14
- 238000003466 welding Methods 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 10
- 229910000838 Al alloy Inorganic materials 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 239000010703 silicon Substances 0.000 claims description 6
- 239000004065 semiconductor Substances 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 description 13
- 239000002184 metal Substances 0.000 description 13
- 239000000945 filler Substances 0.000 description 12
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 5
- 239000000956 alloy Substances 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910003023 Mg-Al Inorganic materials 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/02—Manufacture or treatment of semiconductor devices or of parts thereof
- H01L21/04—Manufacture or treatment of semiconductor devices or of parts thereof the devices having at least one potential-jump barrier or surface barrier, e.g. PN junction, depletion layer or carrier concentration layer
- H01L21/50—Assembly of semiconductor devices using processes or apparatus not provided for in a single one of the subgroups H01L21/06 - H01L21/326, e.g. sealing of a cap to a base of a container
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/28—Selection of soldering or welding materials proper with the principal constituent melting at less than 950 degrees C
- B23K35/286—Al as the principal constituent
Description
技術分野
本発明は、アルミニウム合金パツケージの気密
封止法に関する。
従来技術と問題点
マイクロ波用アンプなどに使用する金属パツケ
ージは、従来、ステンレス鋼などの鉄系材料を使
用していたが、アンプの高出力化、軽量化の要求
を満足させることができない欠点があつた。これ
に対してアルミニウム系材料は熱伝導が良好で、
しかも軽量な利点を有するが、反面、パツケージ
のケースとカバーとをレーザー溶接するときに、
溶接部は冷却速度が大きすぎるので、急冷されて
クラツクを生じ易く、パツケージの気密封止を保
てない欠点があつた。
発明の目的
本発明の目的は上記欠点を解消したアルミニウ
ム合金パツケージの製法を提供することである。
発明の構成
本発明の上記目的は、アルミニウム合金のケー
スとカバーとからなる半導体パツケージの製法で
あつて、ケースとカバーとを気密封止するため
に、ケースとカバーとの間にけい素4.0〜12.5重
量%を含み、不可避不純物を除いて残部がアルミ
ニウムよりなるアルミニウムろう材を、溶接面よ
り突出させて挿入してレーザー溶接することを特
徴とするアルミニウム合金パツケージの製法によ
つて達成することができる。
実施例
第1図は半導体パツケージの概略を示し、第2
図はパツケージのケース1とカバー2との間にろ
う材3を挿入した溶接部を拡大して示す。この実
施例では、ケースおよびカバーはJISH4000記載
の合金番号A5052(2.2〜2.8%Mg−Al)および
A1100(99%Al)からそれぞれなる。なおこの場
合は、上記組合を用いたが、たとえばA6061(0.8
〜1.2%Mg−Al)などの種々のアルミ合金の使用
が可能である。溶接条件は、平均出力250〜350W
のパルスYAGレーザを使用し、パルス幅4〜6
mm/s、パルスレート15〜20P/sのビームを、
アルゴン雰囲気中で溶接部のろう材に照射した。
また溶接速度は4〜6mm/sで行つた。
ろう材は、けい素含量を0〜12.5重量%の範囲
で変化させ、かつ厚みを0〜1000μmのの範囲で
変化させ、これに、ビーム径0.3mmφおよび0.7mm
φのビームを照射した。なお溶接肉盛りの影響を
調べる目的でろう材を溶接面より0.5mm突出させ、
または突出させないでビーム径0.3mmφで溶接し
た。前者の結果を第1表に、後者の結果を第2表
に示す。またレーザビーム径を0.7mmφとし、ろ
う材を0.5mm突出させて溶接した結果を第3表に
示す。これらの表における溶接結果はクラツク発
生が無い場合を良(〇)、有する場合を不可(×)
とした。またビーム径に対して厚すぎて溶接は十
分に行なえるが強度的に不足する場合を可(△)
として表示した。
第1および第2表から明かなように、ろう材を
突出させて配置することにより、肉盛り効果を生
じ、ろう材の厚みが薄い場合にもクラツクのない
良好な溶接が可能となる。
けい素含量4.0〜12.5重量%のアルミニウムろ
う材を使用した溶接部は、X線マイクロアナライ
ザにより、熱間強度の高いAlSi固溶合金となつ
ていることが判明した。
TECHNICAL FIELD The present invention relates to a method for hermetically sealing an aluminum alloy package. Conventional technology and problems Metal packages used in microwave amplifiers have traditionally been made of iron-based materials such as stainless steel, but they have the drawback of not being able to meet the demands for higher output and lighter weight amplifiers. It was hot. On the other hand, aluminum-based materials have good thermal conductivity,
Moreover, it has the advantage of being lightweight, but on the other hand, when laser welding the package case and cover,
Since the cooling rate of the welded portion is too high, cracks are likely to occur due to rapid cooling, and the package cannot be kept airtight. OBJECTS OF THE INVENTION It is an object of the present invention to provide a method for producing an aluminum alloy package that eliminates the above-mentioned drawbacks. Structure of the Invention The above-mentioned object of the present invention is to provide a method for manufacturing a semiconductor package consisting of an aluminum alloy case and a cover, in which silicon 4.0~ This can be achieved by an aluminum alloy package manufacturing method characterized by inserting an aluminum brazing filler metal containing 12.5% by weight, the remainder of which is aluminum except for unavoidable impurities, so as to protrude from the welding surface and laser welding it. can. Embodiment Figure 1 shows an outline of a semiconductor package, and Figure 2 shows an outline of a semiconductor package.
The figure shows an enlarged welded portion where a brazing material 3 is inserted between a case 1 and a cover 2 of the package. In this example, the case and cover are alloy number A5052 (2.2~2.8% Mg-Al) listed in JISH4000 and
Each consists of A1100 (99% Al). In this case, the above combination was used, but for example A6061 (0.8
Various aluminum alloys can be used, such as ~1.2% Mg-Al). Welding conditions are average output 250~350W
using a pulsed YAG laser with a pulse width of 4 to 6
mm/s, pulse rate 15-20P/s beam,
The filler metal in the weld was irradiated in an argon atmosphere.
The welding speed was 4 to 6 mm/s. The silicon content of the brazing filler metal was varied in the range of 0 to 12.5% by weight, and the thickness was varied in the range of 0 to 1000 μm, and the beam diameters were 0.3 mmφ and 0.7 mm.
A beam of φ was irradiated. In addition, in order to investigate the effect of weld build-up, the filler metal was made to protrude 0.5 mm from the weld surface.
Or welded with a beam diameter of 0.3mmφ without protruding. The former results are shown in Table 1, and the latter results are shown in Table 2. Table 3 shows the results of welding with the laser beam diameter set to 0.7 mmφ and the brazing filler metal protruding 0.5 mm. The welding results in these tables are rated good (〇) if there is no cracking, and poor (x) if there is.
And so. In addition, cases where the thickness is too thick for the beam diameter and sufficient welding can be performed, but the strength is insufficient (△)
It was displayed as As is clear from Tables 1 and 2, by arranging the brazing filler metal in a protruding manner, a build-up effect is produced and good crack-free welding is possible even when the thickness of the brazing filler metal is thin. An X-ray microanalyzer revealed that the welded part using an aluminum brazing filler metal with a silicon content of 4.0 to 12.5% by weight was an AlSi solid solution alloy with high hot strength.
【表】【table】
【表】
ろう材のけい素含量が4.0重量%より少ないと、
溶接部にクラツクが発生し易い。これは溶接部に
できるAlSi固溶合金中のSi量が少なくて十分な
熱間強度をもちえないためである。また12.5重量
%を超えると、ろう材自身が硬くなつて脆くなる
ので、ろう材の薄板を製造することが困難とな
り、好ましくない。ろう材の厚みが1000μmを超
えると、ビーム径の0.3mmφに対して厚すぎるの
で、溶接時に溶融する部分がろう材のみとなり十
分な溶接が得られない。しかし、ビーム径を0.7μ
mとすれば、表3に示す如く溶接が良好に行なわ
れ、かつクラツクの発生もない。しかし、1000μ
mより厚い場合は、ビーム径をさらに大きくしな
いと良好な結果が得られないので、実用的でな
い。[Table] If the silicon content of the brazing filler metal is less than 4.0% by weight,
Cracks are likely to occur in welded parts. This is because the amount of Si in the AlSi solid solution alloy formed in the weld is too small to have sufficient hot strength. Moreover, if it exceeds 12.5% by weight, the brazing material itself becomes hard and brittle, making it difficult to produce a thin plate of the brazing material, which is not preferable. If the thickness of the filler metal exceeds 1000 μm, it is too thick for the beam diameter of 0.3 mmφ, and only the filler metal will be melted during welding, making it impossible to obtain sufficient welding. However, the beam diameter is 0.7μ
m, welding is performed well as shown in Table 3, and no cracks occur. However, 1000μ
If it is thicker than m, good results cannot be obtained unless the beam diameter is further increased, which is not practical.
【表】
ビーム径を0.3mmφとするとき、ろう材の厚み
は200〜600μmとすることが最も好ましい。ケー
スおよびカバーの材料がJIS H4000記載の合金番
号A5052、A6061、A1100などのアルミニウム合
金であるとき、挿入材としてけい素含量4.0〜
12.5重量%のろう材薄板を使用し、溶接面より
0.5mm突出させて、上記の好ましい条件で肉盛り
溶接したパツケージは、ヘリウム漏洩試験におい
て10-10atm.c.c./sより少ない漏洩量を示し十分
な気密性を有していた。
発明の効果
本発明によつて、アルミニウム合金材料のケー
スとカバーとから、実用上まつたく問題のない軽
量かつ熱伝導の良好な気密封止パツケージを安定
に、信頼性よく製造することができる。[Table] When the beam diameter is 0.3 mmφ, the thickness of the brazing material is most preferably 200 to 600 μm. When the material of the case and cover is aluminum alloy such as alloy number A5052, A6061, A1100 listed in JIS H4000, the silicon content as insert material is 4.0~
Using a thin plate of 12.5% brazing filler metal, from the welding surface
The package, which was protruded by 0.5 mm and overlay welded under the above preferable conditions, showed a leakage amount of less than 10 -10 atm.cc/s in a helium leak test and had sufficient airtightness. Effects of the Invention According to the present invention, it is possible to stably and reliably manufacture a lightweight, airtight package with good thermal conductivity and no practical problems from a case and cover made of an aluminum alloy material.
第1図は半導体パツケージの略斜視図であり、
第2図はケースとカバーとの間の溶接部の拡大断
面図である。
1……ケース、2……カバー、3……ろう材。
FIG. 1 is a schematic perspective view of a semiconductor package;
FIG. 2 is an enlarged sectional view of the weld between the case and the cover. 1...Case, 2...Cover, 3...Brazing material.
Claims (1)
る半導体パツケージの製法であつて、ケースとカ
バーとを気密封止するために、ケースとカバーと
の間に、けい素4.0〜12.5重量%を含み、不可避
不純物を除いて残部がアルミニウムよりなるアル
ミニウムろう材を、溶接面より突出させて、挿入
し、レーザー溶接することを特徴とする、アルミ
ニウム合金パツケージの製法。 2 アルミニウムろう材が厚み100〜1000μmで
ある、特許請求の範囲第1項記載の製法。[Scope of Claims] 1. A method for manufacturing a semiconductor package consisting of an aluminum alloy case and a cover, in which 4.0 to 12.5 weight of silicon is added between the case and the cover in order to hermetically seal the case and the cover. %, the remainder of which is aluminum except for unavoidable impurities, is inserted so as to protrude from the welding surface, and laser welded. 2. The manufacturing method according to claim 1, wherein the aluminum brazing material has a thickness of 100 to 1000 μm.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58139492A JPS6031247A (en) | 1983-08-01 | 1983-08-01 | Manufacture of aluminum alloy package |
EP83307418A EP0117352A1 (en) | 1983-02-24 | 1983-12-06 | A process for welding aluminium-based elements and a welded assembly |
US07/012,156 US4760240A (en) | 1983-02-24 | 1987-02-09 | Process for laser welding of aluminum based elements |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58139492A JPS6031247A (en) | 1983-08-01 | 1983-08-01 | Manufacture of aluminum alloy package |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6031247A JPS6031247A (en) | 1985-02-18 |
JPH0133943B2 true JPH0133943B2 (en) | 1989-07-17 |
Family
ID=15246520
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58139492A Granted JPS6031247A (en) | 1983-02-24 | 1983-08-01 | Manufacture of aluminum alloy package |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6031247A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE68926211T2 (en) * | 1988-10-28 | 1996-11-07 | Sumitomo Electric Industries | Carrier for a semiconductor device |
US5519184A (en) * | 1994-05-20 | 1996-05-21 | Litton Systems, Inc. | Reusable laser welded hermetic enclosure and method |
JP5169548B2 (en) * | 2008-07-03 | 2013-03-27 | トヨタ自動車株式会社 | Weld penetration depth evaluation method |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59161052A (en) * | 1983-02-24 | 1984-09-11 | Fujitsu Ltd | Manufacture of aluminum alloy package |
-
1983
- 1983-08-01 JP JP58139492A patent/JPS6031247A/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59161052A (en) * | 1983-02-24 | 1984-09-11 | Fujitsu Ltd | Manufacture of aluminum alloy package |
Also Published As
Publication number | Publication date |
---|---|
JPS6031247A (en) | 1985-02-18 |
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