JPH0621322B2 - Ceramic expansion brazing alloy for brazing - Google Patents
Ceramic expansion brazing alloy for brazingInfo
- Publication number
- JPH0621322B2 JPH0621322B2 JP859786A JP859786A JPH0621322B2 JP H0621322 B2 JPH0621322 B2 JP H0621322B2 JP 859786 A JP859786 A JP 859786A JP 859786 A JP859786 A JP 859786A JP H0621322 B2 JPH0621322 B2 JP H0621322B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- brazing
- thermal expansion
- present
- ceramics
- 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 - Lifetime
Links
- 229910045601 alloy Inorganic materials 0.000 title claims description 42
- 239000000956 alloy Substances 0.000 title claims description 42
- 239000000919 ceramic Substances 0.000 title claims description 23
- 238000005219 brazing Methods 0.000 title claims description 19
- 229910052759 nickel Inorganic materials 0.000 claims description 18
- 239000012535 impurity Substances 0.000 claims description 2
- 230000009466 transformation Effects 0.000 description 11
- 239000000203 mixture Substances 0.000 description 10
- 238000001816 cooling Methods 0.000 description 8
- 229910000833 kovar Inorganic materials 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 7
- 239000000463 material Substances 0.000 description 5
- 229910001374 Invar Inorganic materials 0.000 description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 4
- 229910052709 silver Inorganic materials 0.000 description 4
- 239000004332 silver Substances 0.000 description 4
- 230000035882 stress Effects 0.000 description 4
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 229910017083 AlN Inorganic materials 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000004781 supercooling Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Landscapes
- Ceramic Products (AREA)
Description
【発明の詳細な説明】 本発明はAl2O3セラミツクスよりも一段と熱膨張係数
が小さく比較的強度の高い緻密なセラミツクスに対して
ろう付することの出来る熱膨張調整合金に関するもので
ある。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a thermal expansion control alloy which can be brazed to a dense ceramic having a smaller thermal expansion coefficient than Al 2 O 3 ceramics and a relatively high strength.
従来、セラミツクスに金属をろう付するには、熱膨張係
数の出来るだけ適合した金属や合金を選定して、ろう付
の際の冷却過程で両者の熱膨張係数の差に起因して発生
する熱応力を極力小さくするようにしたり、あるいは
鋼,銀,アルミニウム等のかなり柔軟な金属を中間緩衝
材として間に挾んでこの熱応力による歪を吸収するよう
に工夫して、実施されて来た。Conventionally, to braze a metal to ceramics, a metal or alloy that has a thermal expansion coefficient that is as close as possible is selected, and the heat generated due to the difference in thermal expansion coefficient between the two in the cooling process during brazing. It has been carried out by making the stress as small as possible, or by devising a soft metal such as steel, silver, and aluminum as an intermediate cushioning material to intervene to absorb the strain due to this thermal stress.
しかしながら、近年、比較的機械的性質の優れた強度が
高く、かつ熱膨張係数の小さな炭化物系、窒化物系のセ
ラミツクスとして、例えば常圧焼結SiC,反応焼結SiC-S
i,常圧焼結Si3N4,常圧焼結AlN,などのセラミツクス
焼結体が開発されるに及んで、これらのセラミツクスに
ろう付することの出来る熱膨張係数の小さな金属や合金
を開発する必要に迫られて来た。室温〜800℃の銀ろ
う付温度の昇温範囲で熱膨張係数の最も小さな金属はW
であり、その値は45×10-6/℃程度であるので、Si
C,SiC-Si あるいはAlN等の熱膨張係数が4〜5×10-6
/℃の範囲内程度のセラミツクス焼結体のろう付にはか
ろうじて用いることが出来る。しかし、Wは非常に硬質
で脆く、柔軟性に乏しいため、接合部に歪を残留させや
すく、さらに資源的に乏しく高価であるため満足出来る
材料ではない。又従来Al2O3セラミツクスの接合用合金
として知られているCo 17.0重量%,Ni 29.0
重量%,残部実質的にFe よりなるコバール合金は室温
〜430℃までの温度範囲でも熱膨張係数が4.8×1
0-6/℃程度であり、室温〜800℃の範囲では平均
8.8×10-6/℃となるため、前記の如き低熱膨張性
のセラミツクスに適用することは困難である。However, in recent years, as carbide-based and nitride-based ceramics having relatively high mechanical properties and high strength and a small thermal expansion coefficient, for example, normal pressure sintering SiC, reaction sintering SiC-S.
With the development of ceramics sintered bodies such as i, atmospheric pressure sintered Si 3 N 4 and atmospheric pressure sintered AlN, metals and alloys with a small thermal expansion coefficient that can be brazed to these ceramics have been developed. I have been forced to develop. The metal with the smallest coefficient of thermal expansion is W in the temperature range of room temperature to 800 ℃ for silver brazing.
And the value is about 45 × 10 −6 / ° C.
The thermal expansion coefficient of C, SiC-Si or AlN is 4-5 × 10 -6
It can be barely used for brazing ceramics sintered bodies within the range of / ° C. However, since W is extremely hard, brittle, and poor in flexibility, strain is likely to remain in the joint portion, and resources are scarce and expensive, so it is not a satisfactory material. Further, Co 17.0 wt% and Ni 29.0 which are conventionally known as alloys for joining Al 2 O 3 ceramics are used.
The Kovar alloy, which is composed of wt% and the balance of Fe, has a thermal expansion coefficient of 4.8 × 1 even in the temperature range from room temperature to 430 ° C.
It is about 0 −6 / ° C., and the average is 8.8 × 10 −6 / ° C. in the range of room temperature to 800 ° C., so it is difficult to apply it to the low thermal expansion ceramics as described above.
本発明は、これらの状況に鑑みてなされたものであり、
熱膨張係数の小さな5.0×10-6/℃以下のセラミツ
クスで強度が高く、抗析力20kg/mm2以上の値を有す
る緻密質のセラミツクスに対して比較的強度を損なうこ
となくろう付可能な合金を提供することを目的としてい
る。The present invention has been made in view of these circumstances,
The ceramics with a small thermal expansion coefficient of 5.0 × 10 −6 / ° C. or less have high strength, and brazing to the dense ceramics having a segregation force of 20 kg / mm 2 or more without compromising the strength. The aim is to provide possible alloys.
本発明のセラミツクスろう付用熱膨張調整合金は、(以
下重量%の重量を省略する)第1図にA領域とし示され
る範囲、即ち、 40%≦Ni%+Co%,24.0%≦Ni%,Ni%
+0.47Co%≧34.0%,Ni%+0.3Co%
≦34.5% Ni%+0.58Co%≦37.8%,の全ての不等式
を満足するような範囲のCoとNi,さらに残部実質的
にFe及び不可避的不純物よりなることを特徴としてい
る。但し、Si,Mn,Cなどの脱酸材成分を合計0.6%
以下含むことも出来る。The thermal expansion control alloy for ceramics brazing of the present invention has a range shown as an A region in FIG. 1 (hereinafter, weight% is omitted), that is, 40% ≦ Ni% + Co%, 24.0% ≦ Ni. %, Ni%
+ 0.47Co% ≧ 34.0%, Ni% + 0.3Co%
≦ 34.5% Ni% + 0.58Co% ≦ 37.8%, Co and Ni in a range that satisfies all the inequalities, and the balance is substantially Fe and inevitable impurities. However, the total content of deoxidizing materials such as Si, Mn, C is 0.6%.
It can also include:
本発明の合金の成分は第1図中にB点として示される前
記のコバール合金や、室温から100℃の温度範囲で熱
膨張係数が1.3×10-6/℃という非常に小さな値を
有することで知られている Co4%,Ni13%,残
部鉄よりなり、同図中に点Cとして示されるスーパーイ
ンバー合金や、36%Ni,残部鉄よりなり点Dで示さ
れるインバー合金などと共に示すことが出来る。The composition of the alloy of the present invention has the above-mentioned Kovar alloy shown as point B in FIG. 1 and a very small coefficient of thermal expansion of 1.3 × 10 −6 / ° C. in the temperature range from room temperature to 100 ° C. It is known to have 4% Co, 13% Ni, and the balance iron, and is shown together with the Super Invar alloy shown as point C in the figure, and the Invar alloy made of 36% Ni and the balance iron at point D. You can
従来より一般に知られているこれらの合金はいずれも、
−80℃程度の低温に冷却されても結晶構造をγからα
へと変態してしまうことのない成分範囲として、点a,
b近傍を通る曲線より上側のNi,Coの多い領域に属
している。本発明合金は逆に−80℃程度の温度以上で
はこのγ→α変態を発生するように成分範囲を設定した
ものであるので、Ni%+0.3Co%≦34.5%の
境界線abの下側の範囲のNiとCoの成分とし、さら
に冷却時の熱膨張係数が、低熱膨張セラミツクスとの接
合のためには、最大でも4.0×10-6/℃未満の値に
抑えたい為に直線bあるいはaeの間の領域、即ちNi
%+0.58Co%≦37.8%と40%≦Ni%+C
o%とを満足するNiとCoの成分範囲としている。さ
らに、上記γ→α変態の逆変態、即ち昇温時にγ→α変
態がろう付温度である750〜900℃程度で生じ得る
範囲として直線ed及びdc以上の領域、即ちNi%+
0.47%≧34.0%及び24.0%≦Ni%とを満足す
るNiとCoの成分範囲としている。Each of these alloys, which are generally known from the past,
The crystal structure changes from γ to α even when cooled to a temperature as low as −80 ° C.
As a component range that does not transform into
It belongs to a region containing a large amount of Ni and Co above the curve passing near b. On the contrary, since the alloy of the present invention has the composition range set so that the γ → α transformation occurs at a temperature of about −80 ° C. or higher, the boundary line ab of Ni% + 0.3Co% ≦ 34.5% is satisfied. Since Ni and Co components in the lower range are used and the coefficient of thermal expansion during cooling is to be kept to a value of less than 4.0 × 10 −6 / ° C. at the maximum in order to bond with low thermal expansion ceramics. The area between the straight lines b or ae, that is, Ni
% + 0.58Co% ≦ 37.8% and 40% ≦ Ni% + C
The composition range of Ni and Co that satisfies o% is set. Further, as a range in which the reverse transformation of the γ → α transformation, that is, the γ → α transformation can occur at a brazing temperature of about 750 to 900 ° C. at the time of temperature rise, a region above the straight lines ed and dc, that is, Ni% +
The composition ranges of Ni and Co satisfy 0.47% ≧ 34.0% and 24.0% ≦ Ni%.
本発明のabcdeで囲まれた成分範囲のNiとCo,
さらに残部実質的にFeよりなる熱膨張調整合金は上記
の説明の如く、室温から400℃までの熱膨張係数が
4.0×10-6/℃未満であり、さらにろう付後の冷却
中、あるいは強制的に−80℃程度まで徐々に過冷却する
ことにより、あるいは加工することにより、容易にγ→
α変態を生じる合金である。同図中の実線の曲線は冷却
に際してのγ→α変態の開始温度を、点線はキユーリー
点の温度を示す。Ni and Co in the composition range surrounded by abcde of the present invention,
Further, the balance of the thermal expansion adjusting alloy consisting essentially of Fe has a thermal expansion coefficient of less than 4.0 × 10 −6 / ° C. from room temperature to 400 ° C. as described above, and during cooling after brazing, Alternatively, by forcibly gradually cooling to about -80 ° C or by processing, γ →
An alloy that undergoes alpha transformation. In the figure, the solid line curve shows the starting temperature of the γ → α transformation during cooling, and the dotted line shows the temperature at the Curie point.
第2図中にコバール合金の熱膨張曲線(1),及び本発明
の合金の例として0℃まで冷却されて、αとγが共存す
る成分と、−80℃まで過冷却されて殆んどαだけとな
つた成分との熱膨張曲線を各々(2),(3)として示す。即
ち、本発明合金は、加熱,昇温時に履歴を生じるので、
この履歴を上手に利用して前記のろう付によつて生じる
応力,歪を吸収しようとするものである。FIG. 2 shows the thermal expansion curve (1) of Kovar alloy, and as an example of the alloy of the present invention, it was cooled to 0 ° C., a component in which α and γ coexist, and supercooled to −80 ° C. The thermal expansion curves of the components with only α are shown as (2) and (3), respectively. That is, since the alloy of the present invention produces a history during heating and temperature rise,
This history is used effectively to absorb the stress and strain generated by the brazing.
第3図に本発明の合金とSi3N4などの熱膨張係数が3.
2×10-6/℃程度のメタライズ処理を施した焼結体と
を融点が780℃の共晶銀ろうを用いてろう付接合する
場合の原理を熱膨張曲線によつて説明する。本発明合金
と窒化珪素の冷却による収縮はイロハニ,及びチニの線
で表わされ、今、合金の収縮を示す線の方を基準にして
考えると、ろう付後銀ろうの柔軟な温度範囲の780℃
〜500℃の領域では、合金及びセラミツクスは各々独
自にイロ,及びチリの如く収縮する。しかし500℃以
下では銀ろうによつて互いに拘束されながら変形し、セ
ラミツクスはチリニと平行な収縮を示す線ロヘヌの如く
収縮しようとするので、室温ではヌニの分に相当する歪
が残留すると考えられる。しかしながら本発明合金の本
例の合金は0℃まで冷却すると、一部γ→α変態を生じ
熱膨張曲線に変化を生じるので、次に昇温する場合には
ホヘトイの如く膨張し、400℃の点で前記の残留歪を
殆んど吸収してしまうことができる。その後さらに昇温
を続けると若干逆の方向の歪が生じるろうがろう材自身
が軟化し柔軟となるので合成とセラミツクスは互いに独
自に膨張出来るようになるので問題とはなりにくい。さ
らに点トでα→γ変態を生じ殆んどγのみの単一の相と
なる。FIG. 3 shows the thermal expansion coefficient of the alloy of the present invention and Si 3 N 4 etc.
The principle of brazing and joining a sinter that has been subjected to a metallizing treatment of about 2 × 10 −6 / ° C. using eutectic silver solder having a melting point of 780 ° C. will be described using a thermal expansion curve. The shrinkage of the alloy of the present invention and silicon nitride due to cooling is represented by the lines of Irohani and Chini. Considering now the line showing the shrinkage of the alloy as a reference, the flexible temperature range of silver solder after brazing is considered. 780 ° C
In the region of ~ 500 ° C, the alloy and the ceramic shrink independently like yellow and dust. However, at temperatures below 500 ° C, they are deformed while being constrained by silver brazing, and the ceramics try to shrink like the line Rohenu, which shows shrinkage parallel to the chillini, so it is thought that at room temperature, a strain equivalent to the amount of Nuni remains. . However, when the alloy of the present invention of this example is cooled to 0 ° C., a partial γ → α transformation occurs to cause a change in the thermal expansion curve. At this point, the above residual strain can be almost absorbed. If the temperature is further increased thereafter, a strain in the opposite direction will occur, but the brazing filler metal itself will soften and become flexible, so that the composite and the ceramics will be able to expand independently of each other, so there is no problem. Furthermore, at the point G, the α → γ transformation occurs, and almost a single phase consisting of only γ is formed.
本発明の熱膨張調整合金は上記の如く、γα変態を利用
して、ろう付の際の残留応力,歪を消滅あるいは軽減し
ようとするものであり、従来の一般に知られているコバ
ールや42%ニツケル−鉄合金等とは本質的に思想を異
つたものとしている。本発明は、前記の如く、窒化物や
炭化物などのセラミツクスの熱膨張係数が3×10
-6台、あるいは4×10-6台のセラミツクスを対象とす
る金属とのろう付を可能とするものであり、タングステ
ンなどの希少金属を使う必要がないことも考慮に入れる
と、本発明の効果は極めて大きい。As described above, the thermal expansion control alloy of the present invention is intended to eliminate or reduce the residual stress and strain during brazing by utilizing the γα transformation, and the conventional generally known Kovar or 42% The idea is essentially different from nickel-iron alloy and the like. According to the present invention, as described above, the coefficient of thermal expansion of ceramics such as nitrides and carbides is 3 × 10.
-6 or 4 × 10 -6 ceramics which can be brazed with a target metal, and considering that it is not necessary to use a rare metal such as tungsten, The effect is extremely large.
以下実施例によつて本発明を説明する。The present invention will be described below with reference to examples.
実施例1. 本発明合金として、第1表に記載の成分の合金を配合溶
解しさらに熱間圧延によつて10mmより5mmの板厚と
し、さらに冷間厚延によつて3mmの板材とした。その
後、熱膨張試験片を切り出して1000℃の熱処理後、
0℃あるいは−80℃に冷却して、熱膨張係数及び熱膨
張曲線によりα,γの識別をして同表記載の如き結果を
得、いずれも−80℃以上でγ→α変態を生じ、γの熱
膨張係数は4.0×10-6/℃未満であることを証明し
た。Example 1. As the alloy of the present invention, alloys having the components shown in Table 1 were blended and melted, and hot rolled to a plate thickness of 10 mm to 5 mm, and further cold rolled to a plate material of 3 mm. After that, a thermal expansion test piece is cut out and heat-treated at 1000 ° C.,
After cooling to 0 ° C. or −80 ° C., α and γ were identified by the thermal expansion coefficient and the thermal expansion curve, and the results shown in the same table were obtained. In both cases, the γ → α transformation occurs at −80 ° C. or higher, It was proved that the coefficient of thermal expansion of γ was less than 4.0 × 10 -6 / ° C.
実施例2. 本発明合金として前記実施例中のNo.5,No.10を選び
Si3N4の常圧焼結セラミツクスをNi,Cr,Zrを含
むメタライズ用組成物を用いて、メタライズ処理後、共
晶銀ろうを用い、2mmの厚みの中間緩衝材料としてこれ
らの合金を用い、直径12mmの炭素鋼にろう付後、−8
0℃に過冷さ却せて、室温の剪断強度を測定した。又、
比較の為にコバール合金を用いた場合についても測定し
た。No.10は7.9kg/mm2,No.5は9.5kg/mm2,コ
バールの場合は8.5kg/mm2の値を示し、本発明合金が
室温においても残留応力を緩和していることを示した。 Example 2. As the alloy of the present invention, No. 5 and No. 10 in the above examples were selected.
Using a metallizing composition containing Ni, Cr, and Zr, a pressure-pressure sintered ceramic of Si 3 N 4 and using a eutectic silver braze after metallizing, using these alloys as an intermediate buffer material having a thickness of 2 mm. -8 after brazing to carbon steel with a diameter of 12 mm
After supercooling to 0 ° C., the shear strength at room temperature was measured. or,
For comparison, the measurement was performed also when Kovar alloy was used. No. 10 shows a value of 7.9 kg / mm 2 , No. 5 shows a value of 9.5 kg / mm 2 , and Kovar shows a value of 8.5 kg / mm 2 , showing that the alloy of the present invention relaxes the residual stress even at room temperature. I showed that.
以上の如く本発明は低熱膨張セラミツクスのろう付に関
して新規な手法を提供するものであり、従来解決出来な
かつた困難な問題を解決するうえで非常に有効である。As described above, the present invention provides a novel method for brazing a low thermal expansion ceramics, and is very effective in solving a difficult problem that could not be solved in the past.
第1図は本発明の熱膨張調整合金の成分範囲を示すFe,C
o,Ni の3元組成図であり、A領域は本発明合金の成分
範囲、B,C,D点は各々従来より公知のコバール,ス
ーパーインバー,インバーの各合金を示し、各黒点は第
1表中記載の各合金の成分を示す。又実線は冷却に際し
てγ→α変態が開始する温度を示し、点線はキユーリー
点を示す。 第2図はコバール合金,本発明合金第1表記載のNo.9
の合金及びNo.7の合金の熱膨張曲線を各々(1),(2),
(3)で示し、(1),(2)は0℃まで冷却、(3)は−80℃ま
で過冷却させた場合である。 第3図は本発明合金の1組成のものと、窒化珪素セラミ
ツクス焼結体の熱膨張及びろう付による残留歪を図示
し、本発明合金の原理を示す図である。FIG. 1 shows the composition range of the thermal expansion control alloy of the present invention Fe, C
FIG. 3 is a ternary composition diagram of o and Ni, where region A is the composition range of the alloy of the present invention, points B, C and D are the conventionally known alloys of Kovar, Super Invar and Invar, and the black dots are the first. The components of each alloy described in the table are shown. The solid line shows the temperature at which the γ → α transformation starts during cooling, and the dotted line shows the Curie point. FIG. 2 shows Kovar alloy, No. 9 described in Table 1 of the present invention alloy.
The thermal expansion curves of alloy No. 7 and alloy No. 7 are (1), (2),
Shown by (3), (1) and (2) are when cooled to 0 ° C, and (3) is when supercooled to -80 ° C. FIG. 3 is a diagram showing the principle of the alloy of the present invention by illustrating one composition of the alloy of the present invention and the residual strain due to thermal expansion and brazing of a silicon nitride ceramics sintered body.
Claims (1)
i%,Ni%+0.47Co%≧34.0%,Ni%+
0.3Co%≦34.5%,Ni%+0.58Co%≦
37.8%(重量%の重量を省略)の全ての不等式を満
足するような範囲の、CoとNi,さらに残部実質的に
Fe及び不可避的不純物よりなることを特徴とするセラ
ミツクスろう付用熱膨張調整合金。1. 40% ≦ Ni% + Co%, 24.0% ≦ N
i%, Ni% + 0.47Co% ≧ 34.0%, Ni% +
0.3Co% ≦ 34.5%, Ni% + 0.58Co% ≦
Heat for brazing ceramics characterized by being composed of Co and Ni, and the balance being substantially Fe and inevitable impurities, in a range satisfying all inequalities of 37.8% (weight% is omitted). Expansion adjustment alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP859786A JPH0621322B2 (en) | 1986-01-17 | 1986-01-17 | Ceramic expansion brazing alloy for brazing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP859786A JPH0621322B2 (en) | 1986-01-17 | 1986-01-17 | Ceramic expansion brazing alloy for brazing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62167833A JPS62167833A (en) | 1987-07-24 |
| JPH0621322B2 true JPH0621322B2 (en) | 1994-03-23 |
Family
ID=11697377
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP859786A Expired - Lifetime JPH0621322B2 (en) | 1986-01-17 | 1986-01-17 | Ceramic expansion brazing alloy for brazing |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0621322B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2909856B2 (en) * | 1991-11-14 | 1999-06-23 | 日本特殊陶業株式会社 | Joint of ceramic substrate and metal |
| US12553113B2 (en) | 2020-03-24 | 2026-02-17 | Shinhokoku Material Corp. | Low thermal expansion cast steel and method of production of same |
| EP4617396A1 (en) * | 2024-03-15 | 2025-09-17 | Shinhokoku Material Corp. | Low thermal expansion alloy |
-
1986
- 1986-01-17 JP JP859786A patent/JPH0621322B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62167833A (en) | 1987-07-24 |
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