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JPH0329516B2 - - Google Patents
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JPH0329516B2 - - Google Patents

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Publication number
JPH0329516B2
JPH0329516B2 JP57032349A JP3234982A JPH0329516B2 JP H0329516 B2 JPH0329516 B2 JP H0329516B2 JP 57032349 A JP57032349 A JP 57032349A JP 3234982 A JP3234982 A JP 3234982A JP H0329516 B2 JPH0329516 B2 JP H0329516B2
Authority
JP
Japan
Prior art keywords
bonding
insert material
vibration
energy
joining
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
Application number
JP57032349A
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Japanese (ja)
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JPS58151977A (en
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Filing date
Publication date
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Priority to JP57032349A priority Critical patent/JPS58151977A/en
Publication of JPS58151977A publication Critical patent/JPS58151977A/en
Publication of JPH0329516B2 publication Critical patent/JPH0329516B2/ja
Granted legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は接合部材間に金属又は合金のインサー
ト材を用いて拡散接合する方法に係り、特に拡散
接合を安定にし、かつ接合強度を高めるのに好適
な拡散接合方法に関する。 金属の拡散接合法は、一般に固相線以下の温度
で材料に変形を生じさせない程度の圧力をかけ真
空下や不活性雰囲気下にて行う接合方法である。 この拡散接合方法は、従来より多用されている
融接法やろう付に対し最大の特徴は接合部及びそ
の近傍が熱的・相的な変化が少なく、母材並みの
性質が得られることである。2つの金属が接合す
ることは両者の間に金属結合を生じさせることに
あるので、接合面は清浄で、かつ平坦でなければ
ならない。また、優れた洗浄を用いても、有機
物、ガス、酸化物等を吸着し、拡散に妨害となる
ばかりか、接合界面にそれらが残留して接合強度
の低下原因となり易い。従つて、これらの弊害に
対して種々の対策が講じられている。その1つと
して接合部材間にインサート材を介装し、インサ
ート材を溶融することによつて接合面を密着さ
せ、その後拡散処理によつて母材とインサート材
相互の成分の平均化を図る、いわゆる液相拡散接
合法が知られている(特開昭47−33850号公報、
特公昭49−6470号公報)。これらの方法は耐熱超
合金、特に強化機構の根源となるγ″相を析出して
なるNi基、Co基、Fe基等の超合金等に適用さ
れ、それ相当の成果を挙げている。しかしなが
ら、この種の耐熱超合金はγ″相形成の主役をなす
Al,Tiを多量に含有しているため接合面が酸化
し易く、接合面に酸化物を残留する場合が生じて
いる。酸化物が残留すると脆弱な酸化物が起点と
なつて接合面が破断し易くなる危険がある。また
拡散速度が小さい元素が多量に含まれているので
液体一固体間での液相拡散の割には接合時間を短
縮することができない。さらに接合部及びその近
傍のγ″相及び結晶粒の大きさ、分布状態を改善
し、接合強度を高める余地が残されている。 本発明の目的は、接合部に生成される酸化物を
分解、分散されること、インサート材を早期溶融
させること、及びその後の拡散を速めて接合部及
びその近傍の組織を均一微細化することによつて
接合強度を高めることができる拡散接合方法を提
供することにある。 本発明は、Al及びTiを含む析出硬化型のNi基
超合金からなる被接合部材間にインサート材を介
在させ、非酸化性雰囲気中で加熱加圧し接合する
拡散接合方法において、インサート材をNi基超
合金と同等の組成にB及びSiを含有させた非晶質
Ni基合金により形成し、被接合部材間の接合面
を加熱加圧するとともに、インサート材が融解し
ている間に接合面に少なくとも3500VPMの超音
波振動を与え、ついで所定温度で加熱保持して拡
散接合後、溶体化処理及び時効処理を施すように
構成されている。 以下本発明をさらに詳細に説明する。 本発明において、接合部材は耐熱合金、及び一
般の炭素鋼、合金鋼等を使用できる。耐熱合金と
してはγ″相析出強化型の超耐熱合金(Co基、Ni
基、Fe基)のように接合強度が著しく要求され
るものに特に有効である。インサート材は金属又
は合金を用いることができ、その形態は粉末状、
箔状、リボン状のいずれでもよい。インサート材
として非昌質リボンを用いる場合、金属原子の運
動エネルギーを付与することにより得られる効果
の他に非昌質リボン自体の有する特性によつて次
のような利点がある。すなわち第1は非昌質リボ
ンは耐腐食性を有するので接合強度が高く、第2
に極めて薄くかつ均一の厚みとすることができる
ので接合時間が短く、かつ接合強度が高くなり、
第3は強度が高いので接合部材間に介装する形状
に容易に製作でき、かつ介装のための操作が簡便
である。 接合部材間にインサート材を介装し、拡散接合
処理する際、真空下又は保護雰囲気にて任意の面
圧力が与えられる。保護雰囲気としてAr,Ne,
He,H2,CO等の雰囲気とするのがよい。 本発明において、このような雰囲気において、
熱エネルギーと熱エネルギー以外でもあつて、金
属原子の運動エネルギーを高めるためのエネルギ
ー(以下単にエネルギーA)とを付与するもので
ある。エネルギーAによつて金属原子の活性化エ
ネルギーを小さくし、運動を容易にする。このよ
うなエネルギーAとしては振動エネルギー、電磁
誘導エネルギー、高周波誘導エネルギー等が挙げ
られる。 次にこのようなエネルギーAによる効果を、特
に振動エネルギーを例に説明する。振動エネルギ
ーにより金属原子の運動が高められるので、静止
状態に比べてインサート材の融解が極めて速くな
る。 インサート材の融解速度は、接合面の密着化に
関連しており、インサート材の融解が遅いと液相
となる部分が量的に少ないので融液が極所まで侵
入しないうちに等温凝固を開始する危険性があ
る。従つて、密着化のためにはインサート材は瞬
時にして融解することが大切であり、この点、振
動は極めて効結果をもたらす。振動は又、一時的
に液相となつた場合、その中に混在している酸化
物(特にAl、Ti、Cr系)を接合界面に集積させ
ず、分散させ、かつ、酸化物の形状を分断させる
働きをも見い出された。このことは、応力が付加
した際脆弱な酸化物が起点となつて破断するよう
な危険度が大幅に低下するものである。本発明者
らの実験によれば、純金属、炭素鋼、低合金鋼等
の接合においてインサート材の成分中に酸化物形
成元素が含有されていない場合には上記問題はほ
とんどないが、インサート材の成分中に酸化性の
大きい元素が存在する場合は振動の効果が明確で
あり、接合界面の組織上酸化物がほとんど認めら
れなくなる。従つてインサート材成分中にAl,
Ti,Crが多量に含まれるときに振動の効果が最
も発揮できる。振動エネルギーを接合材に付与す
るることは、インサート材の融解を速めるので融
液が極所に入り込んでから凝固する。従つて等温
凝固を速めることになるので、インサート材を溶
融させた温度よりも下げて接合処理を行うことも
できる。このことは、接合部及びこの近傍の組織
及び結晶粒を粗大化させない狙いがあり、接合強
度が厳しく要求される部材に対して有効となる。 このように熱エネルギーとともに振動エネルギ
ーを付与する狙いは、インサート材の早期融解と
等温凝固の促進にある。従つて熱エネルギーの付
与によつてインサート材が融解し始める前、及び
等温凝固が完了した後は振動エネルギーを与える
必要はない。 第1図は時間経過に伴う温度、圧力、振動時期
を示す模式図である。第1図に示すように接合温
度Tがインサート材溶融温度Tiに達する直前で
振動エネルギーの付与を開始(t1)し、融解した
インサート材が母材の成分を得て凝固完了したと
判定し得る時期(t2)に振動エネルギーの付与を
停止するのが望ましい。 インサート材が、凝固後、振動を付与している
と、接合境界において成分的にも、組織的にも未
完成領域を破壊する危惧を生じるためである。な
お、未完成領域の破壊は振動数と振幅及び励振位
置に依存するので、接合部強度を安定化するため
には接合母材とインサート材との構成成分及びイ
ンサート融解温度に応じて、振動エネルギーの停
止タイミングを選択すべきである。 本発明による接合加圧力は振動による密着化が
促進されるため小さい荷重でよい。例えば耐熱超
合金では少なくても2Kgf/cm2で十分である。た
だし、わん曲している接合面の加工は平面に対し
困難でかつ面精度も得がたい。このような曲面同
志の接合においては、接合部の強度の信頼性を確
保するために、インサート材が融解した後、あま
り時間を経過しない時期に加圧力を最初よりも高
めると好都合である。この理由は融解したインサ
ート材が空隙部を満たして面同志を接着せしめ、
接合強度が向上するためである。また、面接着に
必要以外の余分な溶体を接合面からバリとして排
出効果もある。なお、母材とインサート材とが成
分的に及び融点が大きく異なる場合、もしくは接
合界面に母材とインサート材との成分反応によつ
て生じた脆弱な化合物等残存するような場合に積
極的にバリとしての余分な溶体の排出を行わしめ
るため、加圧力をやや高める必要がある。加圧力
を2次的に高める時期は、上記効果を確実に成就
するため重要である。第2図は時間経過に伴う接
合温度(インサート溶融温度)、振動時期と加圧
時期との関係を示す模式図である。この図から明
らかな如く、2次加圧(P2)開始時期はインサ
ート材が融解後及び振動を停止する前であり、こ
のタイミング以外では2次加圧の効果は明確でな
くなる。 次に、振動エネルギーを接合母材に励起させる
手段としては、特に規制するものではないが、実
質的には超音波が好ましい。振動方向も特に規制
するものでなく、応力軸に対し平行方向(縦振
動)でも垂直方向(横振動)でも好結果をもたら
す。振動数は3500VPM以上で、できるだけ高く
することが好ましい。なお、VPMは1分間の振
動数を示し、1VPMは1/60Hzに相当する。 実施例 精密鋳造製Ni基耐熱超合金(Cr;16重量%、
Co;8重量%、W;2.5重量%、Mo;2重量%、
Ta;1.5重量%、Al及びTi;3.4重量%、残Ni)
接合母材とし、インサート材は接合材と同等の成
分に、B(3.2重量%)とSi(2.5重量%)を含有さ
せて融点を降下させた非昌質リボン(非昌質Ni
基合金)を用いた。第3図において、1はチヤン
バー、2は加圧シヤフトであつて、この加圧シヤ
フト2に固定された加圧治具4に上記成分の接合
母材3を装着し、これらの接合母材3のわん曲面
間に上記非昌質リボン5を介装した。 加圧力は0.5Kgf/cm2とし、5×10-4Torrの真
空下で発熱体6によつて加熱を開始した。接合温
度は1170℃であるが、温度900℃に到達してから
接合材に超音波振動子7により15000VPMの振動
を与えつづけた。その後温度が1170℃に達してか
ら加圧力を1.5Kgf/cm2に高め、さらに予備実験
より定めた30分を経過後振動を停止し、合計で5
時間の接合処理を行つた。接合後、炉体より接合
材を取り出し、1120℃×2h溶体化、840℃×24h
時効の熱処理を行つた後、接合部のミクロ組織及
び引張り性質を調べた。その結果、ミクロ組織上
は接合界面及びその近傍のγ″析出相の大きさ、分
布とも母材とほとんど同等であるとともに、結晶
粒が粗大化せず母材よりもむしろ微細であること
が確認できた。 又接合部の引張り性質を第1表に示す。第1表
中、比較例は接合処理時に振動エネルギーを与え
なな以外は実施例と同じである。第1表によれ
ば、本実施例では比較例に比べて引張性質に優
れ、特に伸びの向上が顕著である。この結果か
ら、本発明は複雑な内孔を有するガスタービン動
翼の接合にも十分適用し得ることが確認できた。
The present invention relates to a diffusion bonding method using a metal or alloy insert material between bonding members, and particularly to a diffusion bonding method suitable for stabilizing diffusion bonding and increasing bonding strength. Diffusion bonding of metals is generally a bonding method that is performed under vacuum or an inert atmosphere by applying a pressure that does not cause deformation of the material at a temperature below the solidus line. The biggest feature of this diffusion bonding method, compared to the conventionally widely used fusion welding and brazing methods, is that there is little thermal or phase change in the bonded area and its vicinity, and properties comparable to those of the base metal can be obtained. be. Since the purpose of joining two metals is to create a metallic bond between them, the joining surfaces must be clean and flat. Further, even if excellent cleaning is used, organic substances, gases, oxides, etc. are adsorbed and not only hinder diffusion, but also remain at the bonding interface, which tends to cause a decrease in bonding strength. Therefore, various countermeasures have been taken against these harmful effects. One method is to interpose an insert material between the joining members, melt the insert material to bring the joining surfaces into close contact, and then use a diffusion process to average out the mutual components of the base material and the insert material. The so-called liquid phase diffusion bonding method is known (Japanese Patent Application Laid-Open No. 47-33850,
Special Publication No. 49-6470). These methods have been applied to heat-resistant superalloys, particularly Ni-based, Co-based, Fe-based superalloys, etc., which are formed by precipitating the γ″ phase, which is the root of the strengthening mechanism, and have achieved considerable results. , this kind of heat-resistant superalloy plays the main role in the formation of the γ″ phase.
Since it contains a large amount of Al and Ti, the bonding surface is easily oxidized, and oxides may remain on the bonding surface. If oxide remains, there is a risk that the bonding surface will easily break due to the weak oxide becoming a starting point. Furthermore, since it contains a large amount of elements with low diffusion rates, it is not possible to shorten the bonding time considering the liquid-phase diffusion between a liquid and a solid. Furthermore, there is still room to improve the size and distribution of the γ'' phase and crystal grains in and around the joint to increase the joint strength. To provide a diffusion bonding method capable of increasing the bonding strength by dispersing the insert material, melting the insert material early, and speeding up the subsequent diffusion to uniformly refine the structure of the bonded portion and its vicinity. The present invention relates to a diffusion bonding method in which an insert material is interposed between members to be joined made of a precipitation hardening Ni-based superalloy containing Al and Ti, and the members are joined by heating and pressurizing in a non-oxidizing atmosphere. Amorphous insert material containing B and Si with the same composition as Ni-based superalloy
Formed from a Ni-based alloy, the joint surfaces between the members to be joined are heated and pressurized, and while the insert material is melting, ultrasonic vibrations of at least 3500 VPM are applied to the joint surfaces, and then heated and held at a predetermined temperature to diffuse. After joining, the structure is such that solution treatment and aging treatment are performed. The present invention will be explained in more detail below. In the present invention, a heat-resistant alloy, general carbon steel, alloy steel, etc. can be used for the joining member. As heat-resistant alloys, γ″ phase precipitation strengthened super heat-resistant alloys (Co-based, Ni
It is particularly effective for materials that require extremely high bonding strength, such as (Fe-based, Fe-based). The insert material can be made of metal or alloy, and its form is powder,
It may be either foil-like or ribbon-like. When a non-membrane ribbon is used as an insert material, in addition to the effect obtained by imparting kinetic energy of metal atoms, the following advantages are provided by the properties of the non-metamorphic ribbon itself. In other words, the first reason is that the non-corrosive ribbon has high bonding strength because it has corrosion resistance, and the second reason is that the non-corrosive ribbon has high bonding strength.
Since it can be made extremely thin and uniform in thickness, the bonding time is short and the bonding strength is high.
Thirdly, since it has high strength, it can be easily manufactured into a shape that can be inserted between joining members, and the operation for inserting it is simple. When an insert material is interposed between joining members and a diffusion bonding process is performed, an arbitrary surface pressure is applied under vacuum or in a protective atmosphere. Ar, Ne, as a protective atmosphere
It is preferable to use an atmosphere of He, H 2 , CO, etc. In the present invention, in such an atmosphere,
It imparts thermal energy and energy other than thermal energy (hereinafter simply referred to as energy A) for increasing the kinetic energy of metal atoms. Energy A reduces the activation energy of metal atoms and facilitates their movement. Such energy A includes vibration energy, electromagnetic induction energy, high frequency induction energy, and the like. Next, the effect of such energy A will be explained, particularly taking vibration energy as an example. The vibrational energy enhances the motion of the metal atoms, resulting in extremely rapid melting of the insert material compared to the static state. The melting speed of the insert material is related to the adhesion of the joint surfaces, and if the insert material melts slowly, the portion that becomes a liquid phase is small in quantity, so isothermal solidification begins before the melt penetrates to the extreme. There is a risk of Therefore, in order to achieve close contact, it is important that the insert material melts instantly, and in this respect, vibration is extremely effective. Also, when vibration temporarily becomes a liquid phase, it prevents the oxides (especially Al, Ti, and Cr systems) mixed therein from accumulating at the bonding interface, disperses them, and changes the shape of the oxides. It was also discovered that it has the ability to cause division. This greatly reduces the risk that the fragile oxide will become a starting point and break when stress is applied. According to experiments conducted by the present inventors, when joining pure metals, carbon steel, low-alloy steel, etc., the above-mentioned problems are almost non-existent if the insert material does not contain any oxide-forming elements. When a highly oxidizing element is present in the components, the effect of vibration is clear, and almost no oxides are observed on the structure of the bonding interface. Therefore, the insert material contains Al,
The vibration effect is most effective when large amounts of Ti and Cr are included. Applying vibrational energy to the bonding material accelerates the melting of the insert material, so that the melt enters the extreme regions and then solidifies. Therefore, since isothermal solidification is accelerated, the joining process can be performed at a temperature lower than the temperature at which the insert material was melted. This is aimed at preventing the structure and crystal grains in and around the joint from becoming coarse, and is effective for members where joint strength is strictly required. The purpose of applying vibrational energy in addition to thermal energy is to promote early melting and isothermal solidification of the insert material. Therefore, it is not necessary to apply vibrational energy before the insert material begins to melt due to the application of thermal energy and after isothermal solidification is completed. FIG. 1 is a schematic diagram showing temperature, pressure, and vibration timing over time. As shown in Figure 1, the application of vibrational energy is started (t 1 ) just before the joining temperature T reaches the insert material melting temperature Ti, and it is determined that the molten insert material has acquired the components of the base material and solidification has been completed. It is desirable to stop applying vibrational energy at the time when vibration energy is to be obtained (t 2 ). This is because if the insert material is subjected to vibration after solidification, there is a risk that the unfinished region at the bonding boundary will be destroyed both in terms of composition and structure. Furthermore, since the destruction of the unfinished area depends on the vibration frequency, amplitude, and excitation position, in order to stabilize the joint strength, the vibration energy must be adjusted according to the constituent components of the joining base material and insert material and the insert melting temperature. The timing of stopping should be selected. The bonding force according to the present invention may be a small load because the bonding force is promoted by vibration. For example, for heat-resistant superalloys, at least 2 Kgf/cm 2 is sufficient. However, machining a curved joint surface is more difficult than machining a flat surface, and it is also difficult to obtain surface accuracy. In joining such curved surfaces, in order to ensure the reliability of the strength of the joint, it is advantageous to increase the pressing force from the beginning shortly after the insert material has melted. The reason for this is that the molten insert material fills the void and bonds the surfaces together.
This is because the bonding strength is improved. It also has the effect of discharging excess solution that is not necessary for surface bonding from the bonding surface as burrs. In addition, if the base material and the insert material differ greatly in composition and melting point, or if there is a weak compound remaining at the bonding interface due to a component reaction between the base material and the insert material, In order to discharge excess solution as burrs, it is necessary to increase the pressing force slightly. The timing of secondarily increasing the pressing force is important in order to reliably achieve the above effects. FIG. 2 is a schematic diagram showing the relationship between bonding temperature (insert melting temperature), vibration timing, and pressurization timing over time. As is clear from this figure, the secondary pressurization (P 2 ) starts after the insert material melts and before the vibration stops, and the effect of the secondary pressurization is not clear at timings other than this. Next, although there are no particular restrictions on the means for exciting vibration energy into the joining base material, ultrasonic waves are substantially preferable. The direction of vibration is not particularly limited either, and good results can be obtained either in a direction parallel to the stress axis (longitudinal vibration) or in a direction perpendicular to the stress axis (transverse vibration). The frequency is preferably 3500 VPM or higher, preferably as high as possible. Note that VPM indicates the frequency of vibration per minute, and 1 VPM corresponds to 1/60Hz. Example Precision casting Ni-based heat-resistant superalloy (Cr; 16% by weight,
Co: 8% by weight, W: 2.5% by weight, Mo: 2% by weight,
Ta: 1.5% by weight, Al and Ti: 3.4% by weight, remaining Ni)
The bonding base material is a non-selective ribbon (non-selective Ni) containing B (3.2% by weight) and Si (2.5% by weight) in the same composition as the bonding material to lower the melting point.
base alloy) was used. In FIG. 3, 1 is a chamber, 2 is a pressure shaft, and the bonding base materials 3 of the above components are mounted on a pressure jig 4 fixed to the pressure shaft 2, and these bonding base materials 3 are The amorphous ribbon 5 was interposed between the curved surfaces. The applied pressure was 0.5 Kgf/cm 2 , and heating was started using the heating element 6 under a vacuum of 5×10 −4 Torr. The bonding temperature was 1170°C, but after the temperature reached 900°C, the ultrasonic vibrator 7 continued to apply vibrations of 15000 VPM to the bonding material. After that, when the temperature reached 1170℃, the pressure was increased to 1.5Kgf/ cm2 , and after 30 minutes determined from the preliminary experiment, the vibration was stopped.
A time bonding process was performed. After bonding, the bonding material was taken out of the furnace body and subjected to solution treatment at 1120°C for 2 hours, then at 840°C for 24 hours.
After aging heat treatment, the microstructure and tensile properties of the joint were investigated. As a result, it was confirmed that the size and distribution of the γ'' precipitated phase at and near the bonding interface were almost the same as the base metal in terms of the microstructure, and that the crystal grains did not become coarse and were rather finer than the base metal. The tensile properties of the joints are shown in Table 1. In Table 1, the comparative examples are the same as the examples except that no vibration energy is applied during the joining process. The Example has excellent tensile properties compared to the Comparative Example, and the improvement in elongation is particularly remarkable.From these results, it is confirmed that the present invention can be fully applied to joining gas turbine rotor blades with complex inner holes. did it.

【表】 以上のように本実施例よれば、熱エネルギー
と、超音波エネルギーとを付与することによつ
て、インサート材の早期溶融と等温凝固の促進を
促すとともに、接合界面における酸化物の分散と
分断化を計り、低加圧下で耐熱合金で形成した接
合部材とインサート材同志の安定かつ強固な接合
部を得ることができる。
[Table] As described above, according to this example, by applying thermal energy and ultrasonic energy, early melting of the insert material and promotion of isothermal solidification are promoted, and the dispersion of oxides at the bonding interface is It is possible to obtain a stable and strong joint between the joining member made of a heat-resistant alloy and the insert material under low pressure.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図及び第2図は接合時間と温度、圧力、振
動との関係を示す模式図、第3図は本発明の実施
例を示す装置の概略構成図である。 3……接合母材、5……インサート材、6……
発熱体、7……超音波振動子。
FIGS. 1 and 2 are schematic diagrams showing the relationship between bonding time, temperature, pressure, and vibration, and FIG. 3 is a schematic diagram of an apparatus showing an embodiment of the present invention. 3... Bonding base material, 5... Insert material, 6...
Heating element, 7... Ultrasonic vibrator.

Claims (1)

【特許請求の範囲】[Claims] 1 Al及びTiを含む析出硬化型のNi基超合金か
らなる被接合部材間にインサート材を介在させ、
非酸化性雰囲気中で加熱加圧し接合する拡散接合
方法において、前記インサート材を前記Ni基超
合金と同等の組成にB及びSiを含有させた非晶質
Ni基合金により形成し、前記被接合部材間の接
合面を加熱加圧するとともに、前記インサート材
が融解している間に前記接合面に少なくとも
3500VPMの超音波振動を与え、ついで所定温度
で加熱保持して拡散接合後、溶体化処理及び時効
処理を施すことを特徴とする拡散接合方法。
1 An insert material is interposed between the members to be joined made of a precipitation hardening type Ni-based superalloy containing Al and Ti,
In the diffusion bonding method of bonding by heating and pressurizing in a non-oxidizing atmosphere, the insert material is an amorphous material containing B and Si with the same composition as the Ni-based superalloy.
The insert material is made of a Ni-based alloy, and the joining surfaces between the members to be joined are heated and pressurized, and at least
A diffusion bonding method characterized by applying ultrasonic vibration of 3500 VPM, then heating and holding at a predetermined temperature to perform diffusion bonding, followed by solution treatment and aging treatment.
JP57032349A 1982-03-03 1982-03-03 Diffusion bonding method Granted JPS58151977A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57032349A JPS58151977A (en) 1982-03-03 1982-03-03 Diffusion bonding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57032349A JPS58151977A (en) 1982-03-03 1982-03-03 Diffusion bonding method

Publications (2)

Publication Number Publication Date
JPS58151977A JPS58151977A (en) 1983-09-09
JPH0329516B2 true JPH0329516B2 (en) 1991-04-24

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP57032349A Granted JPS58151977A (en) 1982-03-03 1982-03-03 Diffusion bonding method

Country Status (1)

Country Link
JP (1) JPS58151977A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19747846A1 (en) * 1997-10-30 1999-05-06 Daimler Benz Ag Component and method for producing the component
JP5853365B2 (en) * 2010-07-28 2016-02-09 日産自動車株式会社 Joining apparatus and joining method

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5852473B2 (en) * 1976-07-05 1983-11-22 株式会社白山製作所 Welding method for steel materials, etc.
JPS551922A (en) * 1978-06-21 1980-01-09 Hitachi Ltd Jointing method for aluminum parts

Also Published As

Publication number Publication date
JPS58151977A (en) 1983-09-09

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