JPH0223499B2 - - Google Patents
Info
- Publication number
- JPH0223499B2 JPH0223499B2 JP59233346A JP23334684A JPH0223499B2 JP H0223499 B2 JPH0223499 B2 JP H0223499B2 JP 59233346 A JP59233346 A JP 59233346A JP 23334684 A JP23334684 A JP 23334684A JP H0223499 B2 JPH0223499 B2 JP H0223499B2
- Authority
- JP
- Japan
- Prior art keywords
- graphite
- bonding
- vanadium
- molybdenum
- melting point
- 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
Landscapes
- Ceramic Products (AREA)
Description
(産業上の利用分野)
本発明はグラフアイトと高融点金属との接合材
料の製造方法に関するものである。更に詳しく
は、本発明は、グラフアイトと、周期律表b、
b、b属の高融点金属との接合材料を溶融相
を生じさせることなく、反応拡散固相接合によつ
て製造する方法に関する。これらの接合材料はX
線管球ターゲツト、レーザービーム反射鏡、電
極、軸受けなどの各種耐高温部品として広範な利
用が期待される。また、現在研究開発が進められ
ているトカマク型核融合炉の第1壁構成部品とし
ても期待されている。
(従来技術)
従来のグラフアイトと高融点金属との接合材料
の製造方法としては、大半はろう付け法によつて
いる。
そのろう材としては、例えば、Ti―Cu―Ni、
Ti―Cu―Si(グラフアイトと銅との接合用)、Ti
―78Ag―22Cu(グラフアイトとグラフアイトと
の接合用、USP、2739375号)、Fe―36〜45Ni―
Ti(グラフアイトとグラフアイトまたはTiとの接
合用、特許第290561号)、35Au―35Ni―30Mo
(グラフアイトとTiとの接合用)などが知られて
いる。
これらの接合材料ではろう材の融点でその耐用
温度が限定され、普通のもので1000℃以下、特殊
な場合でも1400℃を最高使用限界としている。
一方、ろう材を使わない固相接合法、例えば、
グラフアイトのブロツク上にタングステンを貼り
つける方法として、モリブデンとレニウム(重量
%50/50)混合粉ペースト剤を接合面に塗布し、
1800℃、300Kg/cm2、保持時間30分の条件下で拡
散接合る方法が知られている。この方法は高価な
レニウム貴金属を必要とする上、処理温度も1800
℃の高温を必要とする問題点がある。
(発明の目的)
本発明は前記のような従来方法の問題点を解消
するためになされたもので、その目的はグラフア
イトと高融点金属との接合を比較的低温で、高価
な金属を必要とせず、反応拡散固相接合によつて
接合材料を製造する方法を提供するにある。
(発明の構成)
本発明者は前記目的を達成すべく鋭意研究の結
果、グラフアイトと、モリブデンまたはバナジウ
ムと相互に固溶する周期律表b、b、b属
の高融点金属を接合するに際し、中間層として、
モリブデン―バナジウム合金、またはバナジウム
―チタン合金(チタンが80重量%以下)の(1)イオ
ンプレーテイング、マグネトロンスパツタリング
などによる物理蒸着膜を高融点金属の表面に配設
するか、(2)前記合金の箔を接合面に介在させ、溶
融させることなく圧着加熱すると、拡散固相反応
により強固に接合し得られることを究明し得た。
この知見に基いて本発明を完成した。
すなわち、本発明の要旨は、モリブデンまたは
バナジウムと相互に固溶する周期律表b、
b、b属の高融点金属とグラフアイトとの接合
に際し、モリブデン―バナジウム合金またはバナ
ジウム―チタン合金(ただし、チタン80重量%以
下)の物理蒸着層、それらの合金箔を用いて固相
接合することを特徴とするグラフアイトと高融点
金属との接合材料の製造方法にある。
本発明における蒸着膜厚は数μm蒸着すること
が好ましい。その組成は高融点金属基材の熱膨脹
係数を考慮して選定することがよい。組成成分の
比率を変化させて、基材の熱膨脹係数を合わすよ
うにすればよい。ただし、バナジウム―チタン合
金においてはチタンが80重量%を越えると、界面
反応層での炭化チタン濃度が高くなり、接合面の
密着性が悪くなるので、チタン80重量%以下のバ
ナジウム―チタン合金であることが必要である。
なお、グラフアイト表面に上記物理蒸着層を配
設することによつて接合することも可能である
が、この蒸着層の密着性を優れたものとするため
には、超音波洗浄等による前処理が可能で、か
つ、装着装置への取付けも容易な、高融点金属表
面にこの物理蒸着層を配設するのが有利である。
前記蒸着膜に代え、それらの合金の箔でもよ
い。箔の厚さは、50〜100μmの範囲であることが
好ましい。更に箔の両面に上記の蒸着膜を形成さ
せたものであつてもよい。比較的低温での固相拡
散が進行し、強固な接合が得られる。グラフアイ
トの接合面は予めバフ研磨し、極力清浄化してお
くことが好ましく、また、固相接合時の圧縮荷重
がグラフアイト全面に均等に加わるように、グラ
フアイトの厚さは均一で且つ平旦に仕上げるのが
よい。グラフアイトには種々の材質のものがある
が、熱膨脹係数が接合する金属基材のそれにでき
るだけ近いもの、あるいはそれより若干小さいも
のを選ぶのがよい。それは加熱または冷却時に熱
膨脹の差異によりグラフアイト層に熱応力(特に
引張応力)を生じさせないためである。
前記中間層をグラフアイトと高融点金属との間
に入れ、これを真空槽中で例えばタングステン製
圧接治具間にはさみ込み、圧接治具を油圧式プレ
スなどにより加圧し、同時に高周波加熱により所
定の温度に加熱する。これにより拡散固相反応が
進行して接着される。タングステン圧接治具には
予めBN粉末などの離型剤をスプレーしておく
と、接合材との離型が容易となる。
代表的な接合条件は5×10-6Torrの真空下で、
1300〜1450℃、平均圧力7Kg/mm2、処理時間10〜
20分である。
実施例 1
モリブデン基材に中間層としてバナジウム―モ
リブデン合金(重量で50/50)の組成の蒸着膜
を、イオンプレーテイングで約7μm施した。厚さ
0.4mmのポコグラフアイト(米国Pocoグラフアイ
ト社製、A×F―5Q)と上記のモリブデン基材
の蒸着層側とを密着させ、これを5×10-6Torr
の真空下で、平均加圧力7Kg/mm2、温度1400℃で
10分間接合処理を行つた。
得られた接合材料を、室温で引張速度0.5mm/
minで引張試験を行つた。密着力は2.7Kg/mm2で
あり、且つ破断面の観察から破壊はグラフアイト
層内で大半起つていた。即ち、グラフアイトの引
張強度以上の密着力が得られたことを示す。
実施例 2
モリブデン基材に中間層としてバナジウム60重
量%―チタン40重量%の組成の蒸着層をイオンプ
レーテイングで約5μm施した以外は実施例1と同
様な条件で接合材料を作つた。得られた接合材料
をホローカソードプラズマ銃から発生する低電圧
大電流電子ビーム(ビーム径1cm2φ)をグラフア
イト面に短時間照射することにより熱衝撃試験を
行つた。その結果、熱流束1.5KW/cm2、1秒間
の照射によりグラフアイト表面にビームによるス
ポツト状の揮発による黒化がみらたが、グラフア
イト層のスポーリング、剥離は全く生じなかつ
た。これにより優れた熱衝撃特性を有することが
分かる。
実施例 3
タングステン基材にモリブデン90重量%―バナ
ジウム10重量%の組成の蒸着膜をマグネトロンス
パツタリグで約60μm施した。マグネトロンスパ
ツタリングでは、モリブデンターゲツト(陰極)
上にバナジウム片を置いて同時スパツター法によ
り上記組成の膜を作製した。厚さ0.25mmのグラフ
アイト(東洋炭素(株)製IG―11)を用い、実施例
1と同時な接合条件で接合材料を作つた。
得られた接合材料を実施例2におけると同様な
電子ビーム熱衝撃試験で高温特性の測定を行つ
た。熱流束3.0KW/cm2、1.5秒間の照射で、グラ
フアイト及び基材の一部が第1図1,2に示した
ように電子ビームのあたつた位置に対応してスポ
ツト状に溶融した。1は表面、2は1の実線部分
の切断面の顕微鏡写真である。しかしながら、基
材には、溶融部に沿つて黒鉛層が強固に密着して
おり、接合性がよいことを示している。
実施例 4
実施例1におけるモリブデン基材に代え、チタ
ン、ジルコニウム、ハフニウム、ニオブ、タンタ
ル及びバナジウム基材を用い、実施例1と同様に
して接合材料を作つた。
実施例1とほぼ同じ結果が得られた。
実施例 5
モリブデン―50重量%バナジウム合金箔(厚み
60μm)を、モリブデン基材と厚み1mmのグラフ
アイト(米国Pocoグラフアイト社製、A×F―
5Q)との間に介在させ、5×10-6Torrの真空下、
平均加圧力10Kg/mm2、温度1400℃で10分間接合処
理した。
得られた接合材料は、インストロン引張・圧縮
試験装置を用いて、クロスヘツドスピード5mm/
secで曲げ荷重を加え、急速曲げ試験を行つた。
その結果、グラフアイトの割れにもかかわらず、
モリブデン基材からグラフアイトが剥離すること
はなかつた。
また、上記の合金箔にモリブデン―バナジウム
(50:50)の蒸着層を形成し、これを用いて同様
に接合したところ、上記同様の良好な接合が得ら
れた。この時の温度は1200℃でも充分であつた。
実施例 6
実施例2と同様にして、タングステン基材にバ
ナジウム―チタン合金蒸着層を形成して接合を行
つた。この時の合金層のチタン含有量を変化さ
せ、その接合性を評価した。その時の結果を示し
たものが次の表1である。
チタン含有率が80%を超えると所定の接合は得
られないことがわかる。接合界面のX線マイクロ
アナライザーによる分析の結果、剥離の生じる高
チタン合金層の場合には、グラフアイトとチタン
との反応によつてTiCが生成していることが確認
された。
(Industrial Application Field) The present invention relates to a method for manufacturing a bonding material between graphite and a high-melting point metal. More specifically, the present invention relates to graphite, periodic table b,
The present invention relates to a method for manufacturing a bonding material with a high melting point metal of Group B or Group B by reaction-diffusion solid phase bonding without producing a molten phase. These joining materials are
It is expected to be widely used as various high-temperature-resistant parts such as wire tube targets, laser beam reflectors, electrodes, and bearings. It is also expected to be used as the first wall component of tokamak-type fusion reactors, which are currently being researched and developed. (Prior Art) Most conventional methods for producing bonding materials between graphite and high-melting point metals are based on brazing. Examples of the brazing filler metal include Ti-Cu-Ni,
Ti-Cu-Si (for bonding graphite and copper), Ti
-78Ag-22Cu (for bonding graphite to graphite, USP, No. 2739375), Fe-36~45Ni-
Ti (for bonding graphite and graphite or Ti, Patent No. 290561), 35Au-35Ni-30Mo
(for bonding graphite and Ti), etc. are known. The usable temperature of these bonding materials is limited by the melting point of the brazing material, with the maximum usable limit being 1,000°C or less for normal materials, and 1,400°C for special cases. On the other hand, solid phase bonding methods that do not use brazing filler metals, for example,
As a method of pasting tungsten on graphite blocks, a mixed powder paste of molybdenum and rhenium (wt% 50/50) is applied to the joint surface.
A method of diffusion bonding under the conditions of 1800° C., 300 Kg/cm 2 and a holding time of 30 minutes is known. This method requires the expensive precious metal rhenium and also requires a processing temperature of 1800°C.
There is a problem that high temperature of ℃ is required. (Purpose of the Invention) The present invention was made to solve the problems of the conventional methods as described above, and its purpose is to bond graphite and high-melting point metal at a relatively low temperature, requiring the use of expensive metals. Another object of the present invention is to provide a method for producing a bonding material by reaction-diffusion solid-phase bonding. (Structure of the Invention) As a result of intensive research to achieve the above-mentioned object, the present inventor has found that when joining graphite and a high-melting point metal of Groups B, B, and B of the Periodic Table that are mutually solid-solved with molybdenum or vanadium. , as the middle layer,
(1) Placing a physical vapor deposition film of molybdenum-vanadium alloy or vanadium-titanium alloy (titanium is 80% by weight or less) by ion plating, magnetron sputtering, etc. on the surface of the high-melting point metal, or (2) It has been found that when a foil of the alloy is interposed on the bonding surface and the bonding and heating is performed without melting, a strong bond can be obtained through a diffusion solid phase reaction.
The present invention was completed based on this knowledge. That is, the gist of the present invention is that periodic table b, which is a solid solution with molybdenum or vanadium,
When bonding a high-melting point metal of group B or B to graphite, solid phase bonding is performed using a physical vapor deposition layer of molybdenum-vanadium alloy or vanadium-titanium alloy (however, titanium 80% by weight or less) or alloy foil thereof. A method for producing a bonding material between graphite and a high melting point metal is provided. The thickness of the deposited film in the present invention is preferably several μm. The composition is preferably selected in consideration of the coefficient of thermal expansion of the high melting point metal base material. The ratio of the composition components may be changed to match the coefficient of thermal expansion of the base material. However, in vanadium-titanium alloys, if titanium exceeds 80% by weight, the concentration of titanium carbide in the interfacial reaction layer increases and the adhesion of the bonding surface deteriorates. It is necessary that there be. Note that it is possible to bond by disposing the above-mentioned physical vapor deposition layer on the surface of graphite, but in order to improve the adhesion of this vapor deposition layer, pretreatment such as ultrasonic cleaning is required. It is advantageous to arrange this physical vapor deposited layer on a high melting point metal surface, which allows easy attachment to the mounting device. Instead of the vapor-deposited film, a foil of an alloy thereof may be used. Preferably, the thickness of the foil is in the range 50-100 μm. Furthermore, the above-mentioned vapor-deposited film may be formed on both sides of the foil. Solid phase diffusion progresses at relatively low temperatures, resulting in a strong bond. It is preferable to buff the bonding surface of the graphite in advance and keep it as clean as possible, and the thickness of the graphite should be uniform and smooth so that the compressive load during solid phase bonding is evenly applied to the entire surface of the graphite. It is better to finish it. There are various materials for graphite, but it is best to choose one whose coefficient of thermal expansion is as close as possible to that of the metal base material to be joined, or slightly smaller than that of the metal base material to be joined. This is because thermal stress (particularly tensile stress) is not generated in the graphite layer due to differences in thermal expansion during heating or cooling. The intermediate layer is placed between graphite and a high-melting point metal, and this is sandwiched between, for example, a tungsten pressure-welding jig in a vacuum chamber, and the pressure-welding jig is pressurized with a hydraulic press or the like, and at the same time, it is heated to a predetermined value by high-frequency heating. Heat to temperature. As a result, a diffusion solid phase reaction progresses and adhesion occurs. Spraying a mold release agent such as BN powder on the tungsten pressure welding jig in advance makes it easier to release the mold from the bonding material. Typical bonding conditions are under a vacuum of 5×10 -6 Torr.
1300~1450℃, average pressure 7Kg/ mm2 , processing time 10~
It's 20 minutes. Example 1 A vapor-deposited film having a composition of vanadium-molybdenum alloy (50/50 by weight) was applied as an intermediate layer to a molybdenum base material to a thickness of about 7 μm by ion plating. thickness
A 0.4 mm Pocographite (manufactured by Pocographite, USA, A×F-5Q) was brought into close contact with the vapor-deposited layer side of the above molybdenum base material, and this was heated to 5×10 -6 Torr.
Under vacuum, average pressure 7Kg/mm 2 and temperature 1400℃
The bonding process was performed for 10 minutes. The obtained bonding material was stretched at room temperature at a tensile rate of 0.5 mm/
A tensile test was conducted at min. The adhesion strength was 2.7 Kg/mm 2 , and observation of the fracture surface showed that most of the fracture occurred within the graphite layer. That is, it shows that adhesion strength greater than the tensile strength of graphite was obtained. Example 2 A bonding material was produced under the same conditions as in Example 1, except that a vapor deposited layer having a composition of 60% by weight vanadium and 40% by weight titanium was applied as an intermediate layer to a molybdenum base material to a thickness of about 5 μm by ion plating. A thermal shock test was conducted on the obtained bonding material by irradiating the graphite surface with a low voltage, high current electron beam (beam diameter: 1 cm 2 φ) generated from a hollow cathode plasma gun for a short period of time. As a result, when irradiated with a heat flux of 1.5 KW/cm 2 for 1 second, blackening was observed on the graphite surface due to spot-like volatilization by the beam, but no spalling or peeling of the graphite layer occurred. This shows that it has excellent thermal shock properties. Example 3 A vapor deposited film having a composition of 90% by weight molybdenum and 10% by weight vanadium was applied to a tungsten base material to a thickness of about 60 μm using a magnetron sputtering rig. In magnetron sputtering, molybdenum target (cathode)
A film having the above composition was produced by a simultaneous sputtering method with a vanadium piece placed on top. A bonding material was prepared using graphite (IG-11 manufactured by Toyo Tanso Co., Ltd.) with a thickness of 0.25 mm under the same bonding conditions as in Example 1. The high temperature properties of the obtained bonding material were measured by the same electron beam thermal shock test as in Example 2. With a heat flux of 3.0 KW/cm 2 and irradiation for 1.5 seconds, part of the graphite and base material melted in spots corresponding to the positions hit by the electron beam, as shown in Figure 1, 1 and 2. . 1 is a photomicrograph of the surface, and 2 is a photomicrograph of a cut section of the solid line portion of 1. However, the graphite layer was firmly adhered to the base material along the fused portion, indicating good bondability. Example 4 A bonding material was produced in the same manner as in Example 1 except that titanium, zirconium, hafnium, niobium, tantalum, and vanadium base materials were used in place of the molybdenum base material in Example 1. Almost the same results as in Example 1 were obtained. Example 5 Molybdenum-50% by weight vanadium alloy foil (thickness
60 μm) with a molybdenum base material and 1 mm thick graphite (manufactured by Poco Graphite, USA, A×F-
5Q), under a vacuum of 5×10 -6 Torr,
Bonding was performed at an average pressure of 10 Kg/mm 2 and a temperature of 1400° C. for 10 minutes. The obtained bonding material was tested using an Instron tensile/compression tester at a crosshead speed of 5 mm/
A rapid bending test was performed by applying a bending load at sec.
As a result, despite the cracking of graphite,
Graphite did not peel off from the molybdenum base material. Further, when a molybdenum-vanadium (50:50) vapor deposited layer was formed on the above alloy foil and bonded in the same manner using this, good bonding similar to the above was obtained. At this time, a temperature of 1200°C was sufficient. Example 6 In the same manner as in Example 2, a vanadium-titanium alloy vapor deposited layer was formed on a tungsten base material and bonding was performed. At this time, the titanium content of the alloy layer was varied and the bondability was evaluated. Table 1 below shows the results. It can be seen that when the titanium content exceeds 80%, the desired bonding cannot be achieved. Analysis of the bonded interface using an X-ray microanalyzer confirmed that in the case of a high titanium alloy layer where peeling occurs, TiC is generated by the reaction between graphite and titanium.
【表】
(発明の効果)
本発明の方法によると、使用する中間層とし
て、モリブデン―バナジウム、またはバナジウム
―チタン合金を使用するため、従来法における低
融点ろう材を使用する場合に比べて高温に耐え、
また、従来法の固相接合法に比べて貴金属を用い
ることなく、より低温によつて、極めて強固に接
合した接合材料が得られる優れた効果を有する。[Table] (Effects of the invention) According to the method of the present invention, molybdenum-vanadium or vanadium-titanium alloy is used as the intermediate layer, so the temperature is higher than that in the case of using a low melting point brazing filler metal in the conventional method. endure,
In addition, compared to conventional solid-phase bonding methods, this method has an excellent effect in that extremely strongly bonded bonding materials can be obtained at lower temperatures without using noble metals.
第1図は実施例3の方法によつて得られた接合
材料の電子顕微鏡写真で、1は表面、2は1の実
線部分の切断面を示す。
FIG. 1 is an electron micrograph of the bonding material obtained by the method of Example 3, where 1 shows the surface and 2 shows the cut section of the solid line portion of 1.
Claims (1)
る周期律表b、b、b属の高融点金属とグ
ラフアイトとの接合に際し、モリブデン―バナジ
ウム合金またはバナジウム―チタン合金(ただ
し、チタン80重量%以下)の物理蒸着層を高融点
金属表面に配設して固相接合することを特徴とす
るグラフアイトと高融点金属との接合材料の製造
方法。 2 モリブデンまたはバナジウムと相互に固溶す
る周期律表b、b、b属の高融点金属とグ
ラフアイトとの接合に際し、モリブデン―バナジ
ウム合金またはバナジウム―チタン合金(ただ
し、チタン80重量%以下)の合金箔を介して固相
接合することを特徴とするグラフアイトと高融点
金属との接合材料の製造方法。[Claims] 1. When bonding graphite with a high-melting point metal of Groups b, b, b of the periodic table that is mutually solid-solved with molybdenum or vanadium, molybdenum-vanadium alloy or vanadium-titanium alloy (however, titanium 1. A method for producing a bonding material between graphite and a high-melting point metal, which comprises disposing a physical vapor deposition layer of 80% by weight or less on the surface of the high-melting point metal and performing solid phase bonding. 2. When bonding graphite with a high-melting point metal of group b, b, or b of the periodic table that is a solid solution with molybdenum or vanadium, a molybdenum-vanadium alloy or a vanadium-titanium alloy (however, titanium 80% by weight or less) A method for producing a bonding material between graphite and a high-melting point metal, characterized by solid phase bonding via an alloy foil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23334684A JPS61111979A (en) | 1984-11-07 | 1984-11-07 | Method for producing bonding material between graphite and high melting point metal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23334684A JPS61111979A (en) | 1984-11-07 | 1984-11-07 | Method for producing bonding material between graphite and high melting point metal |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61111979A JPS61111979A (en) | 1986-05-30 |
| JPH0223499B2 true JPH0223499B2 (en) | 1990-05-24 |
Family
ID=16953704
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP23334684A Granted JPS61111979A (en) | 1984-11-07 | 1984-11-07 | Method for producing bonding material between graphite and high melting point metal |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61111979A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4740429A (en) * | 1985-07-22 | 1988-04-26 | Ngk Insulators, Ltd. | Metal-ceramic joined articles |
| JP2676413B2 (en) * | 1989-11-10 | 1997-11-17 | 山梨県 | Method for joining graphite and titanium or titanium alloy |
| CN102240836B (en) * | 2011-07-04 | 2013-01-16 | 常熟理工学院 | Vacuum brazing method for molybdenum and graphite |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5516111A (en) * | 1978-06-30 | 1980-02-04 | Nat Jutaku Kenzai | Device for fitting roof |
-
1984
- 1984-11-07 JP JP23334684A patent/JPS61111979A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61111979A (en) | 1986-05-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6528123B1 (en) | Coating system to permit direct brazing of ceramics | |
| US8557383B2 (en) | Method of producing a material composite | |
| JP2003523830A (en) | Joining method of copper and stainless steel | |
| US6315188B1 (en) | Surface preparation for high purity alumina ceramics enabling direct brazing in hydrogen atmospheres | |
| JPH04228480A (en) | Composite being stable at high temperature and preparation thereof | |
| JPH0229634B2 (en) | ||
| JPH08301669A (en) | Preparation of thermally highly loadable structural part | |
| JPH0223499B2 (en) | ||
| US4689810A (en) | Composite rotary anode for X-ray tube and process for preparing the composite | |
| JPH0520392B2 (en) | ||
| JPH10216960A (en) | Composite joint body of beryllium, copper alloy and stainless steel and composite joint method | |
| US20050091820A1 (en) | Using infrared rays for quick joining a golf club head | |
| JPS58185761A (en) | Diffusion bonding method for material comprising aluminum mainly | |
| JP4331370B2 (en) | Method for manufacturing HIP joined body of beryllium and copper alloy and HIP joined body | |
| CN115846788A (en) | Low-temperature brazing method for NiTi shape memory alloy and 316L stainless steel | |
| JP3629578B2 (en) | Ti-based material and Cu-based bonding method | |
| JP4151859B2 (en) | Method for joining sputtering target plates | |
| CN108249422A (en) | The rapid generation of graphene film surface metalation pad | |
| CN112620855A (en) | Brazing method and brazing base material to be welded obtained by brazing method | |
| JPS61288065A (en) | Target | |
| JPH06263553A (en) | Joined body of carbonaceous material to metal | |
| JP2676413B2 (en) | Method for joining graphite and titanium or titanium alloy | |
| JPH01183477A (en) | Method for bonding metal to ceramic | |
| JP2000119072A (en) | Joining method of silicon nitride and carbon steel | |
| JPH035073A (en) | Method for joining cemented carbide and steel and joined body thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |