JPH028828B2 - - Google Patents
Info
- Publication number
- JPH028828B2 JPH028828B2 JP60184759A JP18475985A JPH028828B2 JP H028828 B2 JPH028828 B2 JP H028828B2 JP 60184759 A JP60184759 A JP 60184759A JP 18475985 A JP18475985 A JP 18475985A JP H028828 B2 JPH028828 B2 JP H028828B2
- Authority
- JP
- Japan
- Prior art keywords
- pure
- alloy
- brazing
- brazed
- layer
- 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
Description
〔産業上の利用分野〕
この発明は、軽量にして、冷却効果が高く、例
えば炭酸ガスレーザーの反射鏡や、真空炉の内壁
材などとして用いるのに適した複合ろう付け部材
の製造法に関するものである。
〔従来の技術〕
従来、一般に、例えば炭酸ガスの反射鏡とし
て、純Cu製表面を鏡面仕上げしたものや、さら
にこの表面にAuめつきを施したものなどが用い
られている。
しかしながら、これらのCu製反射鏡では、レ
ーザー照射時間が長くなると、鏡面に加工材から
発生した金属や非金属の蒸気が蒸着し、その反射
率が低下するようになるばかりでなく、鏡面がレ
ーザーのエネルギーを吸収して溶融し、反射鏡を
破損してしまうなどの事故が発生している。
このような事故を防止するには、定期的に鏡面
の蒸着物を除去しなければならないが、反射鏡を
構成する純CuやAuめつきは非常に軟らかいため
に、ふき取るときに鏡面を傷つけ易く、反射特性
を損うことが多発していた。
このようなことから、近年、炭酸ガスレーザー
の反射鏡の材料として、純Cuに代つて硬質のMo
を使用することが定着しつつある。このMo製反
射鏡としては、特に単結晶のものや、微細な結晶
粒の多結晶のものが蒸発物の付着も少なく、すぐ
れた性能を発揮するものである。
〔発明が解決しようとする問題点〕
一方、炭酸ガスレーザー装置は、地上設備ばか
りでなく、宇宙ステーシヨンにも設置されるもの
であるため、装置自体の軽量化が要求されるよう
になつており、これに伴つて、比重の大きい(重
質の)Mo製反射鏡の重量軽減が強く望まてい
る。
〔問題点を解決するための手段〕
そこで、本発明者等は、上述のような観点か
ら、Mo製反射鏡などのMo部材や、Mo合金部
材、さらに同様に重質のW部材やW合金部材に着
目し、これの軽量比をはかるべく研究を行なつた
結果、純Mo、Mo合金、純W、およびW合金の
うちのいずれかからなる部材の一部を軽量の(比
重の小さい)純AlまたはAl合金で構成し、一方、
例えば純Moと純Alは、比重(純Mo:10.2、純
Al:2.7)、熱膨張率(純Mo:5×10-6/℃、純
Al:23.3×10-6/℃)、および熱伝導率(純Mo:
0.35cal/cm―s―℃、純Al:0.53cal/cm―s―
℃)など種々の点で特性上著しく異なるので、こ
れら両部材を高い接合強度でろう付けすることは
きわめて困難であるが、上記の純Mo、Mo合金、
純W、およびW合金のうちのいずれかからなる部
材のろう付け面に、予め、イオンプレーテイング
法やめつき法などの公知の手段により平均層厚で
0.01〜50μmのCu層を固着形成しておき、この状
態で、前記Cu層を介し、Si:6〜14重量%を含
有するAl合金からなるろう材をはさんで純Alま
たはAl合金部材のろう付け面と重ね合わせ、真
空中で加熱すると、高い接合強度でのろう付けが
可能となるという知見を得たのである。
この発明は、上記知見にもとづいてなされたも
ので、純Mo、Mo合金、純W、およびW合金の
うちのいずれかからなる被ろう付け部材のろう付
け面に、平均層厚で0.01〜50μmのCu層を固着形
成しておき、この被ろう付け部材を、前記Cu層
を介し、Si:6〜14重量%を含有するAl合金か
らなるろう材を用いて、純AlまたはAl合金から
なる基体に真空ろう付けすることからなる複合ろ
う付け部材の製造法に特徴を有するものである。
なお、この発明の方法において、Cu層の平均
層厚を0.01〜50μmに限定したのは、その平均層
厚が0.01μm未満では所望の接合強度を確保する
ことができず、一方その平均層厚が50μmを越え
ると、Cu層形成時に発生した内部残留歪によつ
て、ろう付け時に被ろう付け部材のろう付け面か
らCu層を剥離するようになるという理由にもと
づくものである。また、同じくろう材のSi含有量
については、その含有量が6重量%未満では、ろ
う材の融点が660℃を越えて高くなりすぎ、基体
の融点より高いろう付け温度を必要とする場合が
生じるようになつて、ろう付けが不可能となる場
合が生じ、一方その含有量が14重量%を越えて
も、ろう材の融点が660℃を越えるようになる場
合が生ずるようになるばかりでなく、被ろう付け
部材との反応が著しくなつてエロージヨンを起す
ようになることから、その含有量を6〜14重量%
と定めたのである。
〔実施例〕
つぎに、この発明の方法を実施例により説明す
る。
被ろう付け部材として、それぞれ第1表に示さ
れる組成を有し、かつ直径:200mm×厚さ:2mm
の寸法をもつた各種部材を用意し、この被ろう付
け部材の片側面に、予め、第1表に示される形成
手段にて同じく第1表に示される平均層厚のCu
層を固着形成し、ついで、この被ろう付け部材
を、同じく第1表に示される組成、並びにいずれ
も直径:200mm×厚さ:18mmの寸法をもつた基体
の上面に、前記Cu層を介し、同じく第1表に示
される組成および平均層厚を有するAl合金から
なるろう材をはさんだ状態で重ね合わせ、この上
に3Kgの重りを置き、1×10-5torrの真空中、
600〜630℃の範囲内の所定温度に
[Industrial Application Field] This invention relates to a method for manufacturing a composite brazed member that is lightweight, has a high cooling effect, and is suitable for use as, for example, a reflector for a carbon dioxide laser or an inner wall material for a vacuum furnace. It is. [Prior Art] Conventionally, for example, as a carbon dioxide gas reflecting mirror, a mirror-finished pure Cu surface or a mirror-finished surface, or a mirror plated with Au plating, etc., have been used. However, with these Cu reflectors, when the laser irradiation time becomes long, metal and non-metal vapors generated from the processed materials are deposited on the mirror surface, which not only reduces the reflectance, but also causes the mirror surface to be exposed to the laser. Accidents have occurred in which the mirror absorbs energy and melts, damaging the reflector. To prevent such accidents, it is necessary to regularly remove deposits from the mirror surface, but since the pure Cu and Au plating that makes up the reflective mirror is very soft, it is easy to damage the mirror surface when wiping it off. , the reflective properties were frequently impaired. For this reason, in recent years, hard Mo has been used as a material for carbon dioxide laser reflectors instead of pure Cu.
The use of . As for this Mo reflector, single-crystal ones and polycrystal ones with fine crystal grains exhibit excellent performance with less adhesion of evaporated matter. [Problems to be solved by the invention] On the other hand, since carbon dioxide laser devices are installed not only in ground equipment but also in space stations, there is a growing demand for the device itself to be lightweight. , Along with this, there is a strong desire to reduce the weight of Mo reflectors that have a high specific gravity (heavy). [Means for Solving the Problems] Therefore, from the above-mentioned viewpoint, the present inventors developed Mo members such as Mo reflectors, Mo alloy members, and similar heavy W members and W alloys. As a result of focusing on components and conducting research to measure their weight ratios, we found that some components made of pure Mo, Mo alloy, pure W, and W alloy are lightweight (low specific gravity). Composed of pure Al or Al alloy, while
For example, the specific gravity of pure Mo and pure Al (pure Mo: 10.2, pure
Al: 2.7), thermal expansion coefficient (pure Mo: 5×10 -6 /℃, pure
Al: 23.3×10 -6 /℃), and thermal conductivity (pure Mo:
0.35cal/cm-s-℃, pure Al: 0.53cal/cm-s-
It is extremely difficult to braze these two parts with high bonding strength because their properties differ significantly in various respects such as
The brazing surface of a member made of either pure W or W alloy is coated with an average layer thickness in advance by known means such as ion plating or plating.
A Cu layer of 0.01 to 50 μm is fixedly formed, and in this state, a pure Al or Al alloy member is sandwiched between the Cu layer and a brazing filler metal made of an Al alloy containing 6 to 14% by weight of Si. They discovered that if they are placed over the brazing surface and heated in a vacuum, brazing with high bonding strength is possible. This invention was made based on the above knowledge, and is based on the above-mentioned findings. A Cu layer is fixedly formed in advance, and the member to be brazed is made of pure Al or an Al alloy using a brazing material made of an Al alloy containing 6 to 14% by weight of Si, via the Cu layer. This method is characterized by a method for manufacturing a composite brazing member that is vacuum brazed to a base. In addition, in the method of this invention, the average layer thickness of the Cu layer is limited to 0.01 to 50 μm because if the average layer thickness is less than 0.01 μm, it is not possible to secure the desired bonding strength. This is based on the reason that if the thickness exceeds 50 μm, the internal residual strain generated during the formation of the Cu layer causes the Cu layer to peel off from the brazing surface of the component to be brazed during brazing. Similarly, regarding the Si content of the filler metal, if the content is less than 6% by weight, the melting point of the filler metal will be too high, exceeding 660°C, and a brazing temperature higher than the melting point of the base material may be required. As a result, brazing becomes impossible in some cases, and even if the content exceeds 14% by weight, the melting point of the brazing filler metal often exceeds 660°C. The content should be reduced to 6 to 14% by weight, as the reaction with the parts to be brazed would become significant and cause erosion.
It was established that [Example] Next, the method of the present invention will be explained with reference to an example. Each member to be brazed has the composition shown in Table 1, and diameter: 200 mm x thickness: 2 mm.
Prepare various members with the dimensions of , and pre-coat one side of the member to be brazed with a layer of Cu having the average layer thickness also shown in Table 1 using the forming means shown in Table 1.
The layer is fixedly formed, and then this member to be brazed is placed on the upper surface of a substrate having the composition shown in Table 1 and dimensions of 200 mm in diameter and 18 mm in thickness, with the Cu layer interposed therebetween. , a brazing filler metal made of an Al alloy having the composition and average layer thickness shown in Table 1 was stacked on top of each other, a 3 kg weight was placed on top of the brazing filler metal, and in a vacuum of 1×10 -5 torr,
to a predetermined temperature within the range of 600-630℃
【表】【table】
第1表に示される結果から、本発明法1〜8に
おいては、いずれも従来ろう付け接合がきわめて
困難であるとされていた純Mo、Mo合金、純W、
およびW合金のうちのいずれかからなる部材と、
純AlまたはAl合金からなる部材とを強固な接合
強度でろう付けすることができることが明らかで
ある。
上述のように、この発明の方法によれば、純
Mo、Mo合金、純W、およびW合金のうちのい
ずれかからなる重質の部材の一部を軽質の純Al
またはAl合金で置換することが可能となるので、
各種重質部材の軽量化が可能となり、さらに純
AlまたはAl合金はすぐれた冷却作用をもつので、
例えば炭酸ガスレーザー用反射鏡や真空炉の内壁
材などの製造に適用した場合、これら部材はすぐ
れた性能を長期に亘つて発揮するようになるなど
工業上有用な効果が得られるのである。
From the results shown in Table 1, in methods 1 to 8 of the present invention, pure Mo, Mo alloy, pure W, which were conventionally considered to be extremely difficult to join by brazing,
and a member made of any one of W alloy,
It is clear that a member made of pure Al or an Al alloy can be brazed with strong bonding strength. As mentioned above, according to the method of this invention, pure
Part of a heavy member made of Mo, Mo alloy, pure W, or W alloy is replaced with light pure Al
Or it can be replaced with Al alloy, so
It is now possible to reduce the weight of various heavy components, making it even more pure.
Al or Al alloy has an excellent cooling effect, so
For example, when applied to the manufacture of reflectors for carbon dioxide lasers and inner wall materials for vacuum furnaces, these materials exhibit industrially useful effects such as superior performance over a long period of time.
Claims (1)
ちのいずれかからなる被ろう付け部材のろう付け
面に、平均層厚で0.01〜50μmのCu層を固着形成
し、 ついで、この被ろう付け部材を、前記Cu層を
介し、Si:6〜14重量%を含有するAl合金から
なるろう材を用いて、純AlまたはAl合金からな
る基体に真空ろう付けすることを特徴とする複合
ろう付け部材の製造法。[Claims] 1. A Cu layer having an average layer thickness of 0.01 to 50 μm is fixedly formed on the brazing surface of a member to be brazed made of pure Mo, Mo alloy, pure W, or W alloy. Then, this member to be brazed is vacuum brazed to a base made of pure Al or an Al alloy through the Cu layer using a brazing material made of an Al alloy containing 6 to 14% by weight of Si. A method for manufacturing a composite brazing member characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60184759A JPS6245466A (en) | 1985-08-22 | 1985-08-22 | Production of composite brazing member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60184759A JPS6245466A (en) | 1985-08-22 | 1985-08-22 | Production of composite brazing member |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6245466A JPS6245466A (en) | 1987-02-27 |
| JPH028828B2 true JPH028828B2 (en) | 1990-02-27 |
Family
ID=16158836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60184759A Granted JPS6245466A (en) | 1985-08-22 | 1985-08-22 | Production of composite brazing member |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6245466A (en) |
-
1985
- 1985-08-22 JP JP60184759A patent/JPS6245466A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6245466A (en) | 1987-02-27 |
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