Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPH0378181B2 - - Google Patents
[go: Go Back, main page]

JPH0378181B2 - - Google Patents

Info

Publication number
JPH0378181B2
JPH0378181B2 JP60123258A JP12325885A JPH0378181B2 JP H0378181 B2 JPH0378181 B2 JP H0378181B2 JP 60123258 A JP60123258 A JP 60123258A JP 12325885 A JP12325885 A JP 12325885A JP H0378181 B2 JPH0378181 B2 JP H0378181B2
Authority
JP
Japan
Prior art keywords
alloy
weight
carbon dioxide
reflective mirror
base material
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
JP60123258A
Other languages
Japanese (ja)
Other versions
JPS61279394A (en
Inventor
Masaki Morikawa
Akira Mori
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Materials Corp
Original Assignee
Mitsubishi Materials Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Materials Corp filed Critical Mitsubishi Materials Corp
Priority to JP60123258A priority Critical patent/JPS61279394A/en
Publication of JPS61279394A publication Critical patent/JPS61279394A/en
Publication of JPH0378181B2 publication Critical patent/JPH0378181B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Optical Elements Other Than Lenses (AREA)
  • Laser Beam Processing (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、軽量にして、高い冷却効果を有す
る炭酸ガスレーザの反射鏡材に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a carbon dioxide laser reflecting mirror material that is lightweight and has a high cooling effect.

〔従来の技術〕[Conventional technology]

一般に、炭酸ガスレーザの反射鏡として、例え
ば純銅製表面を鏡面仕上げしたものや、さらにこ
の表面に金めつきを施したものなどが使用されて
いる。
In general, as reflecting mirrors for carbon dioxide lasers, for example, mirror-finished pure copper surfaces or gold-plated surfaces are used.

しかしながら、これらの銅製反射鏡では、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。
However, with these copper 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 become exposed to the laser. Accidents have occurred in which the metal absorbs energy and melts, damaging the reflector.

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
構成する純銅や金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
を損なうことが多発していた。
To prevent such accidents, it is necessary to regularly remove deposits from the mirror surface, but the pure copper and gold plating that make up the reflective mirror are very soft, so the mirror surface is easily damaged when wiped off. Reflection properties were frequently impaired.

このようなことから、近年、炭酸ガスレーザー
の反射鏡材として、純銅に代つて硬質のMoを使
用することが定着しつつある。また、これら金属
製反射鏡材としては、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、すぐれている。
For these reasons, in recent years, the use of hard Mo instead of pure copper has become popular as a reflective mirror material for carbon dioxide lasers. Further, as these metal reflecting mirror materials, single crystal ones and polycrystal ones with fine crystal grains are particularly excellent because they have less adhesion of evaporated substances.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

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、比量の大きい(重質
の)Mo製反射鏡の重量軽減が強く望まれてい
る。
On the other hand, since carbon dioxide gas laser equipment is installed not only on ground equipment but also on space stations, there is a demand for the equipment itself to be lighter, and as a result, the relative weight ( It is strongly desired to reduce the weight of the heavy Mo reflector.

〔問題点を解決するための手段〕[Means for solving problems]

そこで、本発明者等は、上述のような観点か
ら、特にMo製の炭酸ガスレーザー反射鏡に着目
し、これを構成するMoの一部を軽量の(比重の
小さい)AlまたはAl合金で構成することにより
軽量化をはかるべく研究を行なつた結果、Moと
例えばAlは、比重(Mo:10.2,Al:2.7)、熱膨
張率(Mo:5×10-6/℃,Al:23.3×10-6
℃)、および熱伝導率(Mo:0.35cal/cm・sec・
℃,Al:0.53cal/cm・sec・℃)などの種々の点
で特性上著しく異るので、これらを高い接合強度
でろう付けすることはきわめて困難であるとの認
識があつたが、ろう材としてSi:8〜14重量%を
含有するAl合金を用い、真空中でろう付けする
と、MoとAlまたはAl合金を高い接合強度でろう
付けすることが可能となるという知見を得たので
ある。
Therefore, from the above-mentioned viewpoint, the present inventors focused on a carbon dioxide laser reflector made of Mo, and constructed a part of the Mo that constitutes it from lightweight (low specific gravity) Al or Al alloy. As a result of conducting research to reduce weight by 10 -6 /
°C), and thermal conductivity (Mo: 0.35cal/cm・sec・
It was recognized that it would be extremely difficult to braze these with high bonding strength because their properties differ significantly in various respects such as ℃, Al: 0.53 cal/cm・sec・℃). They found that if an Al alloy containing 8 to 14% Si by weight is used as the material and brazed in a vacuum, it is possible to braze Mo and Al or Al alloy with high bonding strength. .

この発明は、上記知見にもとづいてなされたも
のであつて、Mo板材からなる表面部材を、Alま
たはAl合金板材からなる基材に、Si:8〜14重
量%を含有するAl合金ろう材を用いてろう付け
してなる複合ろう付け部材で構成した炭酸ガスレ
ーザー反射鏡材に特徴を有するものである。
This invention was made based on the above knowledge, and consists of a surface member made of a Mo plate, a base material made of an Al or Al alloy plate, and an Al alloy brazing filler metal containing 8 to 14% by weight of Si. The carbon dioxide laser reflecting mirror material is made of a composite brazed member that is brazed using carbon dioxide.

なお、この発明の反射鏡材において、Al合金
ろう材のSi含有量を8〜14重量%と定めたのは、
その含有量は8重量%未満ではろう材の融点が
600℃を越えて高くなりすぎ、基材の融点より高
い融点をもつ場合が生じ、ろう付けが不可能にな
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600℃を越えるようになる
場合が生ずるばかりでなく、Mo板材との反応が
著しくなつてエロージヨンを起すようになるとい
う理由によるものである。
In addition, in the reflective mirror material of this invention, the Si content of the Al alloy brazing material is set to 8 to 14% by weight because:
If the content is less than 8% by weight, the melting point of the filler metal will decrease.
If the temperature exceeds 600℃, it may have a melting point higher than that of the base material, making brazing impossible. On the other hand, even if its content exceeds 14% by weight, This is because not only does the temperature exceed 600°C in some cases, but also the reaction with the Mo plate becomes significant, causing erosion.

〔実施例〕〔Example〕

つぎに、この発明の反射鏡材を実施例に具体的
により説明する。
Next, the reflective mirror material of the present invention will be specifically explained with reference to Examples.

実施例 1 10μmの平均結晶粒径、並びに直径:200mm×
厚さ1.1mmの寸法を有する表面部材としてのMo板
材と、直径:200mm×厚さ:20mmの寸法を有する
基材としての純Al板材(JIS 1100)とを用意し、
これら両板材を、Si:8.1重量%を含有し、残り
がAlと不可避不純物からなる組成を有する厚
さ:0.3mmのAl合金ろう材をはさんで重ね合わせ、
この状態で、10-5torrの真空中、温度:610℃に
10分間保持の条件で真空ろう付けして複合ろう付
け部材とすることにより本発明反射鏡材1を製造
した。
Example 1 Average grain size of 10 μm and diameter: 200 mm×
Prepare a Mo plate material as a surface member with dimensions of 1.1 mm in thickness and a pure Al plate material (JIS 1100) as a base material with dimensions of diameter: 200 mm x thickness: 20 mm.
These two plates were stacked together with a 0.3 mm thick Al alloy brazing filler metal containing 8.1% by weight of Si and the remainder consisting of Al and unavoidable impurities.
In this state, in a vacuum of 10 -5 torr, temperature: 610℃
Reflective mirror material 1 of the present invention was manufactured by vacuum brazing under conditions of holding for 10 minutes to obtain a composite brazed member.

実施例 2 直径:100mm×厚さ:1.1mmの寸法を有する単結
晶Moからなる表面部材としてのMo板材と、直
径:100mm×厚さ:20mmの寸法を有する基板とし
てのAl合金板材(JIS 3003)とを用意し、これ
ら両板材を、Si:11.3重量%を含有し、残りがAl
と不可避不純物からなる組成を有する厚さ:0.3
mmのAl合金ろう材をはさんで重ね合わせ、この
状態で、10-5torrの真空中、温度:595℃に10分
間保持の条件で真空ろう付けして複合ろう付け部
材とすることにより本発明反射鏡材2を製造し
た。
Example 2 A Mo plate material as a surface member made of single crystal Mo having dimensions of diameter: 100 mm x thickness: 1.1 mm, and an Al alloy plate material (JIS 3003) as a substrate having dimensions of diameter: 100 mm x thickness: 20 mm. ) and both of these plates contained 11.3% by weight of Si and the rest was Al.
Thickness: 0.3 with a composition consisting of and unavoidable impurities
This is achieved by stacking Al alloy brazing filler metal of 1.5 mm in size and vacuum brazing it in a vacuum of 10 -5 torr at a temperature of 595°C for 10 minutes to create a composite brazed member. Invention reflective mirror material 2 was manufactured.

実施例 3 表面部材として、直径:150mm×厚さ:1.1mmの
寸法を有し、かつ平均結晶粒径を5μmに調整し
た多結晶MoからなるMo板材を、また基材とし
て、直径:150mm×厚さ:20mmの寸法を有し、か
つSi:1重量%を含有し、残りがAlと不可避不
純物からなる組成を有するAl合金板材をそれぞ
れ用意し、これら両板材を、Si:13.9重量%を含
有し、残りがAlと不可避不純物からなる組成を
有する厚さ:0.3mmのAl合金ろう材をはさんで重
ね合わせ、この状態で、10-5torrの真空中、温
度:595℃に10分間保持の条件で真空ろう付けし
て複合ろう付け部材とすることにより本発明反射
鏡材を製造した。
Example 3 As a surface member, a Mo plate made of polycrystalline Mo having dimensions of diameter: 150 mm x thickness: 1.1 mm and with an average crystal grain size adjusted to 5 μm was used, and as a base material, a Mo plate material having dimensions of diameter: 150 mm x thickness: 1.1 mm was used as a base material. Al alloy plates having a thickness of 20 mm and containing 1% by weight of Si and the rest consisting of Al and unavoidable impurities were prepared. Al alloy brazing filler metal with a thickness of 0.3 mm and having a composition consisting of aluminum and unavoidable impurities are stacked together, and in this state, in a vacuum of 10 -5 torr at a temperature of 595°C for 10 minutes. The reflective mirror material of the present invention was manufactured by vacuum brazing under holding conditions to obtain a composite brazed member.

〔発明の効果〕〔Effect of the invention〕

この結果得られた本発明反射鏡材1〜3につい
て、それぞれ重量を測定したところ、2.1Kg,0.5
Kg、および1.2Kgを示し、この重量はいずれも全
体をMoで製造した場合の約1/3を示すものであ
つて、著しい軽量化がなされたことを示してい
る。
When the weights of the reflective mirror materials 1 to 3 of the present invention obtained as a result were measured, they were 2.1Kg and 0.5Kg.
Kg and 1.2Kg, both of which are approximately 1/3 of the weight of the case where the entire body was made of Mo, indicating a significant weight reduction.

また、本発明反射鏡材1〜3について、それぞ
れMo板材の表面を凹面研摩して鏡面に仕上げ、
一方基材の大部には8本の放射状冷却水路を設け
ることによつて炭酸ガスレーザー用反射鏡を製造
し、これを、それぞれ前者の直径:200mmを有す
る大型のものについては、出力:10kW、時間:
10時間、または後者の2つの直径:100mmおよび
150mmを有する小型のものについては、出力:
5kW、時間:20時間の条件で実用に供したが、
基材がMoに比して冷却効果の高いAlまたはAl合
金で構成されていることと相まつて、使用後の反
射鏡には全く変形が見られなかつた。
In addition, regarding the reflective mirror materials 1 to 3 of the present invention, the surface of the Mo plate material is polished to a mirror surface by concave polishing,
On the other hand, a reflector for carbon dioxide laser is manufactured by providing eight radial cooling channels in most of the base material, and the former has a large diameter of 200 mm and has an output of 10 kW. ,time:
10 hours, or the latter two diameters: 100mm and
For the small size with 150mm output:
It was put into practical use under the conditions of 5kW and 20 hours.
Coupled with the fact that the base material was made of Al or Al alloy, which has a higher cooling effect than Mo, no deformation was observed in the reflector after use.

上述のように、この発明の反射鏡材は、軽質の
AlまたはAl合金板材の基材に表面部材のMo板材
がろう付けされたものからなるので軽量であるば
かりでなく、基材を構成するAlおよびAl合金板
材は高い冷却効果をもつので、炭酸ガスレーザー
の反射鏡として用いた場合に著しくすぐれた性能
を長期に亘つて発揮するのである。
As mentioned above, the reflective mirror material of the present invention is lightweight.
Since it is made of Al or Al alloy plate base material and Mo plate material as the surface member brazed, it is not only lightweight, but also the Al and Al alloy plate material that makes up the base material has a high cooling effect, so carbon dioxide gas When used as a laser reflector, it exhibits outstanding performance over a long period of time.

Claims (1)

【特許請求の範囲】[Claims] 1 Mo板材からなる表面部材を、AlまたはAl合
金板材からなる基材に、Si:8〜14重量%を含有
するAl合金ろう材を用いてろう付けしてなる複
合ろう付け部材で構成したことを特徴とする炭酸
ガスレーザの反射鏡材。
1. A composite brazed member formed by brazing a surface member made of a Mo plate material to a base material made of an Al or Al alloy plate material using an Al alloy brazing material containing 8 to 14% by weight of Si. Reflective mirror material for carbon dioxide lasers.
JP60123258A 1985-06-06 1985-06-06 Brazed composite member Granted JPS61279394A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60123258A JPS61279394A (en) 1985-06-06 1985-06-06 Brazed composite member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60123258A JPS61279394A (en) 1985-06-06 1985-06-06 Brazed composite member

Publications (2)

Publication Number Publication Date
JPS61279394A JPS61279394A (en) 1986-12-10
JPH0378181B2 true JPH0378181B2 (en) 1991-12-12

Family

ID=14856115

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60123258A Granted JPS61279394A (en) 1985-06-06 1985-06-06 Brazed composite member

Country Status (1)

Country Link
JP (1) JPS61279394A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63208802A (en) * 1987-02-26 1988-08-30 Mitsubishi Metal Corp Lighter composite brazed member

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5261152A (en) * 1975-11-14 1977-05-20 Tokyo Shibaura Electric Co Brazing method

Also Published As

Publication number Publication date
JPS61279394A (en) 1986-12-10

Similar Documents

Publication Publication Date Title
KR960010166B1 (en) Diffusion bonded sputtering target assembly and method for manufacturing same
US20030218054A1 (en) Method for forming sputter target assemblies
CN103695898B (en) A kind of titanium alloy surface cermet composite coating and preparation technology thereof
FR2698634A1 (en) Inorganic paint resistant to high temperatures, methods of application and manufacture thereof and spaceship using this paint.
US5965278A (en) Method of making cathode targets comprising silicon
JP2001010874A (en) Method for producing composite material of inorganic material and metal containing aluminum and related products
EP0301492B1 (en) Method for bonding cubic boron nitride sintered compact
US6884511B1 (en) Method for brazing ceramic-containing bodies, and articles made thereby
JPH0378181B2 (en)
JP2536491B2 (en) Composite brazing member for reflector
JP3660014B2 (en) Sputtering target
JPH07278804A (en) Pure Ti target for sputtering thin film formation
JPS62234692A (en) Composite brazing member
JPH028828B2 (en)
JPH0685004B2 (en) High durability infrared reflector
JPH0338946B2 (en)
FR2585730A1 (en) Process for deposition of metals as a thin layer on a nonmetallic substrate, with intermediate deposition of hydrides by reactive cathodic sputtering
JPS6254570A (en) Production of composite brazed member
JP2560126B2 (en) Synchrotron radiation reflection mirror
JPS6281267A (en) Production of composite brazing member
JPH0336402B2 (en)
JPH0575507B2 (en)
JPH0369862B2 (en)
JPH0338948B2 (en)
JPS6254569A (en) Production of composite brazed member