JP2009293108A - METHOD FOR PRODUCING Al-BASED ALLOY SPUTTERING TARGET MATERIAL - Google Patents
METHOD FOR PRODUCING Al-BASED ALLOY SPUTTERING TARGET MATERIAL Download PDFInfo
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- JP2009293108A JP2009293108A JP2008150527A JP2008150527A JP2009293108A JP 2009293108 A JP2009293108 A JP 2009293108A JP 2008150527 A JP2008150527 A JP 2008150527A JP 2008150527 A JP2008150527 A JP 2008150527A JP 2009293108 A JP2009293108 A JP 2009293108A
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 58
- 239000000956 alloy Substances 0.000 title claims abstract description 58
- 238000005477 sputtering target Methods 0.000 title claims abstract description 43
- 239000013077 target material Substances 0.000 title claims abstract description 42
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 23
- 239000000843 powder Substances 0.000 claims abstract description 95
- 238000000034 method Methods 0.000 claims abstract description 56
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 40
- 238000002844 melting Methods 0.000 claims abstract description 38
- 230000008018 melting Effects 0.000 claims abstract description 38
- 239000002245 particle Substances 0.000 claims abstract description 35
- 238000002156 mixing Methods 0.000 claims abstract description 20
- 239000011812 mixed powder Substances 0.000 claims description 10
- 229910052804 chromium Inorganic materials 0.000 claims description 7
- 229910052735 hafnium Inorganic materials 0.000 claims description 7
- 229910052715 tantalum Inorganic materials 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 229910052750 molybdenum Inorganic materials 0.000 claims description 6
- 229910052758 niobium Inorganic materials 0.000 claims description 6
- 229910052721 tungsten Inorganic materials 0.000 claims description 6
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- 229910052726 zirconium Inorganic materials 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 239000000203 mixture Substances 0.000 abstract description 16
- 229910052751 metal Inorganic materials 0.000 description 14
- 239000002184 metal Substances 0.000 description 14
- 238000005204 segregation Methods 0.000 description 11
- 238000001513 hot isostatic pressing Methods 0.000 description 10
- 229910001362 Ta alloys Inorganic materials 0.000 description 6
- 238000000280 densification Methods 0.000 description 6
- 239000000047 product Substances 0.000 description 6
- 238000009718 spray deposition Methods 0.000 description 6
- 239000002775 capsule Substances 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 238000009689 gas atomisation Methods 0.000 description 4
- 238000000889 atomisation Methods 0.000 description 3
- 238000000151 deposition Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000003801 milling Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910001215 Te alloy Inorganic materials 0.000 description 2
- 229910001873 dinitrogen Inorganic materials 0.000 description 2
- 238000011978 dissolution method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000583 Nd alloy Inorganic materials 0.000 description 1
- 229910052779 Neodymium Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052747 lanthanoid Inorganic materials 0.000 description 1
- 150000002602 lanthanoids Chemical class 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000010299 mechanically pulverizing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 238000000988 reflection electron microscopy Methods 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229910052596 spinel Inorganic materials 0.000 description 1
- 239000011029 spinel Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000009692 water atomization Methods 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based alloys
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/3407—Cathode assembly for sputtering apparatus, e.g. Target
- C23C14/3414—Metallurgical or chemical aspects of target preparation, e.g. casting, powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physical Vapour Deposition (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
Description
本発明は、歩留に優れるAl基合金スパッタリングターゲット材の製造方法、及びこの方法で製造されるAl基合金スパッタリングターゲット材に関するものである。 The present invention relates to a method for producing an Al-based alloy sputtering target material excellent in yield, and an Al-based alloy sputtering target material produced by this method.
Al基合金スパッタリングターゲット材は、主として溶解法、スプレイフォーミング法、粉末法などで製造される。 The Al-based alloy sputtering target material is manufactured mainly by a melting method, a spray forming method, a powder method, or the like.
溶解法は、溶融金属を型で成形する方法であり、様々な組成の合金スパッタリングターゲット材を製造できる。しかし、合金添加量が多い場合、溶解法では、粗大金属間化合物が晶出し、これが起点となって鋳造または塑性加工中に割れが生ずる。また、TaなどのようにAlと比べて融点や密度が高い高融点・高密度の元素を合金元素として用いる場合には、凝固偏析が生ずる。そのため、Taなどを含有するAl基合金スパッタリングターゲット材を溶解法で製造すると、歩留が低下する。 The melting method is a method of forming molten metal with a mold, and can produce alloy sputtering target materials having various compositions. However, when the amount of the alloy added is large, in the melting method, a coarse intermetallic compound is crystallized and this is the starting point, and cracks occur during casting or plastic working. Further, when a high melting point / high density element having a higher melting point and density than Al, such as Ta, is used as an alloy element, solidification segregation occurs. Therefore, when an Al-based alloy sputtering target material containing Ta or the like is manufactured by a melting method, the yield is lowered.
スプレイフォーミング法は、溶融金属(溶湯)をガスによってアトマイズし、半凝固状態に急冷した粒子を堆積させ、所定形状のプリフォームを形成する方法である。しかしTaのような融点が高い高融点元素を含むAl基合金では、温度低下に伴い溶湯ノズル内で閉塞が生ずる。またAl−Ta合金などでは、溶湯および液滴温度が高くなるため、液相を多く含む粒子が堆積時に飛散する。その結果、歩留が低下する。 The spray forming method is a method of forming a preform having a predetermined shape by atomizing a molten metal (molten metal) with a gas and depositing rapidly cooled particles in a semi-solid state. However, in an Al-based alloy containing a high melting point element such as Ta having a high melting point, clogging occurs in the molten metal nozzle as the temperature decreases. Moreover, in an Al-Ta alloy etc., since molten metal and droplet temperature become high, the particle | grains with many liquid phases will disperse at the time of deposition. As a result, the yield decreases.
単体金属粉末同士を混合する粉末法は、溶解法で製造が困難な組成のAl基合金を製造するのに用いられることが多い。しかし、希土類元素単体の金属粉末は酸化しやすいため、粉末法を、希土類元素を含有するAl基合金スパッタリングターゲット材の製造に適用することは難しい。 The powder method of mixing single metal powders is often used to produce an Al-based alloy having a composition that is difficult to produce by a melting method. However, since the rare earth element simple metal powder is easily oxidized, it is difficult to apply the powder method to the production of an Al-based alloy sputtering target material containing a rare earth element.
一方、特許文献1や特許文献2には、溶解法と粉末法を組み合わせてスパッタリングターゲット材を製造する方法が開示されている。このうち特許文献1には、まず(1)不活性ガスアトマイズ法によってGe−Te合金粉末およびSb−Te合金粉末を製造し、次いで(2)前記2種の合金粉末を混合・焼結して、Ge−Sb−Te系スパッタリングターゲット材を製造する方法が開示されている。また、特許文献2には、急冷凝固法により製造した固体合金粉末とPt単体の金属粉末とを混合し、この混合粉末をHIP(Hot Isostatic Pressing)処理で緻密化することによってスパッタリングターゲット材を製造する方法が開示されている。
本発明の目的は、希土類元素と、Alよりも高融点の高融点元素を含有するAl基合金スパッタリングターゲット材を歩留良く製造できる方法を提供することにある。 An object of the present invention is to provide a method capable of producing an Al-based alloy sputtering target material containing a rare earth element and a refractory element having a melting point higher than that of Al with a high yield.
上記目的を達成し得た本発明の製造方法は、希土類元素と、Alよりも高融点の高融点元素Xとを含有するAl基合金スパッタリングターゲット材の製造方法であって、アトマイズ法によって製造した希土類元素を含有するAl基合金の第1粉末を用意する工程、前記第1粉末と、前記高融点元素Xから構成される1種以上の第2粉末とを混合する工程、及び前記第1粉末と前記第2粉末の混合粉末を緻密化する工程を含み、前記混合工程において、前記第1粉末の最大粒径(a)が10〜200μmであり、前記第2粉末の最大粒径(b)が10〜150μmであり、(a)と(b)との比((a)/(b))が0.5〜5であるところに要旨を有するものである。 The production method of the present invention that has achieved the above object is a method for producing an Al-based alloy sputtering target material containing a rare earth element and a refractory element X having a melting point higher than that of Al, and is produced by an atomization method. Preparing a first powder of an Al-based alloy containing a rare earth element, mixing the first powder with one or more second powders composed of the refractory element X, and the first powder. And a step of densifying the mixed powder of the second powder, wherein in the mixing step, the maximum particle size (a) of the first powder is 10 to 200 μm, and the maximum particle size (b) of the second powder Is 10 to 150 μm, and the ratio ((a) / (b)) between (a) and (b) is 0.5 to 5.
ここで、(1)希土類元素(以下「REM」と略称する)はNd及び/又はYであること、(2)高融点元素Xは、Ti、Zr、Hf、V、Nb、Ta、Cr、Mo、WおよびNiよりなる群から選ばれる少なくとも1種であることが好ましい。本発明の好ましい製造方法では、REMを1.0〜10原子%および他の元素Xを0.5〜5原子%含有するAl基合金スパッタリングターゲット材を製造する。 Here, (1) the rare earth element (hereinafter abbreviated as “REM”) is Nd and / or Y, and (2) the refractory element X is Ti, Zr, Hf, V, Nb, Ta, Cr, It is preferably at least one selected from the group consisting of Mo, W and Ni. In a preferred production method of the present invention, an Al-based alloy sputtering target material containing 1.0 to 10 atomic percent of REM and 0.5 to 5 atomic percent of other element X is produced.
本発明は、上記製造方法で製造されたAl基合金スパッタリングターゲット材も提供する。 The present invention also provides an Al-based alloy sputtering target material produced by the above production method.
本発明によれば、アトマイズ法によって製造したAl−REM系Al基合金(以下「Al−REM合金」と略称する。)の第1粉末と、Alよりも高融点の高融点元素(以下、Xで代表させる場合がある。)から構成される第2粉末とを混合する際に、それらの最大粒径および比を適切に制御することによって、Al−REM−X系Al基合金(以下「Al−REM−X合金」と略称する。)のスパッタリングターゲット材を歩留良く製造できる。 According to the present invention, a first powder of an Al-REM-based Al-based alloy (hereinafter abbreviated as “Al-REM alloy”) manufactured by an atomizing method, and a refractory element (hereinafter, X When mixing with the second powder composed of the Al-REM-X-based Al-based alloy (hereinafter referred to as “Al”) by appropriately controlling the maximum particle size and ratio thereof. -REM-X alloy ") can be manufactured with good yield.
本発明者は、酸化し易い希土類元素(REM)と、Alよりも高融点の高融点元素(X)を含有するAl−REM−X合金スパッタリングターゲット材を、偏析が生ずることなく、歩留良く製造できる方法を提供するため、検討を重ねてきた。その結果、Al−REM合金の第1粉末と、高融点元素Xの第2粉末を混合するに当たり、上記第1粉末の最大粒径(a)および上記第2粉末の最大粒径(b)、並びにこれらの比((a)/(b))を適正に制御すると、所期の目的が達成されることを見出し、本発明を完成した。詳細には、本発明の方法を用いれば、粉末の混合時、混合粉末の運搬時、及び緻密化処理時(特にHIP処理のカプセル充填時)の振動偏析やころがり偏析が防止され、スパッタリングターゲット材の歩留が向上することが分かった。 The inventor of the present invention has a high yield without causing segregation of an Al-REM-X alloy sputtering target material containing a rare-earth element (REM) that is easily oxidized and a refractory element (X) having a melting point higher than that of Al. Considerations have been made to provide methods that can be manufactured. As a result, in mixing the first powder of the Al-REM alloy and the second powder of the high melting point element X, the maximum particle size (a) of the first powder and the maximum particle size (b) of the second powder, And when these ratios ((a) / (b)) were appropriately controlled, it was found that the intended purpose was achieved, and the present invention was completed. Specifically, the use of the method of the present invention prevents vibration segregation and rolling segregation during powder mixing, mixed powder transportation, and densification processing (particularly during HIP processing capsule filling), and a sputtering target material. It was found that the yield improved.
本発明の製造方法は、
(1)アトマイズ法によって製造したAl−REM合金の第1粉末を用意する工程、
(2)上記の第1粉末と、Alよりも高融点の高融点元素Xから構成される第2粉末とを混合する工程、及び
(3)上記第1粉末と上記第2粉末の混合粉末を緻密化する工程
を含む。また上記工程(3)で得られた緻密体に、必要に応じて、塑性加工(鍛造、圧延、押出加工等)、旋盤加工、フライス加工等を施しても良い。以下、上記工程(1)〜(3)について、順に詳しく説明する。
The production method of the present invention comprises:
(1) A step of preparing a first powder of an Al-REM alloy manufactured by an atomizing method,
(2) a step of mixing the first powder and a second powder composed of a high melting point element X having a melting point higher than that of Al; and (3) a mixed powder of the first powder and the second powder. Including a step of densification. Further, the dense body obtained in the above step (3) may be subjected to plastic working (forging, rolling, extrusion processing, etc.), lathe processing, milling, etc., as necessary. Hereinafter, the steps (1) to (3) will be described in detail.
[工程(1)]
工程(1)では、アトマイズ法によって製造したAl−REM合金の第1粉末を用意する。本発明の製造方法では、REM単体の金属粉末ではなく、Al−REM合金粉末(第1粉末)を使用するので、REMの酸化を防止できる。
[Step (1)]
In step (1), a first powder of an Al-REM alloy manufactured by an atomizing method is prepared. In the production method of the present invention, since the Al-REM alloy powder (first powder) is used instead of the metal powder of REM alone, REM oxidation can be prevented.
第1粉末を製造するためのアトマイズ法は特に限定されず、Al合金分野で良く知られているアトマイズ法(例えばガスアトマイズ法、水アトマイズ法、遠心力アトマイズ法など)を使用できる。アトマイズ法によれば、製造する粉末の粒度分布を制御しやすいなどの利点がある。 The atomizing method for producing the first powder is not particularly limited, and an atomizing method (for example, a gas atomizing method, a water atomizing method, a centrifugal atomizing method, etc.) well known in the Al alloy field can be used. According to the atomization method, there are advantages such as easy control of the particle size distribution of the powder to be produced.
[工程(2)]
次に、本発明の方法を最も特徴付ける工程(2)について説明する。
工程(2)では、上記のAl−REM合金粉末(第1粉末)と、Alよりも高融点の高融点元素(X)から構成される第2粉末とを混合する。このようにAl−REM合金粉末を製造した後に高融点元素(X)を添加することによって、Al−REM−X合金スパッタリングターゲット材を歩留良く製造できる。
[Step (2)]
Next, step (2) that characterizes the method of the present invention will be described.
In the step (2), the Al-REM alloy powder (first powder) is mixed with the second powder composed of the high melting point element (X) having a higher melting point than Al. Thus, by adding the high melting point element (X) after producing the Al-REM alloy powder, the Al-REM-X alloy sputtering target material can be produced with good yield.
上記高融点元素Xは、Alよりも融点が高い元素であり、具体的には、Ti、Zr、Hf、V、Nb、Ta、Cr、Mo、Wの第4〜6族元素、およびNiが挙げられる。これらの高融点元素は、1種のみを含有しても良いし、2種以上を含有しても良い。後に詳しく説明するが、これらの元素と、希土類元素を含むAl基合金スパッタリングターゲット材は、特に、光情報記録媒体のAl基合金反射膜などの製造に好適に用いられるが、上記の高融点元素は、Al基合金の熱伝導率の低下や耐食性の向上などに寄与することが知られている。すなわち、本発明の方法によって得られるAl基合金スパッタリングターゲット材の合金組成およびその含有量は、当該スパッタリングターゲット材を用いて得られるAl合金膜の用途や特性などの関係で適宜決定されるものである。詳細は後述する。 The high melting point element X is an element having a higher melting point than Al. Specifically, Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W group 4-6 elements, and Ni are included. Can be mentioned. These high melting point elements may contain only 1 type and may contain 2 or more types. As will be described in detail later, an Al-based alloy sputtering target material containing these elements and rare earth elements is particularly suitable for the production of an Al-based alloy reflective film of an optical information recording medium. Is known to contribute to a decrease in the thermal conductivity of Al-based alloys and an improvement in corrosion resistance. That is, the alloy composition of the Al-based alloy sputtering target material obtained by the method of the present invention and the content thereof are appropriately determined in relation to the use and characteristics of the Al alloy film obtained using the sputtering target material. is there. Details will be described later.
上記高融点元素Xから構成される第2粉末は、1種のみの高融点元素の単体金属粉末であっても、2種以上の高融点元素を含む合金粉末であっても良い。また、組成が異なる2種類以上の第2粉末を併用しても良い。 The second powder composed of the refractory element X may be a single metal powder of only one refractory element or an alloy powder containing two or more refractory elements. Moreover, you may use together 2 or more types of 2nd powder from which a composition differs.
本発明の製造方法において、第2粉末の製造方法は特に限定されず、機械的粉砕法、化学反応法、電解析出法、アトマイズ法のいずれの方法でも製造可能である。例えば第2粉末は、高融点元素Xの単体金属を溶製し、鋳型で固めた後、機械的に粉砕することで製造できる。 In the production method of the present invention, the production method of the second powder is not particularly limited, and any of a mechanical pulverization method, a chemical reaction method, an electrolytic deposition method, and an atomization method can be used. For example, the second powder can be manufactured by melting a simple metal of the high melting point element X, solidifying it with a mold, and then mechanically pulverizing it.
本発明では、上記工程(2)の混合工程において、第1粉末の最大粒径(a)および第2粉末の最大粒径(b)、並びにこれらの比((a)/(b))を適正に制御することに大きな特徴がある。具体的には、第1粉末の最大粒径(a)が10〜200μmであり、前記第2粉末の最大粒径(b)が10〜150μmであり、(a)と(b)との比((a)/(b))が0.5〜5となるように混合する。後記する実施例に示すように、最大粒径およびその比を適正に制御することによって、粉末の混合時、混合粉末の運搬時、及び工程(3)での緻密化処理時(特にHIP処理のカプセル充填時)の振動偏析やころがり偏析が防止されるため、スパッタリングターゲット材の歩留が向上する。 In the present invention, in the mixing step of the above step (2), the maximum particle size (a) of the first powder, the maximum particle size (b) of the second powder, and the ratio ((a) / (b)) A major feature is proper control. Specifically, the maximum particle size (a) of the first powder is 10 to 200 μm, the maximum particle size (b) of the second powder is 10 to 150 μm, and the ratio between (a) and (b) Mix so that ((a) / (b)) is 0.5-5. As shown in the examples described later, by appropriately controlling the maximum particle size and the ratio thereof, the powder is mixed, the mixed powder is transported, and the densification process in the step (3) (especially the HIP process). Since vibration segregation and rolling segregation during capsule filling are prevented, the yield of the sputtering target material is improved.
ここで粉末の最大粒径とは、光回析・散乱に基づくFraunhofer法によって粉末の粒度分布を測定し、粒径と頻度の関係を明らかにした際に、大粒径側の頻度が3.0%以下を削除したときの粒径の最大値を意味する。本実施例では、粒径分布と最大粒径は、レーザー光回析・散乱式の粒度分析計“日機装(株)MICROTRAC HRA(MODEL:9320−X100”によって測定した。 Here, the maximum particle size of the powder means that when the particle size distribution of the powder is measured by the Fraunhofer method based on light diffraction / scattering and the relationship between the particle size and the frequency is clarified, the frequency on the large particle size side is 3. It means the maximum value of the particle size when 0% or less is deleted. In this example, the particle size distribution and the maximum particle size were measured by a laser diffraction / scattering type particle size analyzer “Nikkiso Co., Ltd. MICROTRAC HRA (MODEL: 9320-X100)”.
まず、第1粉末(Al−REM合金粉末)の最大粒径(a)は、10μm以上(好ましくは50μm以上)、200μm以下(好ましくは150μm以下)である。(a)が200μmを超えると、第1粉末間を第2粉末が移動しやすくなり、混合時・運搬時・緻密化処理時に偏析が生じ易くなる。なお、合金粉末の最大粒径の下限は、実用可能な範囲で設定されたものである。 First, the maximum particle size (a) of the first powder (Al-REM alloy powder) is 10 μm or more (preferably 50 μm or more) and 200 μm or less (preferably 150 μm or less). When (a) exceeds 200 μm, the second powder easily moves between the first powders, and segregation is likely to occur during mixing, transportation, and densification treatment. The lower limit of the maximum particle size of the alloy powder is set within a practical range.
また、第2粉末(他の元素Xの金属または合金粉末)の最大粒径(b)は、10μm以上(好ましくは30μm以上)、150μm以下(好ましくは100μm以下、より好ましくは45μm以下)である。(b)が150μmを超えると、工程(2)での混合度が低下して、偏析が生じ易くなる。なお、金属または合金粉末の最大粒径の下限は、実用可能な範囲で設定されたものである。 The maximum particle size (b) of the second powder (metal or alloy powder of other element X) is 10 μm or more (preferably 30 μm or more), 150 μm or less (preferably 100 μm or less, more preferably 45 μm or less). . When (b) exceeds 150 μm, the degree of mixing in the step (2) is lowered and segregation is likely to occur. The lower limit of the maximum particle size of the metal or alloy powder is set within a practical range.
更に、第1粉末と第2粉末との最大粒径の比である(a)/(b)は、0.5以上(好ましくは0.7以上、より好ましくは2以上)、5以下(好ましくは4.5以下、より好ましくは4以下)である。(a)/(b)が5を超えると、第2粉末が第1粉末間を移動しやすくなり、混合時・運搬時・緻密化処理時に偏析が生じ易くなる。一方(a)/(b)が0.5未満であると、特に密度の大きいX元素から構成される第2粉末を使用する場合、粉末が移動しにくくなって工程(2)での混合度が低下し、偏析が生じ易くなる。 Furthermore, (a) / (b), which is the ratio of the maximum particle size of the first powder to the second powder, is 0.5 or more (preferably 0.7 or more, more preferably 2 or more), 5 or less (preferably Is 4.5 or less, more preferably 4 or less. When (a) / (b) exceeds 5, the second powder easily moves between the first powders, and segregation is likely to occur during mixing, transportation, and densification. On the other hand, when (a) / (b) is less than 0.5, when the second powder composed of the X element having a particularly high density is used, the powder becomes difficult to move and the degree of mixing in the step (2) Decreases and segregation is likely to occur.
上述した(a)、(b)および(a)/(b)は、アトマイズ法などによって製造した第1粉末および第2粉末を、例えば、工程(2)の前に分級(篩分け)などを行うことによって上記範囲に制御することができる。 The above-mentioned (a), (b) and (a) / (b) indicate that the first powder and the second powder produced by the atomizing method are classified (sieved) before the step (2), for example. It is possible to control within the above range by performing.
上記の第1粉末および第2粉末工程の混合手段は特に限定されず、周知の方法、例えばV型混合ミルなどを使用できる。 The mixing means of said 1st powder and 2nd powder process is not specifically limited, A well-known method, for example, a V-type mixing mill etc., can be used.
[工程(3)]
上記工程(2)で得られた混合粉末を、工程(3)で緻密化することによってAl基合金スパッタリングターゲット材(緻密体)を製造できる。なお工程(3)で得られた緻密体に、必要に応じてさらなる加工(例えば塑性加工、旋盤加工、フライス加工など)を施して、さらに形状を付与してもよい。
[Step (3)]
An Al-based alloy sputtering target material (dense body) can be produced by densifying the mixed powder obtained in the step (2) in the step (3). Note that the dense body obtained in the step (3) may be further processed (for example, plastic processing, lathe processing, milling, etc.) as necessary to further give the shape.
混合粉末の緻密化手段は、特に限定されないが、均一な緻密体が得られるHIP処理が好ましい。HIP処理は、例えば80MPa以上の圧力下、400〜600℃の温度で行うことが好ましい。HIP処理の時間は、おおむね1〜10時間の範囲内とすることが好ましい。 The means for densifying the mixed powder is not particularly limited, but HIP treatment capable of obtaining a uniform dense body is preferable. The HIP treatment is preferably performed at a temperature of 400 to 600 ° C. under a pressure of 80 MPa or more, for example. It is preferable that the time for the HIP treatment is approximately in the range of 1 to 10 hours.
なおHIP処理以外の緻密化手段も使用でき、例えば押出加工することによって、塑性加工と共に、混合粉末の緻密化を行っても良い。 Note that densification means other than HIP treatment can also be used. For example, the mixed powder may be densified together with plastic working by extrusion.
必要に応じて行なわれる上記の塑性加工、旋盤加工、フライス加工などは特に限定されず、周知の手段を採用できる。 The plastic processing, lathe processing, milling, and the like performed as necessary are not particularly limited, and well-known means can be employed.
本発明の方法は、Al−希土類元素(REM)−Alよりも高融点元素(X)合金スパッタリングターゲット材の製造に好適に用いられる。ここで、REMには、ランタノイド元素(LaからLuまでの15元素)およびSc(スカンジウム)とY(イットリウム)が挙げられる。好ましくは、Ndおよび/またはYである。高融点元素Xは上述したとおりである。 The method of the present invention is more suitably used for the production of a refractory element (X) alloy sputtering target material than Al-rare earth element (REM) -Al. Here, REM includes lanthanoid elements (15 elements from La to Lu), Sc (scandium), and Y (yttrium). Nd and / or Y are preferred. The high melting point element X is as described above.
本発明の方法によって得られるスパッタリングターゲット材は、特に、光情報記録用Al基合金反射膜の製造に好適に用いられる。上記反射膜は、例えば、特開2005−158236号公報に詳細に記載されている。上記公報には、REM(好ましくはNd及び/又はY)を1.0〜10.0原子%、およびTi、Zr、Hf、V、Nb、Ta、Cr、Mo、WおよびNiよりなる群から選ばれる少なくとも1種を0.5〜5原子%含有するAl基合金反射膜は、低熱伝導率、低溶融温度、高耐食性および高反射率といった優れた特性を有しており、レーザー等でマーキングを行う光情報記録媒体に好適に用いられること、このようなAl基合金反射膜は、同一組成のスパッタリングターゲット材を用いて形成できることが詳しく記載されている。 The sputtering target material obtained by the method of the present invention is particularly suitably used for the production of an Al-based alloy reflective film for optical information recording. The reflective film is described in detail in, for example, Japanese Patent Application Laid-Open No. 2005-158236. In the above publication, REM (preferably Nd and / or Y) is from 1.0 to 10.0 atomic%, and Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W and Ni. The Al-based alloy reflective film containing 0.5 to 5 atomic% of at least one selected has excellent characteristics such as low thermal conductivity, low melting temperature, high corrosion resistance and high reflectance, and is marked with a laser or the like. It is described in detail that the Al-based alloy reflective film can be formed using a sputtering target material having the same composition.
上記公報に記載の反射膜について、より詳細に説明すると以下のとおりである。まず、Al基合金にREMを含有させることによって、その熱伝導率を大きく低減することができる。REMの中でもNdおよびYは、その熱伝導率低減効果が大きい。REM量の好ましい範囲は、1.0原子%以上10原子%以下、より好ましくは2.0原子%以上7原子%以下である。 The reflective film described in the above publication will be described in detail as follows. First, the thermal conductivity can be greatly reduced by including REM in the Al-based alloy. Among REMs, Nd and Y have a large effect of reducing thermal conductivity. A preferable range of the REM amount is 1.0 atom% or more and 10 atom% or less, more preferably 2.0 atom% or more and 7 atom% or less.
Al−REM合金に、さらにTi、Zr、Hf、V、Nb、Ta、Cr、Mo、WおよびNiの少なくとも1種を含有させることによって、耐食性が向上する。また、これら第4〜6族元素およびNiは、Al基合金の熱伝導率を下げることができる。これら元素の中でもTi、Hf、TaおよびCrは、その耐食性改善効果が大きい。これらの好ましい含有量は、0.5原子%以上5原子%以下であり、より好ましくは1.0原子%以上3.0原子%以下である。 Corrosion resistance is improved by adding at least one of Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W and Ni to the Al-REM alloy. Further, these Group 4 to 6 elements and Ni can lower the thermal conductivity of the Al-based alloy. Among these elements, Ti, Hf, Ta and Cr have a great effect of improving the corrosion resistance. These preferable contents are 0.5 atomic% or more and 5 atomic% or less, and more preferably 1.0 atomic% or more and 3.0 atomic% or less.
よって、本発明の方法によって得られるスパッタリングターゲット材を、上記反射膜の成膜に用いるときは、上記反射膜の組成と同じになるように、当該スパッタリングターゲット材の組成を、REM(好ましくはNd及び/又はY)を1.0〜10原子%、Ti、Zr、Hf、V、Nb、Ta、Cr、Mo、WおよびNiよりなる群から選ばれる少なくとも1種の高融点元素を0.5〜5原子%含有するAl基合金とすれば良い。 Therefore, when the sputtering target material obtained by the method of the present invention is used for the formation of the reflective film, the composition of the sputtering target material is set to REM (preferably Nd) so as to be the same as the composition of the reflective film. And / or Y) 1.0 to 10 atomic%, at least one refractory element selected from the group consisting of Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W and Ni is 0.5. An Al-based alloy containing ˜5 atomic% may be used.
上記組成のスパッタリングターゲット材を製造するに当たっては、上記工程(1)において、REMを1.0〜10原子%程度で含有するAl−REM合金の第1粉末を用い、上記工程(2)において、上記高融点元素Xが0.5〜5原子%となる量の第2粉末を用いれば良い。 In producing the sputtering target material having the above composition, in the step (1), the first powder of Al-REM alloy containing about 1.0 to 10 atomic% of REM is used in the step (1). What is necessary is just to use the 2nd powder of the quantity from which the said high melting point element X becomes 0.5-5 atomic%.
なお、上記に挙げた本発明の方法によって得られるスパッタリングターゲット材の組成は、好ましい態様であって、これに限定する趣旨ではない。本発明は、希土類元素(REM)とAlよりも高融点元素(X)を含むAl−REM−X合金スパッタリングターゲット材を歩留まり良く製造できる方法を開示するものであって、その組成や含有量は、当該スパッタリングターゲット材を用いて得られる反射膜などの用途や特性に応じて、適宜適切に決定されるものだからである。よって、上記公報に記載の組成と異なる反射膜を製造する場合は、当該異なる反射膜の組成に応じたスパッタリングターゲット材の組成とすれば良く、このようなものも本発明の範囲内に包含される。 Note that the composition of the sputtering target material obtained by the above-described method of the present invention is a preferred embodiment and is not intended to be limited thereto. The present invention discloses a method capable of producing an Al-REM-X alloy sputtering target material containing a rare earth element (REM) and a higher melting point element (X) than Al with a high yield, and the composition and content thereof are as follows. This is because it is appropriately determined appropriately according to the application and characteristics of the reflective film obtained using the sputtering target material. Therefore, when a reflective film having a composition different from that described in the above publication is manufactured, the composition of the sputtering target material may be set according to the composition of the different reflective film, and such a composition is also included in the scope of the present invention. The
以下、実施例を挙げて本発明をより具体的に説明するが、本発明は以下の実施例によって制限を受けるものではなく、上記・下記の趣旨に適合し得る範囲で適当に変更を加えて実施することも勿論可能であり、それらはいずれも本発明の技術的範囲に包含される。 EXAMPLES Hereinafter, the present invention will be described in more detail with reference to examples. However, the present invention is not limited by the following examples, and appropriate modifications are made within a range that can meet the above and the following purposes. Of course, it is possible to implement them, and they are all included in the technical scope of the present invention.
実施例1
種々の方法によってAl−6原子%Nd−1原子%Ta合金スパッタリングターゲット材を製造し、歩留まりを評価した。
Example 1
The Al-6 atomic% Nd-1 atomic% Ta alloy sputtering target material was manufactured by various methods, and the yield was evaluated.
まず、窒素ガスアトマイズ法によってAl−6.06原子%Nd合金粉末(第1粉末)を製造した。この第1粉末に、Taが1原子%となる量で第2粉末を添加し、V型混合ミルで混合した。なお第1粉末の最大粒径(a)および第2粉末の最大粒径(b)が下記表1に示すように、最大粒径は篩にて調整した。なお最大粒径の測定は、前述した方法で測定した。 First, an Al-6.06 atomic% Nd alloy powder (first powder) was produced by a nitrogen gas atomization method. To this first powder, the second powder was added in an amount such that Ta was 1 atomic%, and mixed with a V-type mixing mill. The maximum particle size (a) of the first powder and the maximum particle size (b) of the second powder were adjusted with a sieve as shown in Table 1 below. The maximum particle size was measured by the method described above.
次にこの混合粉末をカプセル管に充填し、脱気・封入した。その後、最高温度550℃・保持時間2時間・圧力85MPaの条件でHIP処理し、Al−6原子%Nd−1原子%Ta合金スパッタリングターゲット材を製造した。 Next, this mixed powder was filled into a capsule tube, and deaerated and sealed. Then, HIP process was carried out under the conditions of a maximum temperature of 550 ° C., a holding time of 2 hours, and a pressure of 85 MPa to produce an Al-6 atomic% Nd-1 atomic% Ta alloy sputtering target material.
比較のため、以下に記載の溶解法およびスプレイフォーミング法を用い、Al−6原子%Nd−1原子%Ta合金スパッタリングターゲット材を製造した。 For comparison, an Al-6 atomic% Nd-1 atomic% Ta alloy sputtering target material was manufactured using the melting method and spray forming method described below.
溶解法は、以下のようにして行なった。真空誘導溶解炉を用い、アルミナやスピネル等の耐火物るつぼを使用して、溶解温度1350℃、不活性ガス(Ar)雰囲気で溶解し、銅鋳型または鉄鋳型(210mm×210mm×高さ50mm)に鋳造した。得られた鋳塊の底部(5〜10mm)を切り捨てた後、厚さ10mm(製品厚さ5mm+5mm)となるように切断し、施盤加工によってAl−6原子%Nd−1原子%Ta合金スパッタリングターゲット材を製作した。 The dissolution method was performed as follows. Using a vacuum induction melting furnace, using a refractory crucible such as alumina or spinel, melting in an inert gas (Ar) atmosphere at a melting temperature of 1350 ° C, copper mold or iron mold (210 mm x 210 mm x height 50 mm) Cast into. The bottom (5 to 10 mm) of the resulting ingot was cut off, then cut to a thickness of 10 mm (product thickness 5 mm + 5 mm), and an Al-6 atomic% Nd-1 atomic% Ta alloy sputtering target by lathing. Made the material.
スプレイフォーミング法は、以下のようにして行なった。スプレイフォーミング装置(住友重機械工業(株)製)を用い、出湯温度1300℃・溶湯ノズル内径φ5.5mmの条件で、窒素ガスアトマイズによって液滴をつくり、コレクター上に堆積させた。得られたプリフォームをカプセル管に入れて脱気・封入後、温度550℃・圧力85MPa・保持時間2時間の条件でHIP処理を実施した。得られた緻密体を鍛造、圧延後に、厚さ10mm(製品厚さ5mm+5mm)となるように切断し、施盤加工によってAl−6原子%Nd−1原子%Ta合金スパッタリングターゲット材を製作した。 The spray forming method was performed as follows. Using a spray forming apparatus (manufactured by Sumitomo Heavy Industries, Ltd.), droplets were formed by nitrogen gas atomization and deposited on the collector under conditions of a hot water temperature of 1300 ° C. and a molten metal nozzle inner diameter of 5.5 mm. The preform obtained was put into a capsule tube, degassed and sealed, and then subjected to HIP treatment under conditions of a temperature of 550 ° C., a pressure of 85 MPa, and a holding time of 2 hours. The obtained dense body was forged and rolled, then cut to a thickness of 10 mm (product thickness 5 mm + 5 mm), and an Al-6 atomic% Nd-1 atomic% Ta alloy sputtering target material was manufactured by lathing.
このようにして得られたスパッタリングターゲット材の製品歩留は、製品重量/溶解重量で評価した。 The product yield of the sputtering target material thus obtained was evaluated by product weight / dissolved weight.
これらの結果を表1に示す。本実施例では、一般基準に従い、歩留が40%以上のものを合格(○)、40%未満のものを不合格(×)と評価した。なお、歩留ロスには、偏析によって生じたものに加えて、塑性加工時や機械加工時に生じたものも含まれる。 These results are shown in Table 1. In this example, according to the general criteria, a yield of 40% or more was evaluated as pass (◯), and a yield of less than 40% was evaluated as reject (x). The yield loss includes not only those caused by segregation but also those produced during plastic working or machining.
表1の結果から明らかなように、混合時の第1粉末の最大粒径(a)、第2粉末の最大粒径(b)、および(a)/(b)が本発明で規定する要件を満足する方法で製造したNo.3、4、6、9、および10は、いずれも、製品歩留が向上した。 As is clear from the results of Table 1, the maximum particle size (a) of the first powder, the maximum particle size (b) of the second powder, and (a) / (b) at the time of mixing are the requirements specified by the present invention. No. produced by a method satisfying 3, 4, 6, 9, and 10 all improved product yield.
これに対し、本発明で規定する上記要件のいずれかが本発明の範囲を満足しないNo.5、7、および8は、いずれも、製品歩留が低下した。また、従来法である溶解法(No.1)やスプレイフォーミング法(No.2)では、所望の製品歩留は得られなかった。 On the other hand, if any of the above requirements defined in the present invention does not satisfy the scope of the present invention. For all of 5, 7, and 8, the product yield decreased. Moreover, the desired product yield was not obtained by the conventional dissolution method (No. 1) or spray forming method (No. 2).
Claims (5)
アトマイズ法によって製造した希土類元素を含有するAl基合金の第1粉末を用意する工程、
前記第1粉末と、前記高融点元素Xから構成される1種以上の第2粉末とを混合する工程、及び
前記第1粉末と前記第2粉末の混合粉末を緻密化する工程を含み、
前記混合工程において、前記第1粉末の最大粒径(a)が10〜200μmであり、前記第2粉末の最大粒径(b)が10〜150μmであり、(a)と(b)との比((a)/(b))が0.5〜5であることを特徴とするAl基合金スパッタリングターゲット材の製造方法。 A method for producing an Al-based alloy sputtering target material comprising a rare earth element and a refractory element X having a melting point higher than that of Al,
Preparing a first powder of an Al-based alloy containing a rare earth element manufactured by an atomizing method;
Mixing the first powder and one or more second powders composed of the refractory element X; and densifying the mixed powder of the first powder and the second powder;
In the mixing step, the maximum particle size (a) of the first powder is 10 to 200 μm, the maximum particle size (b) of the second powder is 10 to 150 μm, and (a) and (b) The method for producing an Al-based alloy sputtering target material, wherein the ratio ((a) / (b)) is 0.5 to 5.
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PCT/JP2009/060476 WO2009151032A1 (en) | 2008-06-09 | 2009-06-08 | Manufacturing method for aluminum-based alloy sputtering target |
CN200980121618.0A CN102057074A (en) | 2008-06-09 | 2009-06-08 | Manufacturing method for aluminum-based alloy sputtering target |
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JP2015096647A (en) * | 2013-10-08 | 2015-05-21 | 株式会社フルヤ金属 | Alloy target of aluminum and rare earth element and manufacturing method of the same |
CN105132759A (en) * | 2015-09-29 | 2015-12-09 | 济南大学 | Al-Ta intermediate alloy and preparation method and application thereof |
CN116904942A (en) * | 2023-08-01 | 2023-10-20 | 苏州六九新材料科技有限公司 | Aluminum-based alloy target and preparation method thereof |
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