TWI815025B - Sputtering target and method for manufacturing the same - Google Patents
Sputtering target and method for manufacturing the same Download PDFInfo
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- TWI815025B TWI815025B TW109124278A TW109124278A TWI815025B TW I815025 B TWI815025 B TW I815025B TW 109124278 A TW109124278 A TW 109124278A TW 109124278 A TW109124278 A TW 109124278A TW I815025 B TWI815025 B TW I815025B
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- cylindrical base
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- 238000005477 sputtering target Methods 0.000 title claims abstract description 61
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 39
- 238000004544 sputter deposition Methods 0.000 title abstract description 17
- 239000000463 material Substances 0.000 claims abstract description 245
- 239000013077 target material Substances 0.000 claims abstract description 41
- 230000004323 axial length Effects 0.000 claims abstract description 13
- 230000002093 peripheral effect Effects 0.000 claims description 23
- 238000005259 measurement Methods 0.000 claims description 16
- 229910000679 solder Inorganic materials 0.000 claims description 9
- 238000002844 melting Methods 0.000 claims description 5
- 230000008018 melting Effects 0.000 claims description 5
- 238000006073 displacement reaction Methods 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 abstract description 23
- 238000000034 method Methods 0.000 abstract description 22
- 239000011230 binding agent Substances 0.000 abstract 1
- 229910052738 indium Inorganic materials 0.000 description 11
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 11
- 239000000523 sample Substances 0.000 description 10
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 8
- 239000000758 substrate Substances 0.000 description 8
- 239000002184 metal Substances 0.000 description 6
- 238000003825 pressing Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 239000010408 film Substances 0.000 description 4
- 238000011084 recovery Methods 0.000 description 4
- 239000011787 zinc oxide Substances 0.000 description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 3
- 239000004809 Teflon Substances 0.000 description 3
- 229920006362 Teflon® Polymers 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 230000005856 abnormality Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 229910052733 gallium Inorganic materials 0.000 description 3
- AMGQUBHHOARCQH-UHFFFAOYSA-N indium;oxotin Chemical compound [In].[Sn]=O AMGQUBHHOARCQH-UHFFFAOYSA-N 0.000 description 3
- 238000003672 processing method Methods 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- 229910007604 Zn—Sn—O Inorganic materials 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000005401 electroluminescence Methods 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- HRHKULZDDYWVBE-UHFFFAOYSA-N indium;oxozinc;tin Chemical compound [In].[Sn].[Zn]=O HRHKULZDDYWVBE-UHFFFAOYSA-N 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 238000005476 soldering Methods 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910014472 Ca—O Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000846 In alloy Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910020923 Sn-O Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910003077 Ti−O Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910007541 Zn O Inorganic materials 0.000 description 1
- HMRQSZREPBVTLZ-UHFFFAOYSA-N [Ge]=O.[Zn] Chemical compound [Ge]=O.[Zn] HMRQSZREPBVTLZ-UHFFFAOYSA-N 0.000 description 1
- SSWDODWDXMYUNE-UHFFFAOYSA-N [O--].[O--].[Ca++].[Zn++] Chemical compound [O--].[O--].[Ca++].[Zn++] SSWDODWDXMYUNE-UHFFFAOYSA-N 0.000 description 1
- YEDFFHSKPYNLND-UHFFFAOYSA-N [O--].[O--].[O--].[Ca++].[Sn+4] Chemical compound [O--].[O--].[O--].[Ca++].[Sn+4] YEDFFHSKPYNLND-UHFFFAOYSA-N 0.000 description 1
- FDLSOIWNAZCAMB-UHFFFAOYSA-N [O--].[O--].[O--].[Mg++].[Sn+4] Chemical compound [O--].[O--].[O--].[Mg++].[Sn+4] FDLSOIWNAZCAMB-UHFFFAOYSA-N 0.000 description 1
- PZSJVIFHTPOZKX-UHFFFAOYSA-N [O-2].[O-2].[In+3].[Cu+2] Chemical compound [O-2].[O-2].[In+3].[Cu+2] PZSJVIFHTPOZKX-UHFFFAOYSA-N 0.000 description 1
- UDCHZHQIJDRAIT-UHFFFAOYSA-N [W]=O.[Zn].[In] Chemical compound [W]=O.[Zn].[In] UDCHZHQIJDRAIT-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- ZTHDAQDISBUGRY-UHFFFAOYSA-N aluminum copper oxygen(2-) Chemical compound [O--].[O--].[Al+3].[Cu++] ZTHDAQDISBUGRY-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 1
- HERMVCOJYLRNMJ-UHFFFAOYSA-N barium(2+);oxygen(2-);tin(4+) Chemical compound [O-2].[O-2].[O-2].[Sn+4].[Ba+2] HERMVCOJYLRNMJ-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- CDZGJSREWGPJMG-UHFFFAOYSA-N copper gallium Chemical compound [Cu].[Ga] CDZGJSREWGPJMG-UHFFFAOYSA-N 0.000 description 1
- BERDEBHAJNAUOM-UHFFFAOYSA-N copper(I) oxide Inorganic materials [Cu]O[Cu] BERDEBHAJNAUOM-UHFFFAOYSA-N 0.000 description 1
- KRFJLUBVMFXRPN-UHFFFAOYSA-N cuprous oxide Chemical compound [O-2].[Cu+].[Cu+] KRFJLUBVMFXRPN-UHFFFAOYSA-N 0.000 description 1
- 229940112669 cuprous oxide Drugs 0.000 description 1
- AJNVQOSZGJRYEI-UHFFFAOYSA-N digallium;oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[Ga+3].[Ga+3] AJNVQOSZGJRYEI-UHFFFAOYSA-N 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 229910001195 gallium oxide Inorganic materials 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- RHZWSUVWRRXEJF-UHFFFAOYSA-N indium tin Chemical compound [In].[Sn] RHZWSUVWRRXEJF-UHFFFAOYSA-N 0.000 description 1
- BDVZHDCXCXJPSO-UHFFFAOYSA-N indium(3+) oxygen(2-) titanium(4+) Chemical compound [O-2].[Ti+4].[In+3] BDVZHDCXCXJPSO-UHFFFAOYSA-N 0.000 description 1
- ATFCOADKYSRZES-UHFFFAOYSA-N indium;oxotungsten Chemical compound [In].[W]=O ATFCOADKYSRZES-UHFFFAOYSA-N 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- 239000004973 liquid crystal related substance Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- PNHVEGMHOXTHMW-UHFFFAOYSA-N magnesium;zinc;oxygen(2-) Chemical compound [O-2].[O-2].[Mg+2].[Zn+2] PNHVEGMHOXTHMW-UHFFFAOYSA-N 0.000 description 1
- 238000001755 magnetron sputter deposition Methods 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- CAQRFUZAAAEILW-UHFFFAOYSA-N oxygen(2-) tin(4+) titanium(4+) Chemical compound [O--].[O--].[O--].[O--].[Ti+4].[Sn+4] CAQRFUZAAAEILW-UHFFFAOYSA-N 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- YVTHLONGBIQYBO-UHFFFAOYSA-N zinc indium(3+) oxygen(2-) Chemical compound [O--].[Zn++].[In+3] YVTHLONGBIQYBO-UHFFFAOYSA-N 0.000 description 1
- -1 zinc tin germanium oxide Chemical compound 0.000 description 1
- BNEMLSQAJOPTGK-UHFFFAOYSA-N zinc;dioxido(oxo)tin Chemical compound [Zn+2].[O-][Sn]([O-])=O BNEMLSQAJOPTGK-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- 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
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
- C04B37/023—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
- C04B37/026—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/32—Gas-filled discharge tubes
- H01J37/34—Gas-filled discharge tubes operating with cathodic sputtering
- H01J37/3411—Constructional aspects of the reactor
- H01J37/3414—Targets
- H01J37/3423—Shape
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/32—Gas-filled discharge tubes
- H01J37/34—Gas-filled discharge tubes operating with cathodic sputtering
- H01J37/3488—Constructional details of particle beam apparatus not otherwise provided for, e.g. arrangement, mounting, housing, environment; special provisions for cleaning or maintenance of the apparatus
- H01J37/3491—Manufacturing of targets
Abstract
Description
本發明係關於一種具備圓筒形基材和複數個圓筒形靶(target)材的濺鍍靶(sputtering target)及其製造方法,尤其關於一種可使用已彎曲變形而呈翹曲的圓筒形基材作為材料之濺鍍靶的製造方法。 The present invention relates to a sputtering target having a cylindrical base material and a plurality of cylindrical target materials and a manufacturing method thereof. In particular, it relates to a sputtering target that can use a cylinder that has been bent and deformed to become warped. A method for manufacturing a sputtering target using a shaped base material as a material.
在製造有機EL(Electroluminescence,電致發光)、液晶顯示器(display)或觸控面板(touch panel)、和其他顯示裝置(device)時,在用以形成由ITO(indium tin oxide,銦錫氧化物)等所構成之透明導電薄膜的濺鍍中,係以使用在平板狀之基材上接合靶材而成之平板型濺鍍靶的磁控濺鍍(magnetron sputtering)為主流。 When manufacturing organic EL (Electroluminescence, electroluminescence), liquid crystal display (display) or touch panel (touch panel), and other display devices (device), it is used to form ITO (indium tin oxide, indium tin oxide) ), etc., magnetron sputtering using a flat sputtering target in which a target is bonded to a flat substrate is the mainstream.
近年來,一種旋轉式濺鍍(rotary sputtering)已獲得了實用化,該旋轉式濺鍍係使在圓筒形基材之外周面接合靶材而成的圓筒形濺鍍靶繞著軸線旋轉而進行濺鍍。依據此種旋轉式濺鍍,可實現遠比平板型濺鍍靶更高的使用效率,從而具有可獲得高生產力等的優點。 In recent years, a type of rotary sputtering (rotary sputtering) in which a cylindrical sputtering target in which a target material is bonded to the outer peripheral surface of a cylindrical base material is rotated around an axis has been put into practical use. And perform sputtering. This type of rotational sputtering can achieve much higher usage efficiency than a flat-plate type sputtering target, which has the advantage of achieving high productivity.
在平面面板顯示器(flat panel display)或太陽電池所使用的玻璃基板已日益大型化,為了在此大型化的基板上形成薄膜,需要長度2m以上之長條 狀的圓筒形濺鍍靶。然而,由於在製造長度2m以上的圓筒形靶上有其困難,因此,在長條狀圓筒形基材的外側,以朝軸線方向排列複數個之方式配置複數個圓筒形靶材(亦稱為「分割靶材」)。 The glass substrate used in flat panel displays or solar cells has become increasingly larger. In order to form a thin film on this larger substrate, a strip with a length of 2m or more is required. cylindrical sputtering target. However, since it is difficult to produce a cylindrical target with a length of 2 m or more, a plurality of cylindrical targets are arranged in an axial direction outside the long cylindrical base material ( Also known as "split target").
在例如專利文獻1、2中,已揭示了下列內容:製作將靶材朝軸線方向分割為複數個而成的複數個靶材,且將此複數個靶材以朝軸線方向排列之方式配置於圓筒形基材的外周側,並且將該等構件藉由接合材予以接合,藉此製造該濺鍍靶。
For example,
如前所述,當圓筒形基材伴隨著圓筒形濺鍍靶變為長條狀而變為長條狀時,將無法忽視圓筒形基材之翹曲的影響。尤其超過2m之長條狀的圓筒形基材,係具有呈翹曲者較多而且其翹曲幅度亦較大的問題。當圓筒形基材的翹曲較大時,接合材的厚度即變得不均勻,在接合材之厚度較薄的部分會產生冷卻不足,而於濺鍍時招致龜裂(crack)的產生等問題。 As mentioned above, when the cylindrical base material changes into a long shape as the cylindrical sputtering target changes into a long shape, the influence of the warpage of the cylindrical base material cannot be ignored. In particular, long cylindrical base materials exceeding 2 meters have the problem that warpage occurs more often and the warpage amplitude is also larger. When the warpage of the cylindrical base material is large, the thickness of the joining material becomes uneven, and insufficient cooling occurs in the thinner portion of the joining material, which causes cracks during sputtering. etc. questions.
近年來,已變為使用在更大型的第十代玻璃基板上成膜的濺鍍裝置,靶的全長已超過了3m。當靶的全長超過了3m時,前述之翹曲的問題就更為顯著。 In recent years, sputtering equipment has been used to form films on larger tenth-generation glass substrates, and the total target length has exceeded 3m. When the total length of the target exceeds 3m, the aforementioned warping problem becomes more significant.
因此,在專利文獻2中已提出一種方法,該方法係著眼於基材與靶材的偏心,為了抑制此偏心,乃在製造圓筒形靶前先確認圓筒形基材的翹曲,當翹曲較大時,使用衝壓機等矯正圓筒形基材的翹曲。
Therefore,
此外,專利文獻3係以圓筒形基材呈現彎曲為前提,將複數個圓筒形靶材的各者配合圓筒形基材的彎曲變形而進行配置。亦即,其係揭示一種方法,該方法係使各圓筒形靶材的中心軸線傾斜,或使其在周方向的任一位置上朝徑方向偏靠,以確保圓筒形靶材之內周面與圓筒形基材之外周面之間之所需之接合材厚度。
In addition,
[先前技術文獻] [Prior technical literature]
[專利文獻] [Patent Document]
專利文獻1:日本特開2010-100930號公報 Patent Document 1: Japanese Patent Application Publication No. 2010-100930
專利文獻2:國際公開2016/067717號 Patent Document 2: International Publication No. 2016/067717
專利文獻3:日本特開2018-159105號公報 Patent Document 3: Japanese Patent Application Publication No. 2018-159105
專利文獻2所記載的發明,已提出了一種預先測量圓筒形基材的翹曲,當翹曲較大時,使用衝壓機等矯正翹曲的方案。然而,會有如下的問題:在充填接合材時,若預先加熱圓筒形基材、或將經加熱熔融後的接合材充填於圓筒形基材與靶材之間,而使圓筒形基材受到加熱時,則經過矯正後的翹曲將會恢復原狀(亦稱「翹曲復原」)。
The invention described in
此外,專利文獻3所記載的發明,由於係以使用呈彎曲的圓筒形基材為前提,因此會有如下的問題:當圓筒形靶材的軸方向長度未達750mm時,雖可確保所需要的接合材厚度,但另一方面,當圓筒形靶材的軸方向長度達到該750mm以上時,就難以確保所需要的接合材厚度。
In addition, since the invention described in
當在圓筒形基材的外側以排列複數個的方式配設複數個圓筒形靶材而構成圓筒形濺鍍靶時,由於圓筒形靶材間的間隙會在濺鍍時成為結塊(nodule)的原因,因此圓筒形靶材的分割數係以盡量減少為佳。因此,如前所述,伴隨著圓筒形濺 鍍靶的長度逐年變長,圓筒形靶材的軸方向長度亦逐年變長,而有圓筒形靶材亦變長的傾向,而變成無法落在未達750mm的範圍。 When a plurality of cylindrical targets are arranged in an array on the outside of a cylindrical base material to form a cylindrical sputtering target, the gaps between the cylindrical targets will become a junction during sputtering. Because of the nodules, it is better to reduce the number of divisions of the cylindrical target as much as possible. Therefore, as mentioned earlier, with the cylindrical splash The length of the plating target is getting longer year by year, and the axial length of the cylindrical target is also getting longer every year. There is a tendency that the cylindrical target will also become longer, and it will become impossible to fall within the range of less than 750mm.
因此,本發明係關於一種可使用已翹曲的圓筒形基材作為構成材料的濺鍍靶及其製造方法,且欲提供一種新穎的濺鍍靶的製造方法及新穎的濺鍍靶,該新穎的濺鍍靶的製造方法係即使圓筒形靶材的軸方向長度相對較長,而且,即使經過充填接合材時的加熱(亦即,即使在充填接合材時,預先加熱圓筒形基材,或將經加熱熔融後的接合材充填於圓筒形基材與靶材之間,而使圓筒形基材受到加熱),亦可抑制所使用之圓筒形基材之翹曲的影響,結果,可製造接合材的厚度均勻,而且,相鄰之圓筒形靶材間的段差量較小,而且,相鄰之圓筒形靶材間的軸方向距離均勻之濺鍍靶。 Therefore, the present invention relates to a sputtering target that can use a warped cylindrical base material as a constituent material and a manufacturing method thereof, and is intended to provide a novel sputtering target manufacturing method and a novel sputtering target, which The novel sputtering target manufacturing method is to make the axial length of the cylindrical target material relatively long, and even after heating when filling the joining material (that is, even when filling the joining material, the cylindrical base is heated in advance material, or filling the heated and melted joining material between the cylindrical base material and the target material, and heating the cylindrical base material), which can also suppress the warpage of the cylindrical base material used. As a result, it is possible to manufacture a sputtering target in which the thickness of the joining material is uniform, the step difference between adjacent cylindrical targets is small, and the axial distance between adjacent cylindrical targets is uniform.
本發明係提供一種濺鍍靶的製造方法,該濺鍍靶係具備圓筒形基材和圓筒形靶材;該製造方法係具備下列步驟: The invention provides a method for manufacturing a sputtering target. The sputtering target is provided with a cylindrical base material and a cylindrical target material; the manufacturing method includes the following steps:
測量圓筒形基材的翹曲幅度; Measure the warpage amplitude of cylindrical substrate;
進行使圓筒形基材朝與原本翹曲之方向相反之方向翹曲的加工;及 Processing that causes the cylindrical base material to warp in a direction opposite to the original warping direction; and
以在軸方向隔著間隔排列之方式將複數個圓筒形靶材配置於經前述加工過之圓筒形基材的外側,且以接合材將該圓筒形基材與前述圓筒形靶材予以接合。 Arrange a plurality of cylindrical targets at intervals in the axial direction on the outside of the processed cylindrical base material, and use a bonding material to connect the cylindrical base material and the cylindrical target materials are joined.
此外,本發明還提供一種濺鍍靶,該濺鍍靶係具備圓筒形基材和圓筒形靶材,且以接合材將前述圓筒形基材和前述圓筒形靶材予以接合而成者;其中, In addition, the present invention also provides a sputtering target including a cylindrical base material and a cylindrical target material, and the cylindrical base material and the cylindrical target material are joined with a joining material. Become a person; among them,
前述圓筒形靶材中之至少一者係之軸方向的長度為750mm以上,接合材之厚度之最大值與最小值的差為1.0mm以下,相鄰之圓筒形靶材之外周面間之段差 量的最大值為0.5mm以下,相鄰之圓筒形靶材間之軸方向距離之最大值與最小值的差為0.2mm以下。 The length of at least one of the aforementioned cylindrical targets in the axial direction is 750 mm or more, the difference between the maximum and minimum thickness of the joining material is 1.0 mm or less, and the distance between the outer peripheral surfaces of adjacent cylindrical targets is The difference The maximum value of the amount is less than 0.5mm, and the difference between the maximum value and the minimum value of the axial distance between adjacent cylindrical targets is less than 0.2mm.
本發明所提供的製造方法,係考慮因為將圓筒形基材加工之後之加熱而再度變形(亦即前述之翹曲復原),而將圓筒形基材進行加工,使之朝與原本翹曲的方向相反之方向反向翹曲達預定之幅度的方法。因此,即使圓筒形靶材的軸方向長度相對較長,而且,即使經過充填接合材時的加熱,亦可消除所使用之圓筒形基材之翹曲的影響,可製造接合材的厚度均勻,而且,相鄰之圓筒形靶材間的段差量較小,而且,相鄰之圓筒形靶材間的軸方向距離均勻的濺鍍靶。 The manufacturing method provided by the present invention considers that the cylindrical base material is deformed again due to heating after processing (that is, the aforementioned warpage recovery), and the cylindrical base material is processed so that it warps in the same direction as the original one. The direction of curvature is opposite to the direction of reverse warping to a predetermined amplitude. Therefore, even if the axial length of the cylindrical target is relatively long, and even if it is heated when filling the joining material, the influence of the warpage of the cylindrical base material used can be eliminated, and the thickness of the joining material can be manufactured It is a sputtering target that is uniform, has a small step difference between adjacent cylindrical targets, and has a uniform axial distance between adjacent cylindrical targets.
因此,依據本發明所提供的製造方法,可製造一種濺鍍靶,該濺鍍靶係具備圓筒形基材和複數個圓筒形靶材;其中,前述圓筒形靶材中的至少一者係軸方向的長度為750mm以上,接合材之厚度之最大值與最小值的差為1.0mm以下,相鄰之圓筒形靶材之外周面間之段差量的最大值為0.5mm以下,相鄰之圓筒形靶材間之軸方向距離之最大值與最小值的差為0.2mm以下。 Therefore, according to the manufacturing method provided by the present invention, a sputtering target can be manufactured. The sputtering target is provided with a cylindrical base material and a plurality of cylindrical target materials; wherein, at least one of the aforementioned cylindrical target materials The length in the axial direction is more than 750mm, the difference between the maximum and minimum thickness of the joining material is less than 1.0mm, and the maximum step difference between the outer peripheral surfaces of adjacent cylindrical targets is less than 0.5mm. The difference between the maximum value and the minimum value of the axial distance between adjacent cylindrical targets is 0.2mm or less.
再者,若為此種濺鍍靶,則接合層的厚度已確保為均勻,因此不僅不易於濺鍍時產生破裂,而且相鄰之圓筒形靶材間之外周面間的段差量亦較小,而且,該間隙的間隔亦均勻,故可使濺鍍時之異常產生的機率顯著地減少。再者,由於翹曲(亦即彎曲)較少,因此在使靶旋轉時晃動較小,可將圓筒形靶材與基板的距離保持為固定,且可使藉由濺鍍所形成之膜的質均勻。 Furthermore, with this kind of sputtering target, the thickness of the joint layer is ensured to be uniform, so not only is it less likely to crack during sputtering, but the step difference between the outer peripheral surfaces of adjacent cylindrical targets is also relatively small. The gap is small, and the intervals between the gaps are uniform, so the probability of abnormality during sputtering can be significantly reduced. Furthermore, since there is less warpage (i.e., bending), there is less shaking when the target is rotated, and the distance between the cylindrical target and the substrate can be kept constant, and the film formed by sputtering can be The quality is uniform.
1:濺鍍靶 1: sputtering target
2:基材(圓筒形基材) 2: Base material (cylindrical base material)
2a,3a:外周面 2a, 3a: Outer peripheral surface
3:靶材(圓筒形靶材) 3:Target (cylindrical target)
4:接合材 4:Joining materials
5:度盤規 5: Dial gauge
40:製造裝置 40: Manufacturing device
43:下部保持構件 43:Lower retaining member
43b,44b:靶材保持部 43b, 44b: Target holding part
43c:基材保持部 43c: Base material holding part
43d,44c,45c:固定具 43d, 44c, 45c: Fixture
44:靶材保持構件 44:Target holding member
45:基材保持構件 45:Substrate holding member
45b:基材推壓部 45b: Base material pressing part
46:連結構件 46:Connecting components
47,48,50,51:O環 47,48,50,51:O ring
49:空隙部 49: Gap part
d:軸方向距離 d: axial distance
h:段差量 h: step difference
Hmax:最大值 Hmax: maximum value
Hmin:最小值 Hmin: minimum value
L3:軸方向長度 L 3 : axial length
P:加壓方向 P: Pressure direction
X:翹曲幅度 X: warp amplitude
Y:翹曲幅度 Y: warpage amplitude
α:幅度 α: amplitude
圖1係概念性地顯示濺鍍靶之一例的立體圖。 FIG. 1 is a perspective view conceptually showing an example of a sputtering target.
圖2係概念性地顯示呈翹曲之圓筒形基材之一例的立體圖。 FIG. 2 is a perspective view conceptually showing an example of a warped cylindrical base material.
圖3係概念性地顯示測量圓筒形基材之翹曲幅度之方法之一例的圖。 FIG. 3 is a diagram conceptually showing an example of a method of measuring the warpage amplitude of a cylindrical base material.
圖4係概念性地顯示圓筒形基材之加工方法之一例的側視圖,圖4(A)係顯示加工前之狀態的圖,圖4(B)係顯示加工後之狀態的圖。 FIG. 4 is a side view conceptually showing an example of a processing method of a cylindrical base material. FIG. 4(A) is a diagram showing a state before processing, and FIG. 4(B) is a diagram showing a state after processing.
圖5係將所製造之濺鍍靶之一例之要部予以放大顯示的縱剖面圖。 FIG. 5 is an enlarged longitudinal cross-sectional view showing a main part of an example of the sputtering target produced.
圖6係用以說明相鄰之靶材間之段差量h和軸方向距離d的要部放大剖面圖。 FIG. 6 is an enlarged cross-sectional view of a main part for explaining the step difference h and the axial distance d between adjacent targets.
圖7係顯示實施例中所使用之濺鍍靶之製造裝置的縱剖面圖。 FIG. 7 is a longitudinal sectional view showing the manufacturing apparatus of the sputtering target used in the Example.
接著根據實施型態例來說明本發明。惟,本發明不限定於以下所要說明的實施型態。 Next, the present invention will be described based on embodiment examples. However, the present invention is not limited to the embodiments described below.
<本靶製造方法> <Manufacturing method of this target>
本發明之實施型態之一例之濺鍍靶的製造方法(稱為「本靶製造方法」)係一種濺鍍靶的製造方法,該濺鍍靶係具備圓筒形基材2和複數個圓筒形靶材3、3、…;該製造方法係具備下列步驟:
A method for manufacturing a sputtering target (referred to as "this target manufacturing method") as an example of an embodiment of the present invention is a method for manufacturing a sputtering target. The sputtering target is provided with a
測量圓筒形基材2的翹曲幅度及翹曲方向(稱為「測量步驟」); Measure the warpage amplitude and warpage direction of the cylindrical base material 2 (referred to as the "measurement step");
進行使圓筒形基材2朝與原本翹曲之方向相反之方向翹曲的加工(稱為「加工步驟」);及
Perform processing to warp the
以在圓筒形基材2的軸方向隔著間隔排列之方式將複數個圓筒形靶材3、3、…配置於經前述加工過之圓筒形基材2的外側,且以接合材4將該圓筒形基材2與前述圓筒形靶材3予以接合。
A plurality of
(本濺鍍靶) (This sputtering target)
如圖1所示,以本靶製造方法所製造的濺鍍靶(「本濺鍍靶」)1,係以在圓筒形基材2的軸方向隔著間隔排列之方式將複數個圓筒形靶材3配置於一條圓筒形基材2的外側,且以接合材4(未圖示)將圓筒形基材2與前述圓筒形靶材3予以接合而成者。
As shown in FIG. 1 , a sputtering target ("this sputtering target") 1 manufactured by this target manufacturing method is composed of a plurality of cylinders arranged at intervals in the axial direction of a
關於本濺鍍靶1的詳細內容將於後說明。在此先就構成構件進行說明。
Details of this
(靶材) (Target)
靶材係由複數個圓筒形靶材3、3、…所構成者,該複數個圓筒形靶材3係在圓筒形基材2的軸線方向隔著適當間隔而配置於圓筒形基材2的外周側。
The target is composed of a plurality of
各圓筒形靶材3具有較圓筒形基材2之外徑更大的內徑即可。
Each
圓筒形靶材的長度有逐年變長的傾向,但另一方面已被指出,當圓筒形靶材的長度變長時,尤其變為750mm以上時,會有無法確保接合材厚度的問題。然而,依據本靶製造方法,可消除此種問題,且可更進一步地享有本發明的功效。 The length of cylindrical targets tends to become longer year by year, but on the other hand, it has been pointed out that when the length of cylindrical targets becomes longer, especially when it becomes 750 mm or more, there is a problem that the thickness of the joining material cannot be ensured. . However, according to the present target manufacturing method, this problem can be eliminated, and the effects of the present invention can be further enjoyed.
因此,從能夠更享有本發明之功效的觀點而言,前述複數個圓筒形靶材3、3、…中之至少一者,其軸方向長度L3係以750mm以上為佳,其中又以850mm以上(其中又以950mm以上、再其中又以1400mm以上)為更佳。
Therefore, from the perspective of being able to better enjoy the effects of the present invention, it is preferable that the axial length L 3 of at least one of the plurality of
圓筒形靶材3並無限定其材料。可列舉例如包含Cu(銅)、Al(鋁)、In(銦)、Sn(錫)、Ti(鈦)、Ba(鋇)、Ca(鈣)、Zn(鋅)、Mg(鎂)、Ge(鍺)、Y(釔)、La(鑭)、Al(鋁)、Si(矽)、Ga(鎵)、W(鎢)的任一種以上的氧化物。
The material of the
以前述氧化物而言,可列舉例如In-Sn-O(銦錫氧化物)、In-Ti-O(銦鈦氧化物)、In-Ga-Zn-O(銦鎵鋅氧化物)、In-Zn-Sn-O(銦鋅錫氧化物)、In-Ga-Zn-Sn-O(銦錄鋅 錫氧化物)、Ga-Zn-O(鎵鋅氧化物)、In-Zn-O(銦鋅氧化物)、In-Ga-O(銦鎵氧化物)、I-W-O(銦鎢氧化物)、I-Zn-W-O(銦鋅鎢氧化物)、Zn-O(鋅氧化物)、Sn-Ba-O(錫鋇氧化物)、Sn-Zn-O(錫鋅氧化物)、Sn-Ti-O(錫鈦氧化物)、Sn-Ca-O(錫鈣氧化物)、Sn-Mg-O(錫鎂氧化物)、Zn-Mg-O(鋅鎂氧化物)、Zn-Ge-O(鋅鍺氧化物)、Zn-Ca-O(鋅鈣氧化物)、Zn-Sn-Ge-O(鋅錫鍺氧化物)、Cu2O(氧化亞銅)、CuAlO2(二氧化銅鋁)、CuGaO2(二氧化銅鎵)、CuInO2(二氧化銅銦)等。 Examples of the aforementioned oxides include In-Sn-O (indium tin oxide), In-Ti-O (indium titanium oxide), In-Ga-Zn-O (indium gallium zinc oxide), In -Zn-Sn-O (indium zinc tin oxide), In-Ga-Zn-Sn-O (indium zinc tin oxide), Ga-Zn-O (gallium zinc oxide), In-Zn-O ( Indium zinc oxide), In-Ga-O (indium gallium oxide), IWO (indium tungsten oxide), I-Zn-WO (indium zinc tungsten oxide), Zn-O (zinc oxide), Sn- Ba-O (tin-barium oxide), Sn-Zn-O (tin-zinc oxide), Sn-Ti-O (tin-titanium oxide), Sn-Ca-O (tin-calcium oxide), Sn-Mg- O (tin magnesium oxide), Zn-Mg-O (zinc magnesium oxide), Zn-Ge-O (zinc germanium oxide), Zn-Ca-O (zinc calcium oxide), Zn-Sn-Ge- O (zinc tin germanium oxide), Cu 2 O (cuprous oxide), CuAlO 2 (copper aluminum dioxide), CuGaO 2 (copper gallium dioxide), CuInO 2 (copper indium dioxide), etc.
(圓筒形基材) (cylindrical base material)
圓筒形基材2係以中心軸為直線且外周面亦呈與該軸平行的圓筒形者為理想。然而,如圖2所示,新使用的圓筒形基材或回收(recycle)使用的圓筒形基材2係翹曲為彎曲狀(換言之,拱(arch)狀),圓筒形基材2的外周面自直線軸方向起具有偏差。
The
圓筒形基材2的材質係Ti(鈦)、SUS(Steel Special Use Stainless,不鏽鋼材質標準)或Cu等金屬即可。惟,不限定於此等。
The material of the
(接合材) (joining material)
接合材4係於製造濺鍍靶時,以熔融狀態供給至圓筒形基材2與配置於該圓筒形基材2之外周側之預定部位之各圓筒形靶材3之間的間隙,且於充填於該間隙之後硬化,以將圓筒形基材2與圓筒形靶材3予以接合者。
The
接合材4的材質若為能夠使用於該種靶材與基材的接合者,則無特別限定。可列舉例如銦金屬、銦錫金屬、或在銦中添加有微量金屬成分之銦合金金屬等低熔點銲料。
The material of the
前述低熔點銲料的熔點係為150至250℃,故於充填接合材4時,通常將接合材4加熱至150至300℃使之熔融。
The melting point of the aforementioned low melting point solder is 150 to 250°C. Therefore, when filling the joining
<測量步驟> <Measurement procedure>
在測量步驟中,係測量被作為構成材料使用之圓筒形基材2之翹曲幅度及翹曲方向。
In the measurement step, the warp width and warp direction of the
翹曲幅度的測量方法並無特別限定。例如,可使圓筒形基材2進行軸旋轉以測量外周面的位移幅度(亦即翹曲幅度),或者,亦可將圓筒形基材2橫向地載置於平台上,且沿著豎立於平台上而成的垂線來測量平台的平滑面與圓筒形基材2之外周面2a之距離的位移幅度,亦即翹曲幅度。亦可藉由其他方法來測量。
The method of measuring the warpage amplitude is not particularly limited. For example, the
測量翹曲幅度的部位,在圓筒形基材2的長度方向可為一個部位,亦可為二個部位以上。
The location where the warpage amplitude is measured may be one location, or two or more locations in the length direction of the
圓筒形基材2大多翹曲成拱狀,故若在長度方向中心部附近測量翹曲幅度,則可測量最大翹曲幅度及其翹曲方向。
The
惟,未必會翹曲成拱狀,故較佳為在長度方向隔著間隔在複數個部位測量翹曲幅度。例如,以100mm至1000mm的間隔來測量為佳,其中又以200mm以上或800mm以下的間隔(其中又特別以500mm以下的間隔)來測量為更佳。 However, it may not warp into an arch shape, so it is better to measure the warp amplitude at multiple locations at intervals in the length direction. For example, it is preferably measured at an interval of 100 mm to 1000 mm, and more preferably at an interval of 200 mm or more or 800 mm or less (especially an interval of 500 mm or less).
茲說明測量翹曲幅度之具體之測量方法的一例。 This is an example of a specific measurement method for measuring warpage amplitude.
如圖3所示,將圓筒形基材2以水平而且可進行軸旋轉之方式設置,且將度盤規(dial gauge)5抵靠在前述圓筒形基材2的外周面2a,使前述圓筒形基材2轉一圈以測量前述度盤規5的讀數。再者,可將前述度盤規5之讀數的最大值Hmax與最小值Hmin的差(Hmax-Hmin)設為翹曲幅度。
As shown in FIG. 3 , the
此時,使圓筒形基材2進行軸旋轉的手段為任意手段。例如設為載置在二個旋轉輥間上使之旋轉,或設為使圓筒形基材的兩端附近置入於具有V字形溝之支撐台的該溝而載置,且以手或輥使之旋轉,其手段係任意手段。
At this time, any means can be used to rotate the axis of the
在測量步驟中,亦可如上所述地測量所取得之圓筒形基材2之原有的翹曲幅度X及翹曲方向,或者,亦可將所取得的圓筒形基材2進行加熱,且如上所述地測量加熱後之圓筒形基材2之翹曲幅度Y及翹曲方向。
In the measuring step, the original warp amplitude , and measure the warp amplitude Y and warp direction of the heated
當將圓筒形基材2進行加熱,且測量加熱後之圓筒形基材之翹曲幅度Y及翹曲方向時,圓筒形基材2的加熱溫度較佳係設想為:在充填接合材時(亦即,將經加熱熔融後的接合材4充填於圓筒形基材2與圓筒形靶材3之間時)將圓筒形基材2加熱的溫度,或者,由於所充填的接合材4而使圓筒形基材2受到加熱的溫度。惟,若過於高溫,則圓筒形基材2會有表面氧化的可能性。由此觀點而言,關於此時之圓筒形基材2的加熱溫度,較佳為進行加熱而使其表面溫度成為150至300℃,其中又以進行加熱而使其表面溫度成為160℃以上至240℃以下(其中又以170℃以上或230℃以下)為更佳。
When heating the
圓筒形基材2的加熱方法並無特別限定。例如可將基材置入於電爐等,從外部進行加熱,亦可在基材的內部設置加熱器(heater),從內部進行加熱。
The heating method of the
<加工步驟> <Processing steps>
在加工步驟中,係將圓筒形基材2進行加工,使之朝與原本翹曲的方向相反之方向反向翹曲達預定之幅度α。
In the processing step, the
例如,如圖4所示,在測量步驟中的測量位置,朝與在前述測量步驟中所測量之翹曲方向相反之方向加壓而使圓筒形基材2彎曲,且如圖4(B)所示,
將圓筒形基材2進行加工,使之朝與原本翹曲的方向相反之方向反向翹曲達幅度α(換言之,從直線軸位移達α)即可
For example, as shown in FIG. 4 , at the measurement position in the measurement step, the
關於進行加壓的位置,例如可在圓筒形基材2翹曲成拱狀時等,將軸方向中央部加壓一個部位而使之變形。此外,較佳為將在測量步驟中所測量的位置進行加壓。例如較佳為以100mm至1000mm的間隔進行測量,且在各測量點進行加壓而使之變形。
As for the position where the pressure is applied, for example, when the
要使圓筒形基材2朝與原本翹曲之方向相反之方向翹曲的幅度α(mm),較佳為根據在前述測量步驟中所測量之翹曲幅度X或Y來決定。這是因為翹曲幅度X或Y愈大,則翹曲復原的大小就會因為加工後的加熱而愈大之故。
The amplitude α (mm) required to cause the
例如,在測量步驟中,當測量所取得之圓筒形基材2之原有的翹曲幅度而獲得了翹曲幅度X時,要使之翹曲的幅度α(mm)較佳為設為X(mm)×(0.10至2.00),其中又以設為X(mm)×0.50以上或X(mm)×1.50以下(其中又以設為X(mm)×0.80以上或X(mm)×1.40以下、再其中又以設為X(mm)×0.90以上或X(mm)×1.30以下)為更佳。
For example, in the measurement step, when the original warp amplitude of the obtained
此外,在測量步驟中,當將所取得的圓筒形基材2進行加熱,且測量加熱後之圓筒形基材2的翹曲幅度而獲得了翹曲幅度時,要使之翹曲的幅度α(mm)較佳為設為Y(mm)×(0.50至1.50),其中又以設為Y(mm)×0.80以上或Y(mm)×1.40以下(其中又以設為Y(mm)×0.90以上或Y(mm)×1.30以下、再其中又以設為Y(mm)×0.95以上或Y(mm)×1.25以下)為更佳。
In addition, in the measuring step, when the obtained
若實際進行加熱而測量加熱後的翹曲幅度Y,且根據該翹曲幅度Y而決定要使之翹曲的幅度α,則可在加上了所取得之圓筒形基材2的加熱動作之後決定幅度α,故可更進一步減少翹曲復原。
If heating is actually carried out and the warp amplitude Y after heating is measured, and the amplitude α to be warped is determined based on the warp amplitude Y, the heating operation of the obtained
以將圓筒形基材2進行加壓使之翹曲的加工方法而言,例如圖4(A)所示,可列舉例如在測量步驟中的測量位置(一個部位或複數個部位),將圓筒形基材2朝與原本翹曲之方向相反之方向加壓的方法。另外,圖4(A)中的P係顯示加壓方向。此時,以進行加壓的手段而言,可列舉例如機械性的衝壓加工、鍛造加工等。
In the processing method of pressurizing the
惟,若為可使圓筒形基材2翹曲達所期望之幅度的手段,則可採用任意的手段。
However, any method may be used as long as the
此時,為使圓筒形基材的真圓度不會變化,亦可設為將配合圓筒形基材2之形狀而成之圓弧狀者使用於要施加加壓的端子等。
At this time, in order to prevent the roundness of the cylindrical base material from changing, an arc-shaped one formed according to the shape of the
此外,亦可視需要進一步實施熱處理(退火)。 In addition, further heat treatment (annealing) may be performed if necessary.
另外,亦可重複進行將圓筒形基材2進行加壓使之翹曲的加工方法。亦即,亦可設為重複進行將圓筒形基材2進行加壓使之翹曲且更進一步加壓使之翹曲等加壓使之翹曲的處理,最終使圓筒形基材2翹曲達預定幅度α。
In addition, the processing method of pressurizing and warping the
此外,亦可設為重複進行將圓筒形基材2進行加熱(測量翹曲幅度Y)且加壓使之翹曲且更進一步進行加熱並加壓使之翹曲等加熱並加壓使之翹曲的處理,最終使圓筒形基材2翹曲達預定幅度α。此時,在加熱之後測量翹曲幅度Y乙事,只要僅在最初進行即可。
In addition, the
<圓筒形靶材的配置> <Arrangement of cylindrical targets>
使用如上所述實施過加工的圓筒形基材2,以在軸線方向隔著適當間隔排列之方式將複數個圓筒形靶材3、3、…配置於該圓筒形基材2的外周側。
Using the
圓筒形靶材3較佳為在軸線方向隔著0.15mm至0.50mm的間隔排列配置。
The
<接合> <Join>
綜上所述,只要如下設置即可:在配置圓筒形靶材3之後,就將圓筒形基材2及圓筒形靶材3進行加溫,且在圓筒形基材2與圓筒形靶材3的間隙充填熔融狀態的接合材4,並將接合材4冷卻而藉由接合材4將各圓筒形靶材3接合於圓筒形基材2的周圍。
To sum up, it only needs to be set as follows: after arranging the
在充填接合材4之前,將圓筒形基材2及圓筒形靶材3進行加溫的溫度,較佳為設為接合材4的溫度以上。
Before filling the
充填接合材4時之接合材4的溫度為接合材之熔點以上的溫度,較佳為加熱至成為150至300℃,其中又以加熱至成為160℃以上或240℃以下(其中又以加熱至成為170℃以上或230℃以下)為更佳。
The temperature of the joining
接合材之充填及冷卻的方法,係可使用公知的方法。 As the filling and cooling method of the joining material, known methods can be used.
<本濺鍍靶> <This sputtering target>
依據本靶製造方法,即使經過充填接合材時的加熱亦可消除圓筒形基材2之翹曲的影響,故可製造如下的本濺鍍靶。
According to this target manufacturing method, the influence of the warpage of the
作為本濺鍍靶之較佳的一例,可列舉一種濺鍍靶,該濺鍍靶係具備圓筒形基材2和複數個圓筒形靶材3、3、…,其中,前述複數個圓筒形靶材3、3、…中之至少一者係軸方向長度L3為750mm以上,接合材4之厚度之最大值與最小值的差為1.0mm以下,相鄰之圓筒形靶材3、3之外周面3a、3a中之段差量h的最大值為0.5mm以下,相鄰之圓筒形靶材3、3間之軸方向距離d之最大值與最小值的差為0.2mm以下。
As a preferred example of this sputtering target, a sputtering target can be cited. The sputtering target is provided with a
另外,從更享有本發明之功效的觀點而言,圓筒形基材2的長度,較佳為2.0m至4m,其中又以3.0m以上或3.8m以下(其中又以3.3m以上或3.7m以下)為更佳。
In addition, from the viewpoint of enjoying the effect of the present invention more, the length of the
圓筒形基材2的外徑,較佳為125mm至140mm,其中又以130mm以上或135mm以下(其中又以132mm以上或134mm以下)為更佳。
The outer diameter of the
圓筒形靶材3的內徑,較佳為127mm至142mm,其中又以132mm以上或137mm以下(其中又以134mm以上或136mm以下)為更佳。
The inner diameter of the
圓筒形靶材3的壁厚,較佳為5mm至20mm,其中又以6mm以上或16mm以下(其中又以8mm以上或13mm以下)為更佳。
The wall thickness of the
從更享有本發明之功效的觀點而言,圓筒形靶材3中之至少一條的軸方向長度L3,較佳為750mm至1500mm,其中又以850mm以上或1450mm以下(其中又以950mm以上或1450mm以下)為更佳。
From the perspective of better enjoying the effects of the present invention, the axial length L 3 of at least one of the
若接合材4之厚度的最大值與最小值的差為1.0mm以下,則接合材4的厚度已確保為均勻,因此可防止例如在接合材之厚度較薄的部分因為冷卻不足而使靶破裂等,可抑制濺鍍時之破裂的產生。
If the difference between the maximum value and the minimum value of the thickness of the joining
從此觀點而言,接合材4之厚度的最大值與最小值的差較佳為0.5mm以下,且以0.3mm以下為更佳。
From this point of view, the difference between the maximum value and the minimum value of the thickness of the joining
此時,接合材4的厚度較佳為0.5mm以上,其中又以0.7mm以上(其中又以1mm以上)為佳。
At this time, the thickness of the joining
接合材4的厚度,係可藉由超音波探傷裝置來測量。
The thickness of the
若相鄰之圓筒形靶材3、3之外周面3a、3a間之段差量h的最大值(亦即,在軸線方向相鄰之一對圓筒形靶材3、3中,各者之外周面3a、3a中之彼此相
鄰之軸線方向之外端緣之段差量h的最大值)為0.5mm以下,則可減少濺鍍時的異常產生,具體而言,係可減少電弧(arcing)的產生、或隨之所導致之崩裂(chipping)或破裂之產生等的發生機率。反之若段差量h的最大值較0.5mm更大,則有可能變成單側的圓筒形靶材3鼓出的形狀,而在鼓出的邊緣部產生異常放電等不良影響。
If the maximum value of the step difference h between the outer
從此觀點而言,該段差量h的最大值較佳為0.3mm以下,且以0.2mm以下為更佳。 From this point of view, the maximum value of the step difference h is preferably 0.3 mm or less, and more preferably 0.2 mm or less.
另外,該段差量h係可使用例如深度規(depth gauge)等來測量。 In addition, the step difference h can be measured using, for example, a depth gauge.
再者,若相鄰之圓筒形靶材3、3間之軸方向距離(間隔)d之最大值與最小值的差為0.2mm以下,則可更減少濺鍍時之異常產生,例如端部彼此因為濺鍍時之熱膨脹而接觸而產生崩裂或破裂等的機率。例如,在軸方向距離d較大的部分中,會有圓筒形基材2露出,且基材成分被濺鍍而以雜質形態混入於膜的可能性。另一方面,在軸方向距離d較小的部分中,會有相鄰之圓筒形靶材3、3彼此在因為濺鍍的熱而熱膨脹時碰撞,而使圓筒形靶材3破裂的可能性。
Furthermore, if the difference between the maximum value and the minimum value of the axial distance (interval) d between adjacent
從此觀點而言,相鄰之圓筒形靶材3、3間之軸方向距離d之最大值與最小值的差較佳為0.15mm以下,且以0.1mm以下為更佳。
From this point of view, the difference between the maximum value and the minimum value of the axial distance d between adjacent
另外,前述軸方向距離(間隔)d,係可使用例如測隙規(feeler gauge)等來測量。 In addition, the aforementioned axial direction distance (interval) d can be measured using, for example, a feeler gauge.
<語句的說明> <Description of statement>
在本說明書中,當表現為「A至B」(該A、B係任意的數字)時,若未特別聲明,係指「A以上B以下」之意,而且亦包含「較佳為比A大」或「較佳為比B小」之意。 In this specification, when expressed as "A to B" (where A and B are arbitrary numbers), unless otherwise stated, it means "above A and below B", and also includes "better than A". It means "big" or "preferably smaller than B".
此外,當表現為「A以上」(A係任意的數字)或「B以下」(B係任意的數字)時,亦包含「較佳為比A大」或「較佳為未達B」之內容的涵義。 In addition, when expressed as "above A" (A is an arbitrary number) or "below B" (B is an arbitrary number), it also includes "preferably greater than A" or "preferably less than B" The meaning of the content.
[實施例] [Example]
茲藉由以下的實施例來進一步說明本發明。惟,以下的實施例並未意圖限定本發明。 The present invention is further illustrated by the following examples. However, the following examples are not intended to limit the present invention.
<實施例1> <Example 1>
茲將屬於回收品的圓筒形基材(長度3400mm、直徑133mm、壁厚4mm)載置於能夠以可進行軸旋轉之方式支撐的基座上,且以水平而且可進行軸旋轉之方式設置,並將從上方垂下固定的度盤規抵靠在該圓筒形基材之長度方向中央部的外表面,使該圓筒形基材轉一圈以測量前述度盤規的讀數,且測量讀數之最大值Hmax與最小值Hmin的差(Hmax-Hmin)作為翹曲幅度X(初期)。 The cylindrical base material (length 3400mm, diameter 133mm, wall thickness 4mm) that is recycled is placed on a base that can be supported for axis rotation, and is installed horizontally and axis-rotatably. and place the fixed dial gauge hanging down from above against the outer surface of the central portion of the cylindrical base material in the length direction, and make the cylindrical base material rotate once to measure the reading of the aforementioned dial gauge, and measure The difference between the maximum value Hmax and the minimum value Hmin of the reading (Hmax-Hmin) is regarded as the warpage amplitude X (initial stage).
接著,將上述圓筒形基材置入於電爐內,進行加熱而使其表面溫度保持230℃達一小時,且以與上述同樣之方式測量加熱後之翹曲幅度Y(加熱後)。 Next, the above-mentioned cylindrical base material was placed in an electric furnace, heated so that the surface temperature was maintained at 230° C. for one hour, and the warp amplitude Y after heating (after heating) was measured in the same manner as above.
接著,使用衝壓機進行加工,將上述圓筒形基材之長度方向中央部朝與原本翹曲之方向(+方向)相反之方向(-方向)進行加壓,而使之朝該相反之方向(-方向)翹曲達幅度α(=Y×1.0)。 Next, a press machine is used to process the longitudinal center portion of the cylindrical base material in a direction (- direction) opposite to the original direction of warping (+ direction), so that the center portion is pressed in the opposite direction. (- direction) warpage reaches amplitude α (=Y×1.0).
接著,使用如上所述加工過的圓筒形基材,且使用圖7所示的製造裝置40,而如下所述地製造出ITO圓筒形濺鍍靶。
Next, using the cylindrical base material processed as mentioned above, and using the
亦即,準備外徑153mm、內徑133mm、長度300mm、750mm、750mm、300mm的ITO圓筒形分割靶材四個,且將圓筒形分割靶材的外周面藉由 耐熱性薄膜與膠帶予以遮罩(masking),且使用超音波烙鐵將銦銲料打底於接合面(內周面)上。 That is, four ITO cylindrical divided targets with an outer diameter of 153mm, an inner diameter of 133mm, and a length of 300mm, 750mm, 750mm, and 300mm are prepared, and the outer peripheral surface of the cylindrical divided target is Heat-resistant film and tape are masked, and an ultrasonic soldering iron is used to lay indium solder on the joint surface (inner peripheral surface).
另一方面,在如上所述加工過之圓筒形基材的接合面(外周面)亦使用超音波烙鐵打底銦銲料。 On the other hand, an ultrasonic soldering iron is also used to prime the indium solder on the joint surface (outer peripheral surface) of the cylindrical base material processed as described above.
將前述圓筒形基材安裝於裝設有鐵氟龍(Teflon)(註冊商標)製O環(ring)48的基材保持部43c。
The cylindrical base material was attached to the base material holding part 43c equipped with an O-
接著,將鐵氟龍(註冊商標)製O環47裝設於靶材保持部43b,且將前述圓筒形分割靶材安裝一個於靶材保持部43b。此時,前述圓筒形基材下端部與前述圓筒形分割靶材下端部的偏移,係藉由下部保持構件43調整成為0.1mm。此外,在前述圓筒形基材與前述圓筒形分割靶材之間形成有空隙部49。
Next, an O-
再者,在前述圓筒形分割靶材之上堆疊有剩餘的圓筒形分割靶材。在圓筒形分割靶材間,係介置有厚度0.5mm之鐵氟龍(註冊商標)製O環51。在放置於最上方之圓筒形分割靶材的上方裝設O環50,且將最上方的圓筒形分割靶材安裝於靶材保持部44b,藉由靶材保持部44b將圓筒形靶材從其上側壓住。此時,調整九個圓筒形分割靶材的位置,使圓筒形分割靶材間之所有的段差成為0.2mm以下。如此,藉由靶材保持構件44保持住圓筒形靶材的上端部。
Furthermore, the remaining cylindrical divided targets are stacked on the aforementioned cylindrical divided targets. An O-
接著,將基材推壓部45b壓抵於前述圓筒形基材的上端部,且藉由基材推壓部45b保持住圓筒形基材的上端部。此時,一面藉由深度規測量圓筒形靶材之表面與圓筒形基材表面之距離一面調整輔助具的位置,以使圓筒形基材上端部與圓筒形靶材上端部的偏移成為0.1mm以下。 Next, the base material pressing part 45b is pressed against the upper end part of the cylindrical base material, and the upper end part of the cylindrical base material is held by the base material pressing part 45b. At this time, while measuring the distance between the surface of the cylindrical target and the surface of the cylindrical base material with a depth gauge, adjust the position of the auxiliary tool so that the upper end of the cylindrical base material and the upper end of the cylindrical target are aligned The offset becomes 0.1mm or less.
最後,將下部保持構件43、靶材保持構件44、基材保持構件45分別藉由固定具43d、固定具44c、固定具45c固定於鈦製的連結構件46,藉此將圓筒形基材和圓筒形靶材確實地固定於製造裝置40。
Finally, the lower holding
將製造裝置40、圓筒形基材和圓筒形靶材加溫至180℃。
The
從靶材保持構件44的上側,將足供接合圓筒形靶材與圓筒形基材之量之已熔解之175℃的銦銲料注入至空隙部49。
From the upper side of the
將注入於製造裝置40、圓筒形基材、圓筒形靶材和空隙部49之已熔解的銲料進行冷卻。
The melted solder injected into the
在確認銦銲料已固化之後,將所製造之ITO圓筒形濺鍍靶(樣本)從製造裝置40拆下,且取下O環,掏出殘存於圓筒形分割靶材間的銦銲料。
After confirming that the indium solder has solidified, the manufactured ITO cylindrical sputtering target (sample) is removed from the
在以此方式所製造之ITO圓筒形濺鍍靶(樣本)中,如下所述地使用超音波探傷檢查機(株式會社日立電力解決方案(hitachi-power-solutions)製:FS LINE)測量了接合材的厚度。具體而言,係根據在靶材與接合層之界面的反射波和在接合層與基材之界面的反射波之檢測時間的差、以及接合層中之超音波的傳遞速度而算出接合層的厚度。另外,探針(probe)係使用10MHz者,接合層(銦金屬)中之超音波的傳遞速度係設為2700m/s。 The ITO cylindrical sputtering target (sample) manufactured in this manner was measured using an ultrasonic flaw detector (manufactured by Hitachi Power Solutions Co., Ltd.: FS LINE) as follows. The thickness of the joint material. Specifically, the bonding layer is calculated based on the difference in detection time between the reflected wave at the interface between the target material and the bonding layer and the reflected wave at the interface between the bonding layer and the base material, and the propagation speed of the ultrasonic wave in the bonding layer. thickness. In addition, a probe of 10 MHz was used, and the transmission speed of ultrasonic waves in the bonding layer (indium metal) was set to 2700 m/s.
接合材之厚度的測量位置,係設為於一個靶節段(target segment)中,在軸線方向設定從靶節段之兩端之各者往內側偏離10mm的二點、及將該等二點間予以等分為使等分後的值成為50mm以下的各點,且在軸線方向之該測量點的各者中,設為於周方向每隔30°的十二個部位(0°、30°、60°、…及330°的各位置)。在一個基材中,針對所接合之各靶節段,於前述的位置進行測量,將最大值與最小值的差設為接合材的厚度差。 The measurement position of the thickness of the joint material is set in a target segment, two points offset 10mm inward from each end of the target segment in the axial direction, and these two points are The measured points are divided equally into points such that the equally divided value becomes 50 mm or less, and each of the measuring points in the axial direction is divided into twelve positions (0°, 30°) every 30° in the circumferential direction. °, 60°, ... and 330° positions). In one base material, each target segment to be bonded was measured at the aforementioned position, and the difference between the maximum value and the minimum value was defined as the thickness difference of the bonded materials.
此外,使用深度規測量相鄰之靶材間之所有的段差量h,求出段差量h的最大值。 In addition, use a depth gauge to measure all the step differences h between adjacent targets, and find the maximum value of the step difference h.
此外,使用測隙規測量相鄰之靶材間之所有的軸方向距離d,求出其最大值與最小值的差。 In addition, use a feeler gauge to measure all axial distances d between adjacent targets, and find the difference between the maximum value and the minimum value.
相鄰之靶材間之所有段差量h及軸方向距離d的測量位置,係設為在周方向每隔30°的十二個部位(0°、30°、60°、…及330°的各位置)。 The measurement positions of all step differences h and axial distance d between adjacent targets are set to twelve locations (0°, 30°, 60°, ... and 330°) every 30° in the circumferential direction. each location).
<實施例2> <Example 2>
在實施例1中,將最長的圓筒形靶材變更為850mm者,除此以外,均與實施例1同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 1, except that the longest cylindrical target material was changed to 850 mm, an ITO cylindrical sputtering target (sample) was manufactured in the same manner as in Example 1, and each value was measured.
<實施例3> <Example 3>
在實施例1中,將最長的圓筒形靶材變更為1100mm者,除此以外,均與實施例1同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 1, except that the longest cylindrical target material was changed to 1100 mm, the ITO cylindrical sputtering target (sample) was manufactured similarly to Example 1, and each value was measured.
<實施例4> <Example 4>
在實施例1中,將最長的圓筒形靶材變更為1450mm者,除此以外,均與實施例1同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 1, except that the longest cylindrical target was changed to 1450 mm, an ITO cylindrical sputtering target (sample) was manufactured in the same manner as in Example 1, and each value was measured.
<實施例5> <Example 5>
在實施例4中,將圓筒形基材的加熱變更為未實施。亦即,取代將圓筒形基材置入於電爐內進行加熱且測量加熱後的翹曲幅度Y,而是以不進行加熱的方式,使用衝壓機進行加工,將圓筒形基材之長度方向中央部朝與原本翹曲之方向(-+-方向)相反之方向(-方向)進行加壓,而使之朝該相反之方向(-方向)翹曲達幅度α(=X×1.0),除此以外,均與實施例4同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 4, the heating of the cylindrical base material was changed to not be performed. That is, instead of placing the cylindrical base material in an electric furnace for heating and measuring the warp amplitude Y after heating, a stamping machine is used to process the cylindrical base material without heating, and the length of the cylindrical base material is The central part of the direction is pressurized in the direction (- direction) opposite to the original direction of warping (-+- direction), so that it can warp in the opposite direction (- direction) by an amplitude α (=X×1.0) , Except for this, an ITO cylindrical sputtering target (sample) was produced in the same manner as in Example 4, and each value was measured.
<實施例6> <Example 6>
在實施例3中,將圓筒形靶材的材質變更為IGZO,除此以外,均與實施例3同樣地製造IGZO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 3, except that the material of the cylindrical target was changed to IGZO, an IGZO cylindrical sputtering target (sample) was manufactured in the same manner as in Example 3, and each value was measured.
<比較例1> <Comparative example 1>
在實施例2中,將使圓筒形基材翹曲的加工變更為未實施,除此以外,均與實施例2同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 2, an ITO cylindrical sputtering target (sample) was manufactured in the same manner as in Example 2 except that the processing to warp the cylindrical base material was not performed, and each value was measured. .
<比較例2> <Comparative example 2>
在實施例2中,在使圓筒形基材翹曲的加工步驟中,不使之翹曲至原本翹曲之方向的相反側,除此以外,均與實施例2同樣地製造ITO圓筒形濺鍍靶(樣本),且測量出各值。 In Example 2, an ITO cylinder was produced in the same manner as in Example 2, except that the cylindrical base material was not warped to the opposite side of the original warping direction in the processing step of warping it. shape sputtering target (sample), and measure each value.
[表1]
測量所使用之圓筒形基材的翹曲幅度,將該圓筒形基材朝與原本翹曲之方向相反之方向進行加壓,而使圓筒形基材朝與原本翹曲之方向相反之方向反向翹曲,藉由如此進行加工,即使圓筒形靶材的軸方向長度較長(亦即,即使至少一個圓筒形靶材的軸方向長度為750mm以上時),而且,即使經過充填接合材時的加熱(亦即,即使在充填接合材時,預先加熱圓筒形基材,或將經加 熱熔融後的接合材充填於圓筒形基材與靶材之間,而使圓筒形基材受到加熱),亦可消除圓筒形基材之翹曲的影響,結果可得知,可減小接合材之厚度之最大值與最小值的差,亦可縮小相鄰之圓筒形靶材之外周面間的段差量,還可減小相鄰之圓筒形靶材間之軸方向距離之最大值與最小值的差。 Measure the warpage amplitude of the cylindrical base material used, press the cylindrical base material in the opposite direction to the original warping direction, and make the cylindrical base material face the opposite direction to the original warping direction. By processing in this way, even if the axial length of the cylindrical target is longer (that is, even if the axial length of at least one cylindrical target is 750mm or more), and even if After heating when filling the joining material (that is, even when filling the joining material, the cylindrical base material is heated in advance, or the heated The thermally melted joining material is filled between the cylindrical base material and the target material, and the cylindrical base material is heated), which can also eliminate the influence of the warpage of the cylindrical base material. The results show that Reducing the difference between the maximum and minimum thickness of the joining material can also reduce the step difference between the outer peripheral surfaces of adjacent cylindrical targets, and can also reduce the axial direction difference between adjacent cylindrical targets. The difference between the maximum and minimum distance.
2:圓筒形基材 2: Cylindrical base material
P:加壓方向 P: Pressure direction
X:翹曲幅度 X: warp amplitude
α:幅度 α: amplitude
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