TW201242141A - Aluminum alloy sheet for battery case having good moldability and weldability - Google Patents
Aluminum alloy sheet for battery case having good moldability and weldability Download PDFInfo
- Publication number
- TW201242141A TW201242141A TW101102537A TW101102537A TW201242141A TW 201242141 A TW201242141 A TW 201242141A TW 101102537 A TW101102537 A TW 101102537A TW 101102537 A TW101102537 A TW 101102537A TW 201242141 A TW201242141 A TW 201242141A
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- Taiwan
- Prior art keywords
- mass
- cold
- aluminum alloy
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Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 25
- 239000000463 material Substances 0.000 claims abstract description 61
- 239000000203 mixture Substances 0.000 claims abstract description 19
- 239000012535 impurity Substances 0.000 claims abstract description 18
- 239000002245 particle Substances 0.000 claims abstract description 15
- 239000000126 substance Substances 0.000 claims abstract description 8
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 5
- 229910052751 metal Inorganic materials 0.000 claims description 17
- 239000002184 metal Substances 0.000 claims description 17
- 230000001747 exhibiting effect Effects 0.000 claims 1
- HBBGRARXTFLTSG-UHFFFAOYSA-N Lithium ion Chemical compound [Li+] HBBGRARXTFLTSG-UHFFFAOYSA-N 0.000 abstract description 6
- 229910001416 lithium ion Inorganic materials 0.000 abstract description 6
- 229910052782 aluminium Inorganic materials 0.000 abstract description 5
- 229910018084 Al-Fe Inorganic materials 0.000 abstract description 4
- 229910018192 Al—Fe Inorganic materials 0.000 abstract description 4
- 229910052742 iron Inorganic materials 0.000 abstract description 2
- 229910052748 manganese Inorganic materials 0.000 abstract description 2
- 239000011324 bead Substances 0.000 description 54
- 238000011156 evaluation Methods 0.000 description 35
- 230000002159 abnormal effect Effects 0.000 description 33
- 230000000052 comparative effect Effects 0.000 description 26
- 238000003466 welding Methods 0.000 description 26
- 238000012360 testing method Methods 0.000 description 25
- 238000005266 casting Methods 0.000 description 21
- 238000005097 cold rolling Methods 0.000 description 21
- 230000035515 penetration Effects 0.000 description 19
- 238000000137 annealing Methods 0.000 description 18
- 239000012071 phase Substances 0.000 description 15
- 239000000956 alloy Substances 0.000 description 14
- 230000004927 fusion Effects 0.000 description 14
- 229910045601 alloy Inorganic materials 0.000 description 13
- 238000000034 method Methods 0.000 description 12
- 229910000765 intermetallic Inorganic materials 0.000 description 9
- 238000000265 homogenisation Methods 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 230000008018 melting Effects 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 238000009864 tensile test Methods 0.000 description 6
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 5
- 238000007872 degassing Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 238000005098 hot rolling Methods 0.000 description 5
- 239000001257 hydrogen Substances 0.000 description 5
- 229910052739 hydrogen Inorganic materials 0.000 description 5
- 238000005259 measurement Methods 0.000 description 5
- 238000007670 refining Methods 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 238000009749 continuous casting Methods 0.000 description 4
- 235000011389 fruit/vegetable juice Nutrition 0.000 description 4
- 239000011261 inert gas Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 229910052707 ruthenium Inorganic materials 0.000 description 4
- 238000004090 dissolution Methods 0.000 description 3
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 3
- 229910052737 gold Inorganic materials 0.000 description 3
- 239000010931 gold Substances 0.000 description 3
- 238000010191 image analysis Methods 0.000 description 3
- 150000002736 metal compounds Chemical class 0.000 description 3
- 238000012552 review Methods 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 239000000839 emulsion Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 150000002500 ions Chemical class 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 229920005992 thermoplastic resin Polymers 0.000 description 2
- KZEVSDGEBAJOTK-UHFFFAOYSA-N 1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)-2-[5-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidin-5-yl]-1,3,4-oxadiazol-2-yl]ethanone Chemical compound N1N=NC=2CN(CCC=21)C(CC=1OC(=NN=1)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)=O KZEVSDGEBAJOTK-UHFFFAOYSA-N 0.000 description 1
- JXDXANRCLTZYDP-UHFFFAOYSA-N 2-[3-(1,4-diazepan-1-ylmethyl)-4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]pyrazol-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound N1(CCNCCC1)CC1=NN(C=C1C=1C=NC(=NC=1)NC1CC2=CC=CC=C2C1)CC(=O)N1CC2=C(CC1)NN=N2 JXDXANRCLTZYDP-UHFFFAOYSA-N 0.000 description 1
- FYELSNVLZVIGTI-UHFFFAOYSA-N 2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-5-ethylpyrazol-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C=1C=NN(C=1CC)CC(=O)N1CC2=C(CC1)NN=N2 FYELSNVLZVIGTI-UHFFFAOYSA-N 0.000 description 1
- CONKBQPVFMXDOV-QHCPKHFHSA-N 6-[(5S)-5-[[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]piperazin-1-yl]methyl]-2-oxo-1,3-oxazolidin-3-yl]-3H-1,3-benzoxazol-2-one Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)N1CCN(CC1)C[C@H]1CN(C(O1)=O)C1=CC2=C(NC(O2)=O)C=C1 CONKBQPVFMXDOV-QHCPKHFHSA-N 0.000 description 1
- -1 A1 Fe-Si Chemical class 0.000 description 1
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910001152 Bi alloy Inorganic materials 0.000 description 1
- YMRMGNMHZNFVAE-UHFFFAOYSA-N C(CCC)[Ru] Chemical compound C(CCC)[Ru] YMRMGNMHZNFVAE-UHFFFAOYSA-N 0.000 description 1
- 229910017082 Fe-Si Inorganic materials 0.000 description 1
- 229910017133 Fe—Si Inorganic materials 0.000 description 1
- 102100031180 Hereditary hemochromatosis protein Human genes 0.000 description 1
- 101000993059 Homo sapiens Hereditary hemochromatosis protein Proteins 0.000 description 1
- 229910000858 La alloy Inorganic materials 0.000 description 1
- 229910000656 Lu alloy Inorganic materials 0.000 description 1
- 206010039897 Sedation Diseases 0.000 description 1
- 241001062472 Stokellia anisodon Species 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910052785 arsenic Inorganic materials 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 230000001914 calming effect Effects 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 238000004040 coloring Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000005485 electric heating Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001802 infusion Methods 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000004020 luminiscence type Methods 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 150000002737 metalloid compounds Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 235000012149 noodles Nutrition 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- FTIMWVSQXCWTAW-UHFFFAOYSA-N ruthenium Chemical compound [Ru].[Ru] FTIMWVSQXCWTAW-UHFFFAOYSA-N 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 230000036280 sedation Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000004611 spectroscopical analysis Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 229910052712 strontium Inorganic materials 0.000 description 1
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/10—Primary casings; Jackets or wrappings
- H01M50/116—Primary casings; Jackets or wrappings characterised by the material
- H01M50/117—Inorganic material
- H01M50/119—Metals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/32—Bonding taking account of the properties of the material involved
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/05—Accumulators with non-aqueous electrolyte
- H01M10/052—Li-accumulators
- H01M10/0525—Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodes; Lithium-ion batteries
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/10—Primary casings; Jackets or wrappings
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/10—Primary casings; Jackets or wrappings
- H01M50/131—Primary casings; Jackets or wrappings characterised by physical properties, e.g. gas permeability, size or heat resistance
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Manufacturing & Machinery (AREA)
- Sealing Battery Cases Or Jackets (AREA)
Abstract
Description
201242141 六、發明說明: c發明戶斤屬之技術領城】 發明領域 本發明係有關於一種使用於鋰離子電池等的二次電池 用容器之成形性及雷射熔接性優異的高強度鋁合金板。 發明背景 由於A1 - Μη系的3 000系合金在強度、成形性及雷射熔接 性較優異’因而被當作製造鋰離子電池等二次電池用容器 時之素材使用,乃在成形為期望的形狀後,藉由雷射熔接 加以封結密封作為二次電池用容器使用。並且,還有開發 一種將前述3000系合金與既存的3〇〇〇系合金作為基底,進 一步提高強度及成形性的二次電池容器用鋁合金板。 例如’在專利第4001007號公報中有記載一種矩形剖面 電池容器用铭合金板’其特徵在於:作為鋁合金板的組成 含有:Si : 0.10〜0.60質量%、Fe : 0.20~0.60質量%、Cu : 〇.1〇〜0.70 質量 〇/〇、Μη : 0.60〜1.50 質量 %、Mg : 0.20〜1.20 質量%、Zr :超過0.12且低於〇.20質量%、Ti : 〇 〇5〜〇 25質 量%、及B : 0.0010〜〇_〇2質量。/。,剩餘部分係由八丨與無法避 免之雜質所構成’且在圓筒容器深引伸成形法中,相對於 軋延方向的45突耳率為4〜7%。 另一方面’最近亦有開發一種作為電池外殼具有充分 的強度與引伸-引縮加工性、及潛變特性,且雷射熔接性優 異可抑制充電放電循環時外殼厚度增加的方型鋰離子電池 201242141 外殼用鋁合金板。在特開2010_126804號公報中則有記載一 種方型電池容器用鋁合金板,其含有Μη: 0.8質量%以上且 1.8質量°/。以下、Mg :超過〇 6質量%且在1.2質量%以下、及 Cu :超過0.5質量%且在丨5質量。/。以下,並將作為雜質的Fe 限制在0.5質量。/〇以下且將Si限制在〇 3質量%以下,剩餘部 分則具有由A1及無法避免之雜質所構成之組成,又, {001}<100>方位之方位密度方位之方位密 度S之比(C/S)在0.65以上且在1.5以下,此外,最終冷軋延 後之拉伸強度在25〇MPa以上且在330MPa以下,且延伸在 1%以上。 然而’眾知’在以3〇〇〇系合金為基底將其組成加以改 良之鋁合金板中,也有熔接熔入深度不足的問題,有時可 能會產生異常焊珠而在雷射熔接性上有問題。 爰此,亦有開發一種以丨000系為基底且雷射熔接性優 異的一—人電池容器用鋁合金板。在特開2009-127075號公報 中有Z載種脈衝雷射溶接用㉝合金材及電池外殼,其可 將A10叫料藉由脈衝雷㈣接來防止異常部的產生並 均勻地形成良好⑽接.根據該内容,習知,在鱗造過 程中用以抑制結晶粒粗大化所添加的了丨會對熔接部帶來不 良〜a因此,為了防止藉由脈衝雷射熔接將A1 〇〇〇系鋁予 以溶接時之異常部的形成,僅須將含於純财之Ti限制在 低於0.01質量%即可。 ,此外’作為以3_系合金為基底且已改良高強度、成 形r生及炼接性的!呂合金,在特開細3·7施號公報中有記 201242141 載-種由Mn:G.3〜質量超過ι()且至i8質量%、 剩餘。卩刀為A1及無法避免之雜質所構成的二次電池外殼 ,呂口金板還可含有Cu:〇」〜〇謂量%及/或Mg:超過請 l-〇f s% A/^Qr. 〇-〇5~〇.2f 4〇/oA/^Zr: 0.05^0.2 量%。但’對於炫接性並未有詳細的檢討。 配潑^明内容】 發明概要 確實’在1GGG系巾具有料性穩定(異常焊珠數量少) 成形!生優異但強度低之問題1以,在經離子電池大型 化的進展巾職亦有高強度特性之要求,因此,直接適用 1000系的鋁材將有所問題。 扣如則述’在3000系的合金板中,雖可獲得強度與深炫 里:度j旦與1000系的合金板相較之下,有成形性較差且 Ί焊珠數較多之傾向。又,在i刪系的合金板中雖然 、邊優異且異常焊珠數降低’但有強度不足之問題。 本發明係用以解決如上述之課題所提出者,其目的在 '、種具有可適用於大型鋰離子電池容器的高強度、 成形性優異、雷射轉性亦優異的A1m呂合金板。 為了達成其目的’本發明之成形性及熔接性優異之電 /也外设用銘合金板之特徵在於:其具有下述化學組成及圓 等效彳二長5μπι以上的第2相粒子數低於5〇〇個/rmn2的金屬組 織°亥化學組成為:含有Fe : 0.3〜1.5質量%、Mn : 0.3-1.0 暂旦〇/ 里。、Cu : 0.2〜1.〇 質量%、Mg : 0.2〜1_〇質量%、Ti : 〇‘〇02〜〇·20質量0/〇、及Zr : 0.05〜0.20質量%,且Mn/Fe之質 201242141 量比為0.2〜1.0,又,剩餘部分係由八丨及無法避免之雜質所 構成’且作為無法避免之雜質之Si係低於〇 3〇質量%。 在為冷軋未退火材的情況下為呈現2%以上的延伸值且 160MPa以上的拉伸強度者。又,在為冷軋退火材的情況下 則為呈現20%以上的延伸值且丨3〇Mpa以上的拉伸強度者。 由於本發明之紹合金板具有高強度且成形性亦佳,並 具備有良好的雷射熔接性,因此可以低成本製造密閉性能 佳且可抑制膨脹的二次電池用容器。 尤其,在為冷軋未退火材的情況下具有2%以上的延伸 值且16GMPa以上的拉伸強度,又,在為冷軋退火材的情況 下’不僅有13GMPa以上的拉伸強度且延伸值在2()%以上, 展現出良好的成形性。 圖式簡單說明 第1圖係說明異常焊珠數之敎/評估方法的概念圖, ()為炼接焊珠之俯視圖,及⑻為顯示沿著焊珠長度方向之 焊珠寬度變化的圖表。 第2圖係說明炫入深度之測定/評估方法的概念圖,(a) 為溶接焊珠之俯視圖,及(B)為剖面圖。 ^ 用以實施發明之形態 .人電A係將電極體放人容器中以後,藉由熔接等覆 電力X在封所製造。若將此種二次電池使用在行動 六祕 t有充電時谷器内部溫度上升而使容器内部的壓 之It况。所以,當塑造容器的材料強度太低時,有 6 201242141 在所製造之容器產生大大的_之問題。因此,使 料必須具有高強度。 又,由於一般係使用壓製法來作為塑造容器之方法, 因此使用的材料本身須具有良好的壓製成形性。 而且,由於作為覆蓋上蓋子加以密封之方法係使用炫 接法,因此亦要求熔接性優異。還有,作為製造二:欠電+ 用容器等時的熔接法’多使用雷射熔接法。 ’ 而,有關雷射溶接性之課題,例如有:⑴炫接焊珠寬 度之穩定性、熔人深度之穩定性;及⑺獲得相對於溶接悍 珠寬度更深的熔入深度。 般而& 旦熔接焊珠寬度變寬,炼人深度亦有加 =之傾向。所以,可能會局部地在異常焊珠部中產生炼接 焊珠寬度打、m深度加^,嚴重時可能產生熔融部 的貫穿等,而招致電池性能或可#性的降低。 又在另-方面,為了調查炫入深度,必須觀察多處的 加,相當耗費勞力。但,如前述,在同-合金内,熔接 焊珠寬度舰人深度具有相關,從該點看來,藉由測定溶 接焊珠寬絲_異常(粗大)焊珠,可輕易地触問題所在 的異常炼入深度之焊珠比率。 本發月人等為了獲得一種高強度且壓製成形性優異, 並透過生成赠接部之異常焊珠數祕接部中之熔入深度 =查發現雷_接性亦佳私合金板,不斷地重複精關 檢討而達至本發明。 於以下說明其内容。 201242141 首先,說明本發明之二次電池容器用鋁合金板中含有 的各元素之作用、及適當含量等。201242141 VI. Description of the Invention: The invention relates to a high-strength aluminum alloy excellent in formability and laser weldability of a container for a secondary battery used in a lithium ion battery or the like. board. Background of the Invention Since the A1 - Μ 的 3 000 series alloy is excellent in strength, formability, and laser fusion property, it is used as a material for manufacturing a secondary battery container such as a lithium ion battery, and is formed into a desired shape. After the shape, the seal is sealed by laser welding and used as a container for a secondary battery. Further, there has been developed an aluminum alloy sheet for a secondary battery container which further improves the strength and formability by using the above-described 3000 series alloy and an existing three-bismuth alloy as a base. For example, in the patent publication No. 4001007, a metal alloy plate for a rectangular cross-section battery container is characterized in that the composition of the aluminum alloy plate contains: Si: 0.10 to 0.60% by mass, Fe: 0.20 to 0.60% by mass, Cu : 〇.1〇~0.70 Mass 〇/〇, Μη: 0.60~1.50% by mass, Mg: 0.20~1.20% by mass, Zr: more than 0.12 and less than 20.20% by mass, Ti: 〇〇5~〇25 mass %, and B: 0.0010~〇_〇2 quality. /. The remainder is composed of gossip and unavoidable impurities' and in the deep extension forming method of the cylindrical container, the 45-ear ratio with respect to the rolling direction is 4 to 7%. On the other hand, 'a lithium-ion battery with sufficient strength, extension-shrinkage processability, and creep characteristics as a battery case, and excellent in laser fusion properties to suppress an increase in the thickness of the case during charge and discharge cycles has recently been developed. 201242141 Aluminum alloy plate for outer casing. Japanese Laid-Open Patent Publication No. 2010-126804 discloses an aluminum alloy plate for a prismatic battery container, which contains Μη: 0.8% by mass or more and 1.8% by mass/. Hereinafter, Mg: more than 〇6 mass% and 1.2 mass% or less, and Cu: more than 0.5 mass% and 丨5 mass. /. Hereinafter, Fe as an impurity is limited to 0.5 mass. /〇 below and Si is limited to 〇3 mass% or less, and the remaining portion has a composition composed of A1 and unavoidable impurities, and a ratio of azimuthal density S of azimuth density orientation of {001}<100> azimuth (C/S) is 0.65 or more and 1.5 or less, and further, the tensile strength after the final cold rolling is 25 MPa MPa or more and 330 MPa or less, and the elongation is 1% or more. However, in the aluminum alloy plate whose composition is improved by using a 3 lanthanum alloy as a base, there is also a problem that the fusion fusion depth is insufficient, and an abnormal weld bead may be generated in the case of laser fusion. something wrong. In view of this, there has also been developed an aluminum alloy sheet for a human battery container which is based on the 丨000 series and which is excellent in laser welding properties. In Japanese Laid-Open Patent Publication No. 2009-127075, there is a 33-type alloy material for a pulsed laser welding and a battery casing, which can be used to prevent the occurrence of an abnormal portion and uniformly form a good (10) connection by means of a pulsed lightning (four). According to this content, it is conventionally known that the addition of ruthenium for suppressing the coarsening of crystal grains during the scale formation causes a defect to the welded portion. Therefore, in order to prevent the A1 from being spliced by pulsed laser welding, In the formation of the abnormal portion when the aluminum is melted, it is only necessary to limit the Ti contained in the pure money to less than 0.01% by mass. In addition, as a base based on a 3_ series alloy, it has been improved in high strength, forming r and refining! Lu alloy, which has been recorded in the special opening 3·7 application bulletin 201242141, contains Mn:G.3~mass over ι() and to i8 mass%, and remains. The boring tool is a secondary battery case composed of A1 and unavoidable impurities. The Lvkou gold plate may also contain Cu: 〇"~〇"% and/or Mg: exceeds l-〇fs% A/^Qr. 〇 -〇5~〇.2f 4〇/oA/^Zr: 0.05^0.2% by weight. However, there is no detailed review of the splicing. In the case of the 1GGG towel, the material stability is stable (the number of abnormal beads is small). The shape is excellent. However, the problem is low, and the strength is low. The requirements for strength characteristics, therefore, direct application of 1000 series aluminum will have problems. As shown in the figure, in the 3000-series alloy sheet, strength and depth are obtained. Compared with the 1000-series alloy sheet, the moldability is poor and the number of bead balls tends to be large. Further, in the alloy sheet of the i-cut type, the edge is excellent and the number of abnormal beads is lowered, but there is a problem that the strength is insufficient. The present invention has been made to solve the above-mentioned problems, and an object thereof is to provide an A1m alloy sheet which is excellent in high strength, excellent in formability, and excellent in laser turnability, which is applicable to a large-sized lithium ion battery container. In order to achieve the object of the present invention, the electric alloy/external alloy sheet which is excellent in formability and weldability of the present invention is characterized in that it has the following chemical composition and a circular equivalent 彳 two lengths of 5 μm or more and a low number of second phase particles. The chemical composition of the metal structure at 5 / / rmn 2 is: containing Fe: 0.3 to 1.5% by mass, and Mn: 0.3-1.0 temporarily 〇 / 里. , Cu: 0.2 to 1. 〇% by mass, Mg: 0.2 to 1_〇% by mass, Ti: 〇'〇02~〇·20 mass 0/〇, and Zr: 0.05 to 0.20% by mass, and Mn/Fe The mass ratio of 201242141 is 0.2 to 1.0, and the remainder is composed of gossip and unavoidable impurities', and the Si system which is an unavoidable impurity is less than 〇3〇 mass%. In the case of cold-rolled unannealed material, it is a tensile strength of 2% or more and a tensile strength of 160 MPa or more. Further, in the case of a cold-rolled annealed material, it is a tensile strength of 20% or more and a tensile strength of 丨3〇Mpa or more. Since the alloy sheet of the present invention has high strength and good moldability, and has excellent laser welding properties, it is possible to manufacture a container for a secondary battery which has excellent sealing performance and can suppress expansion at a low cost. In particular, in the case of cold-rolled unannealed material, it has an elongation value of 2% or more and a tensile strength of 16 GMPa or more, and in the case of a cold-rolled annealed material, not only has a tensile strength of 13 GMPa or more and an elongation value. Above 2 ()%, good formability is exhibited. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a conceptual diagram showing the number of abnormal beads/evaluation method, () is a plan view of the welded bead, and (8) is a graph showing the variation of the bead width along the length of the bead. Fig. 2 is a conceptual diagram illustrating a method of measuring/evaluating the depth of penetration, (a) is a plan view of the molten solder bead, and (B) is a cross-sectional view. ^ Form for carrying out the invention. The human power A is placed in a container after the electrode body is placed in a container, and is then fabricated by welding or the like. If such a secondary battery is used in action, the internal temperature of the barn rises when charging, and the pressure inside the container is lowered. Therefore, when the material strength of the molded container is too low, there is a problem that the container produced in the 201242141 has a large problem. Therefore, the material must have high strength. Further, since the pressing method is generally used as a method of molding a container, the material used itself must have good press formability. Further, since the method of sealing by covering the upper cover is a damascene method, it is also required to have excellent weldability. Further, as the welding method in the case of manufacturing two: under-electricity + container, etc., a laser welding method is often used. Further, regarding the problem of laser fusion, there are, for example, (1) stability of the width of the soldered bead, stability of the weld depth, and (7) obtaining a deeper penetration depth with respect to the width of the molten bead. As usual, the width of the welded bead is widened, and the depth of the refining has a tendency to increase. Therefore, the width of the welded bead may be locally generated in the abnormal bead portion, and the m depth may be increased. When it is severe, the penetration of the molten portion may occur, which may cause a decrease in battery performance or availability. On the other hand, in order to investigate the depth of the sneak, it is necessary to observe the addition of multiple places, which is quite labor intensive. However, as mentioned above, in the same-alloy, the weld bead width is related to the depth of the ship. From this point of view, the problem can be easily touched by measuring the welded bead wide wire_abnormal (coarse) bead. The ratio of the beads to the abnormal depth of penetration. In order to obtain a high-strength and excellent press-formability, the present-mentioned person and the like, and through the generation of the number of abnormal weld beads in the joint portion, the depth of penetration in the joint portion is found to be arbitrarily Repeat the fine review to achieve the present invention. The contents are explained below. 201242141 First, the action, the appropriate content, and the like of each element contained in the aluminum alloy plate for a secondary battery container of the present invention will be described.
Fe : 0.3〜1.5質量% F e係用以使鋁合金板強度增加並確保雷射熔接之熔入 深度的必要元素。Fe含量若低於〇3質量%,便會使鋁合金 板強度降低且使雷射熔接時之熔入深度減少,故非理想。 Fe含量若超過1.5質量%,則鑄塊鑄造時會結晶出Ai_(Fe · Mn)-Si系及Al0Fe等粗大介金屬化合物而使最終板之成形性 降低,且在雷射溶接時該等介金屬化合物與A丨基質相較之 下較易蒸發而使異常焊珠數增加、熔接性降低,故非理想。 所以,Fe含量係設在5質量%之範圍。較理想的 Fe含量在0.5〜1.5質量。/◦之範圍。更理想的以含量在〇ί 5 質量%之範圍。 Μη : 0.3〜1.0 質量 % Μη係用以使鋁合金板強度增加並確保雷射熔接之熔 入深度的必要元素。Μη含量若低於〇 3質量%,便會使鋁合 金板強度降低且使雷射熔接時之熔入深度減少,故非理 想》Μη含s若超過1 ·〇質量%,則在鑄塊鑄造時會結晶出 Al-(Fe · Mn)-Si系及AUMn等粗大介金屬化合物而使最終板 之成形性降低,且在雷射熔接時該等介金屬化合物與A1基 質相較之下較易蒸發而使異常焊珠數增加、熔接性降低, 故非理想。 所以,Μη含量係設在0.34 〇質量%之範圍。較理想的 Μη含量在0.3〜0.8質量%之範圍。更理想的^^^含量在〇 4〜〇 7 8 201242141 質量。/。之範圍。Fe : 0.3 to 1.5% by mass F e is an essential element for increasing the strength of the aluminum alloy sheet and ensuring the penetration depth of the laser welding. If the Fe content is less than 〇3 mass%, the strength of the aluminum alloy sheet is lowered and the penetration depth at the time of laser welding is reduced, which is not preferable. When the Fe content is more than 1.5% by mass, a coarse intermetallic compound such as Ai_(Fe · Mn)-Si-based or Al0Fe is crystallized during casting, and the formability of the final sheet is lowered, and the fusion is performed at the time of laser fusion. The metal compound is more likely to evaporate than the A ruthenium matrix, and the number of abnormal beads is increased and the weldability is lowered, which is not preferable. Therefore, the Fe content is set in the range of 5% by mass. The desirable Fe content is 0.5 to 1.5 mass. / Range of ◦. More desirably, the content is in the range of 〇ί 5 % by mass. Μη : 0.3~1.0 mass % Μη is an essential element for increasing the strength of the aluminum alloy sheet and ensuring the penetration depth of the laser welding. If the content of Μη is less than 〇3% by mass, the strength of the aluminum alloy sheet is lowered and the penetration depth at the time of laser welding is reduced, so that the non-ideal Μη contains s if it exceeds 〇% by mass, and is cast in the ingot. When the coarse intermetallic compound such as Al-(Fe.Mn)-Si and AUMn is crystallized, the formability of the final sheet is lowered, and the metal compound is easier to compare with the A1 matrix during laser welding. Evaporation increases the number of abnormal beads and reduces the weldability, which is not desirable. Therefore, the Μη content is set in the range of 0.34 〇 mass%. A more desirable Μη content is in the range of 0.3 to 0.8% by mass. More ideal ^^^ content in 〇 4~〇 7 8 201242141 quality. /. The scope.
Ti : 0.002〜0.20質量0Ti : 0.002~0.20 mass 0
Ti可在鑄塊鑄造時作為晶粒微化劑起作用來防止禱造 裂痕。當然,Ti可單獨添加,但藉由與B共存,更可期待強 力的結晶粒之微化效果’因此亦可以桿式硬化機來添加 Al-5%Ti-l%B 等。Ti acts as a grain refiner to prevent pray cracking when the ingot is cast. Of course, Ti can be added alone, but by coexistence with B, a sharpening effect of strong crystal grains can be expected. Therefore, Al-5% Ti-l% B or the like can be added by a rod type hardening machine.
Ti含量若低於0.002質量%,會使鑄塊鑄造時之微化效 果不夠充分,故而有招致鑄造裂痕之虞,並非理想。又, Ti含量若超過0.20質量%,則在鑄塊鑄造時會結晶出ΉΑΐ3 等粗大介金屬化合物而使最終板之成形性降低,故非理想。 所以,Ti含量係設在0.002〜0.20質量%之範圍。較理想 的Ti含量在0.002〜0.15質量%之範圍。更理想的丁丨含量在 0.005〜0.10質量%之範圍。If the Ti content is less than 0.002% by mass, the effect of miniaturization at the time of casting the ingot is insufficient, so that it is not preferable because of the occurrence of casting cracks. In addition, when the Ti content is more than 0.20% by mass, a coarse intermetallic compound such as ruthenium 3 crystallizes during casting of the ingot, and the formability of the final sheet is lowered, which is not preferable. Therefore, the Ti content is set in the range of 0.002 to 0.20% by mass. A desirable Ti content is in the range of 0.002 to 0.15 mass%. More preferably, the content of butyl ruthenium is in the range of 0.005 to 0.10% by mass.
Zr : 0·05〜0.20質量%Zr : 0·05~0.20% by mass
Zr與Ti同樣地可在鑄塊鑄造時作為晶粒微化劑起作用 來防止鑄造裂痕。又,若使丁丨與心共存,可防止伴隨急冷 凝固之熔接焊珠部在凝固時的裂痕發生,而達到脈衝雷射 熔接之高速化。若使Ti、Zr及B共存,則可使防止伴隨急冷 凝固之熔接焊珠部在凝固時產生裂痕的效果更加顯著。Like Ti, Zr acts as a grain refiner to prevent casting cracks when the ingot is cast. Further, by coexisting the butadiene and the heart, it is possible to prevent the occurrence of cracks in the welded bead portion which is rapidly solidified and solidified, and to increase the speed of the pulsed laser welding. When Ti, Zr, and B are coexisted, the effect of preventing cracking of the welded bead portion accompanying rapid solidification during solidification can be made more remarkable.
Zr含量若超過〇.2〇質量%,在鑄塊鑄造時會結晶出 ZrAb等粗大介金屬化合物而使最終板之成形性降低,故柞 理想。Zr含量若低於〇.05質量%則無法獲得充分的效果。所 以’理想的Zr含量為〇.〇5〜0_20質量%。較理想的Zr含量在 〇·〇7〜0.20質量%之範圍。更理想的Zr含量在〇.〇7〜〇. 18質量% 201242141 之範圍。 B : 0·〇〇〇5〜o.io質量% Β亦與Ti、Zr同樣地可在鑄塊鑄造時作為晶粒微化劑起 作用來防止鑄造裂痕。因此,可視需要而含有。 B含篁若超過〇.1〇質量%,會使TiB2變成穩定化的介金 屬化合物而使晶粒微化效果衰減,並有引起DI成形後之外 觀表皮粗糙之虞,故非理想。B含量若低於0.0005質量❶/〇則 無法獲得充分的晶粒微化效果。所以,理想的B含量為 〇·〇〇〇5〜〇_1〇質量%。較理想的β含量在〇.〇〇卜〇 〇5質量%之 範圍。更理想的Β含量在0.001〜〇.〇1質量%之範圍。When the Zr content exceeds 〇2% by mass, a coarse intermetallic compound such as ZrAb is crystallized during casting of the ingot, and the formability of the final sheet is lowered. If the Zr content is less than 〇05.5% by mass, a sufficient effect cannot be obtained. Therefore, the ideal Zr content is 〇.〇5 to 0_20% by mass. The desirable Zr content is in the range of 〜·〇7 to 0.20% by mass. A more desirable Zr content is in the range of 〇.〇7~〇. 18% by mass 201242141. B: 0·〇〇〇5 to o.io% by mass Β Similarly, Ti and Zr can be used as a grain refining agent to prevent casting cracks during casting of the ingot. Therefore, it can be included as needed. When B contains more than 〇1% by mass, TiB2 becomes a stabilized metalloid compound, and the grain refining effect is attenuated, and it is not desirable because the skin is roughened after the formation of DI. If the B content is less than 0.0005 mass ❶ / 〇, sufficient grain miniaturization effect cannot be obtained. Therefore, the ideal B content is 〇·〇〇〇5~〇_1〇% by mass. The ideal β content is in the range of 质量.〇〇卜〇 〇5 mass%. A more desirable strontium content is in the range of 0.001 to 〇.〇1% by mass.
Cu含量:〇·2〜1.〇質量〇/〇Cu content: 〇·2~1.〇Quality 〇/〇
Cu係藉由與Mg—起作為CuMgAl2相而析出至Α1基質 中使鋁合金板強度增加。Cu含量若低於〇.2質量%,則強度 之增加會不夠充分,並非理想。又,相反地,CU含量若多 到超過1.0質量’便會使最終板之成形性降低,故非理想。 所以’ Cu含量係設在0.2〜1.0質量%之範圍。較理想的 Cu含量在〇·2〜0.9質量%之範圍。更理想的Cu含量在〇2〜〇8 質量°/〇之範圍。Cu is precipitated into the ruthenium matrix by precipitation with Mg as a CuMgAl2 phase to increase the strength of the aluminum alloy sheet. If the Cu content is less than 0.2% by mass, the increase in strength may be insufficient, which is not preferable. On the other hand, if the CU content is more than 1.0 mass, the formability of the final sheet is lowered, which is not preferable. Therefore, the 'Cu content is set in the range of 0.2 to 1.0% by mass. The desirable Cu content is in the range of 〇·2 to 0.9% by mass. A more desirable Cu content is in the range of 〇2 to 〇8 mass ° / 〇.
Mg含量:〇.2〜1.0質量%Mg content: 〇.2~1.0% by mass
Mg係藉由與Cu —起作為CuMgAh相而析出至A1基質 中使鋁合金板強度增加。Mg含量若低於〇.2質量%,則強度 之增加會不夠充分,並非理想。又,相反地,Mg含量若多 到超過1.0質量% ’則雷射熔接時會有氧化皮膜產生而使熔 接性降低,故非理想。 201242141 所以,Mg含量係設在0.2〜1_0質量%之範圍。較理想的 Mg含量在0.2〜0.9質量%之範圍。更理想的Mg含量在〇.2〜〇.8 質量%之範圍。 作為無法避免之雜質之Si含量:低於〇.3〇質量% 作為無法避免之雜質之Si含量以限制在低於〇 3〇質 量%為佳。Si含重若在〇.30質莖%以上’在鑄塊铸造時會結 晶出Al-(Fe · Mn)-Si等粗大介金屬化合物而使成形性降低。 較理想的Si含量為低於0.25質量%。更理想的Si含量為低於 0.20質量%。 在本發明中,只要Si含量低於0.20質量。/。,就不會有成 形性及熔接性等特性降低。 其他無法避免之雜質 無法避免之雜質係無法避免地從原料裸金屬或回爐廢 料等混入者,該等的可許容含量為例如:Zn低於〇.25質量 。/〇 ; Ni低於0.20質量% ; G^v低於〇.〇5質量% ; Pb、Bi、 Sn、Na、Ca ' Sr分別低於0.02質量% ;且其他各低於〇 〇5 質量%;只要在該範圍内’即便含有管理外之元素,亦不 會妨礙本發明之效果。The Mg system is precipitated into the A1 matrix by Cu as a CuMgAh phase, and the strength of the aluminum alloy sheet is increased. If the Mg content is less than 0.2% by mass, the increase in strength may be insufficient, which is not preferable. On the other hand, when the content of Mg is more than 1.0% by mass, the oxide film is generated during laser welding, and the weldability is lowered, which is not preferable. 201242141 Therefore, the Mg content is set in the range of 0.2 to 1% by mass. A desirable Mg content is in the range of 0.2 to 0.9% by mass. More preferably, the Mg content is in the range of 〇.2 to 〇.8 mass%. Si content as an unavoidable impurity: less than 〇.3 〇 mass% The Si content as an unavoidable impurity is preferably limited to less than 〇 3 〇 mass %. If the Si content is more than 〇.30 stalks or more, when the ingot is cast, a coarse intermetallic compound such as Al-(Fe·Mn)-Si is crystallized to lower the formability. A desirable Si content is less than 0.25 mass%. A more desirable Si content is less than 0.20% by mass. In the present invention, as long as the Si content is less than 0.20 mass. /. There is no deterioration in properties such as formability and weldability. Other unavoidable impurities Unavoidable impurities are inevitably mixed from bare metal or recycled waste materials. For example, the allowable content of Zn is less than 〇.25 mass. /〇; Ni is less than 0.20% by mass; G^v is less than 〇.〇5 mass%; Pb, Bi, Sn, Na, Ca 'Sr are respectively less than 0.02% by mass; and others are less than 〇〇5 mass% As long as the elements other than the management are contained within the range, the effects of the present invention are not hindered.
Mn/Fe之質量比:on 〇 在本發明範圍内的Fe、Μη含量之範圍内,Mn/Fe比若 低於0.2,則雷射熔接時之熔入深度會減少,故非理想。在 本發明範圍内的Fe、Μη含量之範圍内,Mn/Fe比若超過 L〇,會使異常焊珠數增加,故非理想。 另外,Mn/Fe之質量比會對鑄塊鑄造時結晶出之介金屬 201242141 化合物的種類及數量造成影響。例如:眾知當Mn/Fe質量比 一旦增加,Α^Μη系介金屬化合物之數量亦會增加。 另一方面,雷射熔接時,該等Α丨όΜη等介金屬化合物與 A1 Fe-Si、Alje、AbFe等介金屬化合物相較之下較易蒸發 且不穩定。因此,Mn/Fe比若超過;!.〇,可能會使雷射熔接 時之異常焊珠數增加而使溶接性降低。 又,Μη係藉由固溶於A1基質中來增加材料之熱阻,因 此在確保雷射熔接時之熔入深度之點而言,為比Fe更重要 的元素。因此,Mn/Fe比若低於〇.2,可能會使雷射熔接時 之熔入深度不夠充分。 拉伸強度及延伸值冷軋未退火材:延伸值2%以上且拉伸強 度160MPa以上,冷軋退火材:延伸值2〇%以上且拉伸強度 130MPa以上 而,將Al-Fe系鋁合金板適用於大型鋰離子電池容器等 時’不僅須具有高強度及良好的雷射溶接性,亦需要有良 好的成形性。材料強度可以進行拉伸試驗時之拉伸強度得 知’又,成形性可以拉伸試驗時之延伸值得知。 詳細將於後述之實施例記載,就適用於大型链離子電 池容窃等之本發明之Al-Fe系紹合金板而言,為冷軋未退火 材時’以具有延伸值2%以上且拉伸強度16〇MPa以上之特性 者為宜;為冷軋退火材時’則以具有延伸值20%以上且拉 伸強度130MPa以上之特性者為宜。 金屬組織中之圓等效徑長5μηι以上的第2相粒子數低於5〇〇 個/mm2 12 201242141 如上述之特性’可錯由仔細调整具有前述特定化學組 成之Al-Fe系鋁合金板的金屬組織而顯現。 具體而言,只要使金屬組織中之圓等效徑長5μπι以上 的第2相粒子數低於500個/mm2即可。 不論為冷軋未退火材或為冷軋退火材’在金屬組織上皆 無差異。只要具有如上述之金屬組織,在冷軋未退火材即呈 現2%以上的延伸值且i60MPa以上的拉伸強度,在冷軋退火 材則呈現20%以上的延伸值且130MPa以上的拉伸強度。 接下來’簡單介紹製造如上述之二次電池容器用紹合 金板之方法。 熔解•熔製 ^將原料投入熔解爐中,並在達到預定的熔解溫度時適 當地投人雜㈣行㈣’再視需求使时搶等進行爐内 脫氣後加以鎮靜保持,然後從料表面分離炫潰。 人 认,巧α取顶疋的合金成分,雖然母 :從紹合2原料投人亦相#重要’但直到前述輯劑及炼 間乃極:重要汁面為止,充分取得鎮靜時 鎮靜時間一般以採取30分鐘以上為宜。 以炫解爐崎製之料金 爐後再進行如★ 暫時移至保持 心的鎮㈣間為45分鐘以上。 心㈣ 視需求,亦可通過線内脫氣、遽器。 中,從旋轉轉子將惰性氣體等喷入-汁 中之乳氧擴散至惰性氣體之泡中而除去之種類為 13 201242141 主流。使用氮氣作為惰性氣體時,將露點管理在例如-60°C 以下乃相當重要。鑄塊之氫氣量宜減低至0.20cc/100g以下。 當鑄塊之氫氣量太多時,會在鑄塊之最終凝固部產生 孔隙,因此必須將熱軋延步驟中每1道次之軋縮率限制在例 如7%以上,以消去孔隙。 又,雖然可能因熱軋延步驟前之均質化處理條件而有 所不同,但過度飽和地固溶於鑄塊中之氫氣亦有可能會在 最終板之成形後的雷射熔接時析出,而於焊珠產生多數的 氣孔。所以,較理想的鑄塊之氫氣量為0.15cc/100g以下。 鑄造 鑄塊係藉由半連續鑄造(DC鑄造)而製造。在通常的半 連續鑄造中,由於鑄塊的厚度一般在400〜600mm左右,因 此鑄塊中央部的凝固冷卻速度在l°C/sec左右。所以,尤其 在將高Fe、Μη含量的鋁合金熔汁予以半連續鑄造時,在鑄 塊中央部會有Al-(Fe_Mn)-Si等較粗的介金屬化合物從鋁合 金熔汁結晶出之傾向。 半連續鑄造中之鑄造速度雖會因鑄塊的寬度及厚度而 異,但通常亦會將生產性納入考量而設為50〜70mm/min。 然而,進行線内脫氣時,若考慮到脫氣處理槽内之實質的 熔汁滯留時間,雖因惰性氣體之流量等脫氣條件而異,但 链溶汁之流量(每單位時間之溶汁供給量)愈小,愈可提升槽 内之脫氣效率進而達到減低鑄塊之氩氣量的可能性。又, 雖因鑄造的注入條數等而異,但為了減低鑄塊的氫氣量, 宜將鑄造速度限制為30〜50mm/min。更理想的鑄造速度為 14 201242141 3〇〜4〇mm/min。當然,一旦鑄造速度低於3〇mm/min,便會 使生產性降低,故非理想。而’不消說,鑄造速度愈慢, 愈可使鑄塊中之槽(sump)(固相/液相之界面)的傾斜緩和, 進而可防止鑄造裂痕。 均質化處理:42〇〜600°Cxl小時以上 對藉由半連續鎮造法鑄造而獲得之鑄塊施行均質化處理。 均質化處理係為了使軋延容易進行而將鑄塊保持在高 /m進行鑄造偏析、或解除禱塊内部殘留應力的處理。在本發 明中,必須以保持溫度420〜60(TC保持1小時以上。此時,均 質化處理亦為用以使鑄造時所結晶出構成介金屬化合物的 過渡tl素等在某程度上固溶至基質中之處理。該保持溫度過 低或保持溫度太短的情況下,會有上述過渡元素等之固溶無 法進行而使再結晶粒變粗,進而無法精美地完成DI成形後之 ,觀表皮之虞。又,一旦保持溫度過高,會有引起矯塊中細 微的最終凝固部之CuMgAl2等共晶部分熔融一即所謂的鑄 乂燒結一之虞。較理想的均質化處理溫度為42〇〜59〇。〇。 熱軋延步驟 以預定時間保持在高溫的鑄塊經過均質化處理後,直 接以活動吊具吊起並移送到熱軋延機,又,雖因熱乳延機 機種而異’但-般係藉由數次的乳延道次加以熱軋延而作 Μ定厚度-例如4〜8mm左右-的熱軋板捲取至親。 冷軋延步驟 使已捲取熱軋延板的輕通過冷軋機,且通常會施行數 道-人的冷軋延1時,會因以冷軋延而導人的塑性應變引 15 201242141 起加工硬化’因此,可視 而保持溫 中㈣亦為軟—===”, 批炼爐插人冷軋輥,以3G(M5()t的溫度進行^二= 保持。保持溫度-旦低於3GGt將無法促進軟化, 度若超過4耽齡招致處理成本之增大。又,中間退火若 藉由連續退火爐以例如45代〜55代的溫度㈣15秒鐘以 内之後再急速冷卻,亦可兼作溶體化處理1持溫度—旦 低於45〇c將無法促進軟化’而保持溫度若超過5卿則有 引起鑄砂燒結之虞。 最終退火 在本發明中’於最終冷軋延之後進行之最終退火亦可 為分批處理,例如藉由退火爐以溫度侧〜5GGt:保持1小時 以上,但若藉由連續退火爐以例如·c〜5贼的溫度保持 15秒知以内之後再急速冷卻,亦可兼作顏化處理。 不淪何者,在本發明中,最終退火並非必須,但若考 慮到-般DI成形中之成形性,則以盡可能使最終板軟化為 宜。右亦考量到模具成形㈣巾之成形性,則以作為退火 材、或溶體化處理材為宜。 在以機械強度一而非成形性—為優先之情況下,以冷 軋未退火材作提供。 最終冷軋率 施行最終退火時的最終冷軋率在50〜90%之範圍内為 宜°只要最終冷軋率在該範圍内,可使退火後之最終板的 平均再結晶粒在20〜1〇〇μηι且將延伸值設在20%以上,進而 16 201242141 可精美地完成成形後之外觀表皮。更理想的最終冷軋率在 60〜90%之範圍。 另一方面,未施加最終退火而作為冷軋未退火材時的 最終冷軋率以在5〜40%之範圍為宜。DI成形時,若引縮加 工增多’則必須提供比退火材稍微硬一些的最終板。最終 冷軋率若低於5%,雖因組成而異但會難以將最終板之拉伸 強度設在160MPa以上,又最終冷軋率若超過4〇% ,雖因組 成而異但會難以將最終板之延伸值設在2%以上。 只要最終冷軋率在該範圍内,即可將冷軋未退火最終 板之延伸值設在2%以上且將拉伸強度設在16〇Mpa以上。更 理想的最終冷軋率在1〇〜3〇%之範圍。 藉由經過如上的—般步驟,可獲得二次電池容器用鋁 合金板。 實施例 最終板之作成 將預疋的各種鑄錠予以計量、摻混後,將各(合計8 個供试材)的鑄錠插入填裝至有塗佈脫模材之細掛禍中。 將違等㈣插人電爐内並以·。c加以轉除去熔紐將 炫汁'现度保持在76〇°C,接下來將脫炫邊用助炫劑各6g包入 鋁落中並以塞進器壓入添加。 $接下來’於炫汁中插入喷搶,以流量l.OL/min喷入N2 乳體1〇分鐘以進行脫氣處理。然後進行30分. 鐘的鎮靜,再 媒^ "棒除去浮在熔汁表面上之熔渣後,以勺具採取盤形 樣本至成分分析用鑄模中。 17 201242141 再來’使用夾具依序從電爐内取出坩堝,並於業已預 熱的模具(250mmx200mmx30mm)中縳入銘熔汁。各供試材 的盤开> 樣本係藉由發光分光分析進行組成分析。其結果顯 示於表1。 表1 :供試材的成分組成 供試材 No. 成分組成(質量%) Mn/Fe Si Fe Μη Cu Mg Ti Zr B 實施例1 0.08 1.28 0.50 0.51 0.51 0.08 0.10 0.005 0.39 實施例2 0.07 1.30 0.31 0.76 0.84 0.08 0.10 0.004 0.24 實施例3 0.07 1.27 0.50 0.51 0.51 0.16 0.10 0.006 0.39 實施例4 0.08 1.26 0.52 0.51 0.51 0.08 0.17 0.002 0.41 實施例5 0.08 1.22 0.49 0.30 0.32 0.03 0.05 0.002 0.40 比較例1 0.24 0.49 1.27 0.26 0.53 0.02 0.003 0.001 2.59 比較例2 0.07 1.60 0.94 <0.01 <0.01 0.004 0.002 0.002 0.59 比較例3 0.01 0.011 <0.01 <0.01 <0.01 0.002 0.001 0.002 - 比較例4 0.015 0.28 <0.01 <0.01 <0.01 0.002 0.001 0.001 - 比較例5 0.015 0.015 0.28 <0.01 <0.01 0.002 0.001 0.001 18.7 比較例6 0.5 1.24 0.49 0.52 0.53 0.08 0.10 - 0.40 鑄塊係在切斷鑄塊頭後,將兩面各面削2mrn作成厚度 26mm ° 將該鑄塊插入電加熱爐中,以l〇〇°C/hr的升溫速度加熱 至430 C進行430°Cxl小時的均質化處理,再以熱軋延機施 加熱軋延直到成為6mm厚度為止。 對該熱軋延板施加冷軋延而獲得厚度1.25111111的冷軋 板。將該冷軋板插入退火裝置中進行39〇它χΐ小時保持的中 間退火處理後’從退火裝置取出退火板並加以氣冷。接下 來’對該退火板施加冷軋延而獲得厚度1〇mm的冷軋板。 18 201242141 此時的最終冷軋率為20%。 冷軋退火板係未對前述熱軋延板施加中間退火而直接 施加冷軋延獲得1mm的冷軋板。此時的最終冷軋率為83 最終退火係將冷軋板插入退火裝置中進行39〇χ:χ1小時退 火處理後,從退火裝置取出冷軋板並加以氣冷。 接下來,對以上述方法所製得之最終板(各供試材)進行 成形性、及雷射熔接性之評估。 成形性評估 所獲得之最終板的成形性評估係藉由拉伸試驗之延伸 (%)所進行。 具體而言,以拉伸方向平行於軋延方向的方式採取 JIS5號試驗片,再依據JISZ2241進行拉伸試驗,並求算拉伸 強度(UTS)、0.2%耐力(YS)、及延伸(斷裂延伸)。 在冷軋未退火最終板中,視延伸值在2%以上之供試材 為成形性良好(〇),且視低於2%之供試材為成形性不良 (X)。評估結果顯示於表2。 在冷軋後有施加退火的最終板中,視延伸值在20%以 上之供試材為成形性良好(〇),且視低於20%之供試材為成 形性不良(X)。評估結果顯示於表3。 而,表3中之供試材No·係以表1中所示之各供試材No. 加上10的位數之No.表示。 雷射熔接條件 就所獲得之最終板進行脈衝雷射照射,以進行雷射熔 接性評估。使用LUMONICS公司製YAG雷射熔接機JK701, 201242141 在頻率37.5Hz、溶接速度450mm/min、每脈衝之能量6 〇j、 且遮蔽氣體(氮氣)流量l_5(L/min)的條件下,使同供試材的2 片板以端部彼此毫無間隙的方式抵合,並沿著該部分進行 全長120mm長的脈衝雷射熔接。 雷射熔接性之評估異常焊珠數之測定/評估 接下來,就雷射熔接性評估測定產生於熔接部之異常焊 珠數。首先,將上述120mm長的熔接線之中,中央部6〇〇1111長 的熔接線決定為測定區域。再來,如第丨圖顯示,在熔接方向 以〇.〇5mm之間隔連續測定由沿著6〇mm長之炼接線所形成的 脈衝所成之圓升^炼融焊珠之寬度,算出每長(1區間) 之「平均熔接焊珠寬度」後,計數顯示自各區間之「平均熔 接焊珠寬度」偏離比率在1Ux上之焊珠寬度之處的數量。將 "亥叶數合計60mm(6區間)份’作為其供試材之異常焊珠數。 在本說明書中,視異常焊珠數低於1〇的供試材為異常 焊珠數af估良好(〇)’並視異常焊珠數在1()以上的供試材為 異常焊珠數評料⑽)。將冷乾未敎材之評估結果顯示 於表2,並將冷軋退火板之評估結果顯示於表3 ^ 炫入深度之測定/評估 接下來,就雷射熔接性評估測定熔接部中之熔入深 度:如第2圖顯示’切出與熔接方向呈垂直的方向中之板剖 立並將之埋人熱可塑性樹脂中加以鏡面研磨,以進行炫接 邰垂直剖面之金屬組織觀察。 鑄造時所結晶出的介金屬化合物係藉由脈衝雷射照射 ‘、’、而升m到同並熔解於鋁中,其瞬後將熔融焊珠予 20 201242141 以急冷使其成為構成前述介金屬化合物之Fe、Μη、以等元 素過飽和地固溶於AI基質中之組織。 所以藉由炫接部垂直剖面之金屬組織觀察,在該剖面 中只有未觀察到介金屬化合物的A1基質之區域為紐部分, 藉由測疋δ玄區域離最終板表面的最大深度,可測定溶入深度。 就1供試材進行5剖面的熔入深度測定,並將其平均值 作為其供試材中之熔入深度(μιη)。而,此時,在前述異常 焊珠中之剖面為測定對象以外。 在本魂明書中,視熔入深度22〇μιη以上的供試材為熔 入深度評估良好(〇),並視熔入深度低於220μηι的供試材為 熔入深度評估不良(X)。將冷軋未退火材之評估結果顯示於 表2 ’並將冷軋退火板之評估結果顯示於表3。 表2 :供試材的評估結果(冷軋未退火材)Mass ratio of Mn/Fe: on 〇 In the range of Fe and Μη contents within the range of the present invention, if the Mn/Fe ratio is less than 0.2, the penetration depth at the time of laser welding is reduced, which is not preferable. In the range of Fe and Μη contents within the scope of the present invention, if the Mn/Fe ratio exceeds L〇, the number of abnormal beads increases, which is not preferable. In addition, the mass ratio of Mn/Fe affects the type and amount of the intermetallic metal 201242141 compound crystallized during ingot casting. For example, it is known that as the mass ratio of Mn/Fe increases, the amount of 介^Μη intermetallic compound also increases. On the other hand, when the laser is welded, the metal compound such as Α丨όΜη is more likely to evaporate and be unstable than the metallocene compound such as A1 Fe-Si, Alje or AbFe. Therefore, if the Mn/Fe ratio exceeds ?!, 可能, the number of abnormal beads may be increased when the laser is welded, and the weldability may be lowered. Further, Μη is added to the A1 matrix to increase the thermal resistance of the material, and therefore is an element more important than Fe in terms of ensuring the penetration depth at the time of laser welding. Therefore, if the Mn/Fe ratio is lower than 〇.2, the penetration depth at the time of laser welding may be insufficient. Tensile strength and elongation value Cold-rolled unannealed material: elongation value of 2% or more and tensile strength of 160 MPa or more, cold-rolled annealed material: elongation value of 2% or more and tensile strength of 130 MPa or more, and Al-Fe-based aluminum alloy When the board is suitable for large lithium-ion battery containers, etc., it must not only have high strength and good laser fusion, but also good formability. The strength of the material can be known as the tensile strength at the time of the tensile test. Further, the formability can be known from the elongation value at the time of the tensile test. As will be described in detail in the examples to be described later, the Al-Fe-based alloy sheet of the present invention which is suitable for use in large chain ion battery theft, etc., is an extension value of 2% or more when it is cold-rolled unannealed material. It is preferable to have a tensile strength of 16 MPa or more; and a cold rolled annealed material is preferably one having an elongation value of 20% or more and a tensile strength of 130 MPa or more. The number of the second phase particles having a circle equivalent diameter of 5 μm or more in the metal structure is less than 5 〇〇/mm 2 12 201242141 The above characteristics can be erroneously adjusted by carefully adjusting the Al-Fe-based aluminum alloy plate having the specific chemical composition described above. The metal structure appears. Specifically, the number of second phase particles having a circle equivalent diameter of 5 μm or more in the metal structure may be less than 500/mm2. There is no difference in the metal structure whether it is cold rolled unannealed material or cold rolled annealed material. As long as it has the metal structure as described above, the cold-rolled unannealed material exhibits an elongation value of 2% or more and a tensile strength of i60 MPa or more, and the cold-rolled annealed material exhibits an elongation value of 20% or more and a tensile strength of 130 MPa or more. . Next, a method of manufacturing a gold plate for a secondary battery container as described above will be briefly described. Melting and melting ^ Put the raw materials into the melting furnace, and appropriately inject the miscellaneous (four) rows (4) when the predetermined melting temperature is reached, and then wait for the demand to be tempered, then degas after the furnace, and then calmly maintain, and then from the surface of the material. Separate and smash. People recognize that Qiao α takes the topping of the alloy composition, although the mother: from Shaohe 2 raw materials investment is also # important 'But until the above-mentioned agent and refining is extremely: important juice noodles, fully calm when calming time It is advisable to take more than 30 minutes. In order to let the furnace of the furnace, the furnace is moved to the heart of the town (four) for 45 minutes or more. Heart (4) Depending on the demand, it can also be degassed and smashed through the line. Among them, the type in which the inert gas or the like is sprayed into the bubble of the inert gas from the rotary rotor to remove the type is 13 201242141. When nitrogen is used as the inert gas, it is important to manage the dew point to, for example, -60 ° C or less. The amount of hydrogen in the ingot should be reduced to less than 0.20 cc / 100 g. When the amount of hydrogen in the ingot is too large, voids are generated in the final solidified portion of the ingot, and therefore it is necessary to limit the rolling reduction per pass in the hot rolling step to, for example, 7% or more to eliminate voids. Moreover, although it may be different due to the homogenization treatment conditions before the hot rolling step, the hydrogen which is excessively saturated and solid-dissolved in the ingot may be precipitated during the laser welding after the formation of the final sheet, and Most of the pores are produced in the bead. Therefore, the preferred amount of hydrogen in the ingot is 0.15 cc/100 g or less. Cast ingots are manufactured by semi-continuous casting (DC casting). In the usual semi-continuous casting, since the thickness of the ingot is generally about 400 to 600 mm, the solidification cooling rate at the central portion of the ingot is about 1 ° C / sec. Therefore, especially when the high-Fe and Μη content aluminum alloy melt is semi-continuously cast, a coarse intermetallic compound such as Al-(Fe_Mn)-Si is crystallized from the aluminum alloy melt in the center of the ingot. tendency. Although the casting speed in semi-continuous casting varies depending on the width and thickness of the ingot, it is usually considered to be 50 to 70 mm/min in consideration of productivity. However, in the case of in-line degassing, considering the substantial residence time of the melt in the degassing tank, the flow rate of the chain solution (dissolution per unit time) varies depending on the degassing conditions such as the flow rate of the inert gas. The smaller the juice supply amount, the more the degassing efficiency in the tank can be increased and the possibility of reducing the amount of argon gas in the ingot can be achieved. Further, although the number of castings to be cast varies, etc., in order to reduce the amount of hydrogen in the ingot, the casting speed is preferably limited to 30 to 50 mm/min. A more ideal casting speed is 14 201242141 3〇~4〇mm/min. Of course, once the casting speed is lower than 3 〇mm/min, the productivity is lowered, which is not desirable. And, not to mention, the slower the casting speed, the more the slope of the sump (the interface of the solid phase/liquid phase) in the ingot can be relaxed, thereby preventing the casting crack. Homogenization treatment: 42 〇 to 600 ° C x 1 hour or more The ingot obtained by the semi-continuous casting method was subjected to homogenization treatment. The homogenization treatment is a process of holding the ingot at a height of /m to carry out casting segregation or releasing the residual stress inside the prayer piece in order to facilitate the rolling. In the present invention, it is necessary to maintain the temperature at 420 to 60 (TC is maintained for 1 hour or more. At this time, the homogenization treatment is also to dissolve the transitional tl which constitutes the intermetallic compound during casting, to some extent. When the holding temperature is too low or the temperature is kept too short, the solid solution of the above transition element or the like may not proceed, and the recrystallized grain may become coarse, and the DI forming may not be performed beautifully. Further, once the temperature is kept too high, a eutectic portion such as CuMgAl2 which causes a fine final solidification portion in the block is melted, that is, a so-called cast sinter is sintered. The ideal homogenization temperature is 42. 〇~59〇.〇. The hot rolling step is carried out after homogenization treatment of the ingot which has been kept at a high temperature for a predetermined period of time, and is directly lifted by the movable spreader and transferred to the hot rolling mill, and, although, due to the hot emulsion extension machine However, the hot-rolled sheet is rolled up to the pro-thickness by a number of times of aging, and the hot-rolled sheet is rolled to the pro-cold-rolling step. The light of the extension plate passes through the cold rolling mill and usually The number of rows - the cold rolling of a person will be 1 due to the plastic strain induced by cold rolling, and the work hardening will be carried out from 201242141. Therefore, it can be visually kept warm (4) is also soft -===", The furnace is inserted into a cold roll and is maintained at a temperature of 3G (M5()t). The temperature is maintained below -3GGt, which will not promote softening. If the temperature exceeds 4 years, the processing cost will increase. If it is cooled rapidly by a continuous annealing furnace for a temperature of, for example, 45 passages to 55 generations (four times) for 15 seconds, it may also serve as a solution treatment. The temperature is maintained. If it is less than 45 〇c, it will not promote softening. More than 5 qing has the defects that cause the casting sand to be sintered. Final annealing In the present invention, the final annealing after the final cold rolling may also be batch processing, for example, by annealing the furnace to the temperature side ~ 5GGt: for 1 hour. However, if it is kept in a continuous annealing furnace for a period of 15 seconds, for example, the temperature of the thief is kept for 15 seconds, and then rapidly cooled, it may also serve as a coloring treatment. In any case, in the present invention, final annealing is not essential, but If considering the formability in the general DI forming, then In order to soften the final sheet as much as possible, it is preferable to consider the formability of the mold forming (four) towel as the annealed material or the solution treatment material. The mechanical strength is not the formability. In the case of cold rolled unannealed material, the final cold rolling rate at the final cold rolling rate is preferably in the range of 50 to 90%, as long as the final cold rolling rate is within the range, The average recrystallized grain of the final plate is 20~1〇〇μηι and the extension value is set to 20% or more, and then 16 201242141 can be beautifully finished after forming the skin. The ideal final cold rolling rate is 60~90%. On the other hand, the final cold rolling ratio when cold annealing unannealed material is not applied is preferably in the range of 5 to 40%. In the case of DI forming, if the sizing process is increased, it is necessary to provide a final plate which is slightly harder than the annealed material. If the final cold rolling rate is less than 5%, the composition may vary depending on the composition, but it may be difficult to set the tensile strength of the final sheet to 160 MPa or more, and if the final cold rolling ratio exceeds 4%, it may be difficult to The final plate extension is set at 2% or more. As long as the final cold rolling ratio is within this range, the elongation value of the cold rolled unannealed final sheet can be set to 2% or more and the tensile strength can be set to 16 MPa or more. More preferably, the final cold rolling rate is in the range of 1 〇 to 3 〇%. By the above-described general procedure, an aluminum alloy plate for a secondary battery container can be obtained. EXAMPLES Preparation of final sheet After pre-mixing various ingots, various ingots were metered and blended, and each of the ingots (total of 8 test materials) was inserted and filled into a fine load of the coated release material. Will be in violation of (four) into the electric furnace and to. c. Turning the removal of the smelt will keep the scent of the scent of the juice at 76 ° C. Next, remove the smudges and use 6 g of each of the auxiliaries to be placed in the aluminum drop and press in with a stopper. $Next' was inserted into the scented juice and sprayed into the N2 emulsion for 1 minute at a flow rate of l.OL/min for degassing. Then, for 30 minutes. The sedation of the clock, and then the slag of the float on the surface of the melt was removed, and the disc sample was taken into the mold for component analysis. 17 201242141 Come back again, use the jig to remove the crucible from the electric furnace in sequence, and tie the infusion to the preheated mold (250mmx200mmx30mm). The opening of each test material was analyzed by composition analysis by luminescence spectrometry. The results are shown in Table 1. Table 1: Component composition of the test material. Test material No. Component composition (% by mass) Mn/Fe Si Fe Μη Cu Mg Ti Zr B Example 1 0.08 1.28 0.50 0.51 0.51 0.08 0.10 0.005 0.39 Example 2 0.07 1.30 0.31 0.76 0.84 0.08 0.10 0.004 0.24 Example 3 0.07 1.27 0.50 0.51 0.51 0.16 0.10 0.006 0.39 Example 4 0.08 1.26 0.52 0.51 0.51 0.08 0.17 0.002 0.41 Example 5 0.08 1.22 0.49 0.30 0.32 0.03 0.05 0.002 0.40 Comparative Example 1 0.24 0.49 1.27 0.26 0.53 0.02 0.003 0.001 2.59 Comparative Example 2 0.07 1.60 0.94 <0.01 <0.01 0.004 0.002 0.002 0.59 Comparative Example 3 0.01 0.011 <0.01 <0.01 <0.01 0.002 0.001 0.002 - Comparative Example 4 0.015 0.28 <0.01 <0.01 < 0.01 0.002 0.001 0.001 - Comparative Example 5 0.015 0.015 0.28 <0.01 <0.01 0.002 0.001 0.001 18.7 Comparative Example 6 0.5 1.24 0.49 0.52 0.53 0.08 0.10 - 0.40 The ingot was cut into 2 mrn after cutting the ingot head. Thickness 26mm ° The ingot is inserted into an electric heating furnace, heated to 430 C at a heating rate of 10 ° C / hr for homogenization at 430 ° C for 1 hour, and then hot rolling Extension for rolling up until a thickness of 6mm. A cold rolling was applied to the hot rolled sheet to obtain a cold rolled sheet having a thickness of 1.25111111. The cold rolled sheet was inserted into an annealing apparatus and subjected to an intermediate annealing treatment maintained for 39 hours. The annealed sheet was taken out from the annealing apparatus and air-cooled. Next, cold rolling was applied to the annealed sheet to obtain a cold rolled sheet having a thickness of 1 mm. 18 201242141 The final cold rolling rate at this time is 20%. The cold-rolled annealed sheet was subjected to an intermediate annealing without applying an intermediate annealing to the hot rolled sheet to obtain a cold rolled sheet of 1 mm. The final cold rolling ratio at this time was 83. The final annealing system was performed by inserting a cold-rolled sheet into an annealing apparatus for 39 Torr: after an annealing treatment for 1 hour, the cold-rolled sheet was taken out from the annealing apparatus and air-cooled. Next, the final sheet (each test piece) obtained by the above method was evaluated for formability and laser weldability. The evaluation of the formability of the final sheet obtained by the evaluation of the formability was carried out by extension (%) of the tensile test. Specifically, the JIS No. 5 test piece was taken in such a manner that the stretching direction was parallel to the rolling direction, and the tensile test was performed in accordance with JIS Z 2241, and tensile strength (UTS), 0.2% proof stress (YS), and elongation (fracture were calculated). extend). In the cold-rolled unannealed final sheet, the test material having a stretch value of 2% or more was excellent in formability (〇), and the test material having less than 2% was poor in formability (X). The evaluation results are shown in Table 2. In the final sheet to which annealing was applied after cold rolling, the test material having a stretching value of 20% or more was excellent in formability (〇), and the test material having less than 20% was poor in formability (X). The evaluation results are shown in Table 3. In addition, the test material No. in Table 3 is represented by the number of the number of digits of each of the test materials No. shown in Table 1. Laser welding conditions Pulsed laser irradiation was performed on the final plate obtained for laser fusion evaluation. Using the YAG laser welding machine JK701, 201242141 manufactured by LUMONICS, at the frequency of 37.5 Hz, the fusion speed of 450 mm/min, the energy per pulse of 6 〇j, and the shielding gas (nitrogen) flow rate l_5 (L/min), The two sheets of the test piece were joined in such a manner that the ends were free of each other, and a pulsed laser welding of a total length of 120 mm was performed along the portion. Evaluation of Laser Weldability Measurement/Evaluation of Abnormal Beads Next, the number of abnormal beads generated in the welded portion was measured in terms of laser weldability evaluation. First, among the above-mentioned 120 mm long weld lines, the weld line of the center portion 6 1111 is determined as the measurement area. Further, as shown in the figure, the width of the round-up welding bead formed by the pulse formed along the 6 mm long wire is continuously measured at intervals of 〇.〇5 mm in the welding direction, and each is calculated. After the "average weld bead width" of the long (1 section), the count shows the number of "average weld bead width" deviation ratios in each section at the bead width of 1 Ux. The total number of "Holidays is 60 mm (6 intervals) is taken as the number of abnormal beads of the test material. In this specification, the number of abnormal weld beads is less than 1〇, and the number of abnormal weld beads is a good (〇)', and the number of abnormal weld beads is 1 () or more. Review (10)). The evaluation results of the cold-dried untwisted materials are shown in Table 2, and the evaluation results of the cold-rolled annealed sheets are shown in Table 3. ^ Measurement/Evaluation of the Dying Intensity Next, the melting in the welded portion is determined by the laser fusion evaluation. Into the depth: As shown in Fig. 2, the plate in the direction perpendicular to the welding direction is cut and embedded in the thermoplastic resin to be mirror-polished to observe the metal structure of the vertical cross section. The mesometallic compound crystallized during casting is irradiated with ',' by pulsed laser, and is increased to m and melted in aluminum. Immediately afterwards, the molten bead is fused to 20 201242141 to be quenched to form the aforementioned intermetallic metal. Fe, Μη of the compound, a structure which is solid-solubilized in an AI matrix by supersaturation of an element. Therefore, by observing the metal structure of the vertical section of the splicing portion, only the region of the A1 matrix in which the intermetallic compound is not observed is a new portion in the cross section, and the maximum depth of the 疋 玄 区域 region from the final plate surface can be determined. Dissolution depth. The melting depth of the five sections was measured for the test piece, and the average value was taken as the penetration depth (μιη) in the test piece. In this case, the cross section in the abnormal bead is outside the measurement target. In this Soul book, the test material with a melt penetration depth of 22 〇μηη is well evaluated for the penetration depth (〇), and the test material with a melt penetration depth lower than 220 μη is the poor evaluation of the penetration depth (X). . The evaluation results of the cold-rolled unannealed materials are shown in Table 2' and the evaluation results of the cold-rolled annealed sheets are shown in Table 3. Table 2: Evaluation results of the test materials (cold rolled unannealed materials)
供試材 No. 異常焊珠數 熔入深度 拉伸特性 異常 焊珠 溶入 成形性 (¾伸) 4kW (μηι) UTS (MPa) YS (MPa) 延伸 (%) 實施例1 6 249 214 213 3 〇 〇 〇 實施例2 7 371 225 219 4 〇 〇 〇 實施例3 6 253 219 217 3 〇 〇 〇 實施例4 6 " —— 283 236 235 2 〇 〇 〇 實施例5 1 229 198 190 5 〇 〇 〇 比較例1 19 276 226 217 3 X 〇 〇 比較例2 13 355 140 136 <1 X 〇 X 比較例3 0 185 68 67 8 〇 X 〇 比較例4 0 199 91 89 16 〇 X 〇 比較例5 0 179 85 85 6 〇 X 〇 比較例6 2 251 224 222 <1 〇 〇 X 表3 :供試材的評估結果(冷軋退火材) 21 201242141Test material No. Abnormal weld bead number Melting depth Tensile property Abnormal weld bead melt formability (3⁄4 extension) 4kW (μηι) UTS (MPa) YS (MPa) Extension (%) Example 1 6 249 214 213 3 〇〇〇Example 2 7 371 225 219 4 〇〇〇 Example 3 6 253 219 217 3 〇〇〇 Example 4 6 " —— 283 236 235 2 〇〇〇 Example 5 1 229 198 190 5 〇〇 〇Comparative Example 1 19 276 226 217 3 X 〇〇Comparative Example 2 13 355 140 136 <1 X 〇X Comparative Example 3 0 185 68 67 8 〇X 〇Comparative Example 4 0 199 91 89 16 〇X 〇Comparative Example 5 0 179 85 85 6 〇X 〇Comparative Example 6 2 251 224 222 <1 〇〇X Table 3: Evaluation results of the test materials (cold rolled annealed materials) 21 201242141
供試材 No. 異常焊珠數 熔入深度 拉伸特性 異常 焊珠 溶入 成形性 (延伸) 4kW (μηι) UTS (MPa) YS (MPa) 延伸 (%) 實施例11 1 228 165 90 28 〇 〇 〇 實施例12 8 352 185 123 1 21 〇 〇 〇 實施例13 7 241 167 91 25 〇 〇 〇 實施例14 5 234 166 89 26 〇 〇 〇 實施例15 0 222 135 80 29 〇 〇 〇 比較例11 20 261 160 100 25 X 〇 〇 比較例12 11 340 168 90 17 X 〇 X 比較例13 0 196 67 29 45 〇 X 〇 比較例14 0 205 70 30 43 〇 X 〇 比較例15 0 208 75 41 38 〇 X 〇 比較例16 1 238 170 92 19 〇 〇 X 各供試材之評估 顯示有關冷軋未退火材之評估結果的表2中,實施例 1〜5為本發明之組成範圍内的冷軋材’雷射熔接性(異常焊 珠數评估、〜深度評估)、及成形性皆良好(〇)。 P匕平乂狀1J 1干 Μη含量高為1.27質量%且Mn/Fe比亦 2.59在本發明範11外,雖然以深度評估良好(〇)且成用 良好(〇) ’但異常焊珠數評估不良(X)。 比車乂例2中,Fe含量高為16質量%在本發明範圍 好(〇),但成雜不⑽)且異#焊珠 比較例3〜5Φ,Ayf u 甲Fe、Mn皆低,在本發明範圍外’勒 估^Γ0)且異常焊珠數評估良好(〇)’但溶, 22 201242141 比較例6中,Si4旦二达 然炫入深度評估k W為G.5fM%在本發明範圍外,雖 形性不良(I。义(0)且異常焊珠數評估良好(〇),但成 .“·頁示有闕冷軋退火奸 11〜15ΑϋΒΒ 之评估蛣果的表3尹,實施例 焊珠袁1、 之組成乾15 _退讀,雷射熔接性(異常 數料、以深度評估)、及成形㈣良好(〇)。 ,車父例11中,_含量高為127質量%且麟批亦為 • f本發明範圍外,雖然溶入深度評估良好(〇)且成形性 良子(〇)’但異常焊珠數評估不良(x)。 比較例12中, 雖然熔入深度評估 數評估不良(x)。Test material No. Abnormal weld bead number Melting depth Tensile property Abnormal weld bead melt formability (extension) 4kW (μηι) UTS (MPa) YS (MPa) Extension (%) Example 11 1 228 165 90 28 〇 〇〇Example 12 8 352 185 123 1 21 〇〇〇Example 13 7 241 167 91 25 〇〇〇Example 14 5 234 166 89 26 〇〇〇Example 15 0 222 135 80 29 〇〇〇Comparative Example 11 20 261 160 100 25 X 〇〇Comparative Example 12 11 340 168 90 17 X 〇X Comparative Example 13 0 196 67 29 45 〇X 〇Comparative Example 14 0 205 70 30 43 〇X 〇Comparative Example 15 0 208 75 41 38 〇 X 〇 Comparative Example 16 1 238 170 92 19 〇〇X Evaluation of each test material shows that in Table 2 regarding the evaluation results of the cold-rolled unannealed material, Examples 1 to 5 are cold-rolled materials within the composition range of the present invention. 'The laser fusion properties (abnormal weld bead number evaluation, ~ depth evaluation), and formability are good (〇). The P 匕 flat 1 1J 1 dry Μ η content is 1.27% by mass and the Mn/Fe ratio is also 2.59 outside the scope of the present invention, although the depth is well evaluated (〇) and used well (〇) 'but the number of abnormal beads Poor assessment (X). In the case of the vehicle example 2, the Fe content is as high as 16% by mass in the range of the present invention (,), but the impurity is not (10)) and the different beads are compared with the examples 3 to 5, and the Ayf u is low in Fe and Mn. Outside the scope of the present invention, the evaluation of the number of abnormal beads is good (〇)' but dissolves, 22 201242141 In Comparative Example 6, the Si4 denier dadden into depth evaluation k W is G.5fM% in the present invention. Outside the range, although the shape is poor (I. Yi (0) and the number of abnormal weld beads is well evaluated (〇), but the ".· page shows the results of the evaluation of the results of the evaluation of the results of the cold rolling and annealing of 11~15ΑϋΒΒ, Example Weld Bead Yuan 1, the composition of the dry 15 _ readback, laser fusion (abnormal material, to depth evaluation), and forming (four) good (〇). In the car father example 11, the _ content is 127 quality % and the batch is also outside the scope of the present invention, although the evaluation of the penetration depth is good (〇) and the formability is good (〇), but the abnormal number of beads is poorly evaluated (x). In Comparative Example 12, although the penetration depth is The evaluation number is poorly evaluated (x).
Fe含量尚為丨6質量0/。在本發明範圍外, 良好(〇)’但成形性不良(χ)且異常烊珠 匕較例13〜15中,Fe、Μη皆低,在本發明範圍外雖 然成形性良好(〇)且異常焊珠數評估良好(Ο),但炫入深度 評估不良(X)。 匕較例16中’ Si含1向為〇_5質量。/β在本發明範圍外, 雖然溶入深度評估良好(〇江異常焊珠數評估良好(〇),但 成形性不良(X)。 金屬組織中之第2相粒子數測定 將與所獲得之最終板之軋延方向呈平行的縱剖面(與 LT方向呈垂直的剖面)予以切出紐人熱可塑性樹脂中加 以鏡面研磨’再進行金屬_齡。以光學賴鏡照相拍 攝微金屬組織(母1視野之面積:〇 Q334mm2、各試料拍攝1〇 視野)並進行相片之圖像解析’以測定每單位面積之圓等效 23 201242141 徑長5μηι以上的第2相粒子數。 表4 :第2相/粒+卖欠(單位:個/_2)(冷軋未退火材) 將冷乳未退火材之圖像解析之測定結果顯示於表4,並 將冷軋退火板之圖像解析之測定結果顯示於表5。 供試材No. ---~~~-1 圓等效徑長5μηι以上 實施例1 201 實施例2 ---------J 173 實施例3 401 實施例4 259 比較例1 398 比較例2 1007 比較例3 0 比較例4 0 比較例5 0 比較例6 —-------- 614 表5 .第2相粒子數(單位:個/mm2)(冷軋退火材) 供試材No. 圓等效徑長5μιη以上 實施例11 152 實施例12 182 ~~ 實施例13 380 實施例14 276 比較例11 413 比較例12 965 比較例13 ------- 1 比較例14 0 比較例15 — 一 0 比較例16 553 從顯示有關冷軋未退火材之評估結果的表4可知,在金 24 201242141 屬組織中之圓等效徑長5μπι以上之第2相粒子數在5〇〇個 /mm2以上的情況下(比較例2、6),在拉伸試驗中,在較粗 的第2相粒子與基質之界面中容易產生剝離,因此延伸值會 變低到低於2%。 所以,可知,為了使延伸值在2°/。以上,必須使金屬組 織中之圓等效徑長5μιη以上的第2相粒子數低於5〇〇個 /mm2 ° 從顯示有關冷軋退火材之評估結果的表5可知,在金屬 組織中之圓等效徑長5 μ m以上之第2相粒子數在5 〇 〇個/m阳2 以上的情況下(比較例12、16),在拉伸試驗中,在較粗的第 2相粒子與基質之界面料產生_,所崎伸值會變低到 低於20%。 所以’可知’為了使延伸值在2〇%以上,必須使金屬 組織中之圓等效徑長5μηι以上的第2相粒子數低於5〇〇個 /mm2。 產業上之可利用性 依據本發明,可提供具有可適用於大型鍾離子電池容 器的高強度,且成雜優異、雷_接性紐賴如系銘 合金板。 【圖式簡單說明j 第1圖係說明異常焊珠數七収/評財法的概念圖, ⑷為熔接焊枉俯·’灿)轴科料珠長度方向之 焊珠寬度變化的圖表。 第2圖係說明炫入深度之測定/評估方法的概念圖,㈧ 25 201242141 為熔接焊珠之俯視圖,及(B)為剖面圖。 【主要元件符號說明】 (無) 26The Fe content is still 丨6 mass 0/. In addition to the scope of the present invention, it is good (〇), but the moldability is poor (χ) and the abnormal ruthenium ruthenium is lower than Fe and Μη in Examples 13 to 15, and the formability is good (〇) and abnormal outside the scope of the present invention. The number of beads was well evaluated (Ο), but the depth of the smear was poorly evaluated (X). In Comparative Example 16, 'Si contains 1 direction as 〇_5 mass. /β is outside the scope of the present invention, although the evaluation of the depth of dissolution is good (the evaluation of the number of abnormal beads in the Minjiang River is good (〇), but the formability is poor (X). The number of particles in the second phase of the metal structure is determined and obtained. The longitudinal direction of the final sheet is parallel to the longitudinal section (a section perpendicular to the LT direction), which is cut into the thermoplastic resin of the New Zealand for mirror polishing, and then metal-aged. Photomicrographs are taken by optical photographic mirrors. 1 area of the field of view: 〇Q334mm2, 1 〇 field of view for each sample) and image analysis of the photo 'to determine the number of particles of the second phase equivalent to 23 201242141 diameter 5μηι or more per unit area. Table 4: 2 Phase/grain + sale (unit: one / _2) (cold rolled unannealed material) The measurement results of the image analysis of the cold unannealed material are shown in Table 4, and the image analysis of the cold rolled annealed sheet is determined. The results are shown in Table 5. Test material No. ---~~~-1 Circle equivalent diameter 5 μηι or more Example 1 201 Example 2 ---------J 173 Example 3 401 Example 4 259 Comparative Example 1 398 Comparative Example 2 1007 Comparative Example 3 0 Comparative Example 4 0 Comparative Example 5 0 Comparative Example 6-- ------- 614 Table 5. Number of second phase particles (unit: piece / mm2) (cold rolled annealed material) Test material No. Round equivalent diameter 5 μmη or more Example 11 152 Example 12 182 ~ ~ Example 13 380 Example 14 276 Comparative Example 11 413 Comparative Example 12 965 Comparative Example 13 ------- 1 Comparative Example 14 0 Comparative Example 15 - A 0 Comparative Example 16 553 From showing related cold-rolled unannealed materials Table 4 of the evaluation results shows that in the case where the number of the second phase particles having a circle equivalent diameter of 5 μm or more in the genus of gold 24 201242141 is 5 〇〇/mm 2 or more (Comparative Examples 2 and 6), In the tensile test, peeling is likely to occur at the interface between the coarser second phase particles and the substrate, so that the elongation value is lowered to less than 2%. Therefore, it is understood that in order to make the elongation value 2°/. or more, it is necessary to make The number of second phase particles having a circle equivalent diameter of 5 μm or more in the metal structure is less than 5 〇〇/mm 2 ° From the table 5 showing the evaluation results of the cold rolled annealed material, the circular equivalent diameter in the metal structure is known. When the number of second phase particles having a length of 5 μm or more is 5 〇〇/m cation 2 or more (Comparative Examples 12 and 16), in the tensile test, The interface between the coarse second phase particles and the matrix produces _, and the value of the extension will become lower than 20%. Therefore, 'it is known that in order to make the extension value above 2%, the circle in the metal structure must be equivalent. The number of second phase particles having a diameter of 5 μm or more is less than 5 Å/mm 2 . INDUSTRIAL APPLICABILITY According to the present invention, it is possible to provide a high strength which is applicable to a large-sized ion battery container, and is excellent in impurities. _ 接接纽赖如如铭合金板. [Simple diagram of the drawing, Fig. 1 is a conceptual diagram showing the number of abnormally welded beads, and the evaluation of the width of the bead in the longitudinal direction of the welding bead. Fig. 2 is a conceptual diagram illustrating the measurement/evaluation method of the glazing depth, (8) 25 201242141 is a plan view of the welded bead, and (B) is a sectional view. [Main component symbol description] (none) 26
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