US20020012811A1 - Method of manufacturing an aluminum product - Google Patents
Method of manufacturing an aluminum product Download PDFInfo
- Publication number
- US20020012811A1 US20020012811A1 US09/849,238 US84923801A US2002012811A1 US 20020012811 A1 US20020012811 A1 US 20020012811A1 US 84923801 A US84923801 A US 84923801A US 2002012811 A1 US2002012811 A1 US 2002012811A1
- Authority
- US
- United States
- Prior art keywords
- range
- nickel
- alloy
- ion concentration
- bismuth
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 73
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 49
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 124
- 238000007747 plating Methods 0.000 claims abstract description 62
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 58
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 56
- 238000000034 method Methods 0.000 claims abstract description 55
- 229910052797 bismuth Inorganic materials 0.000 claims abstract description 22
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims abstract description 20
- 229910052751 metal Inorganic materials 0.000 claims abstract description 16
- 239000002184 metal Substances 0.000 claims abstract description 16
- 229910001451 bismuth ion Inorganic materials 0.000 claims abstract description 10
- 229910001453 nickel ion Inorganic materials 0.000 claims abstract description 10
- 238000005219 brazing Methods 0.000 claims description 80
- 229910045601 alloy Inorganic materials 0.000 claims description 31
- 239000000956 alloy Substances 0.000 claims description 31
- 229910052710 silicon Inorganic materials 0.000 claims description 8
- 239000010703 silicon Substances 0.000 claims description 8
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 claims description 7
- 229910000416 bismuth oxide Inorganic materials 0.000 claims description 7
- 238000001816 cooling Methods 0.000 claims description 7
- TYIXMATWDRGMPF-UHFFFAOYSA-N dibismuth;oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[Bi+3].[Bi+3] TYIXMATWDRGMPF-UHFFFAOYSA-N 0.000 claims description 7
- RGHNJXZEOKUKBD-SQOUGZDYSA-M D-gluconate Chemical compound OC[C@@H](O)[C@@H](O)[C@H](O)[C@@H](O)C([O-])=O RGHNJXZEOKUKBD-SQOUGZDYSA-M 0.000 claims description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 6
- 229940036348 bismuth carbonate Drugs 0.000 claims description 6
- GMZOPRQQINFLPQ-UHFFFAOYSA-H dibismuth;tricarbonate Chemical compound [Bi+3].[Bi+3].[O-]C([O-])=O.[O-]C([O-])=O.[O-]C([O-])=O GMZOPRQQINFLPQ-UHFFFAOYSA-H 0.000 claims description 6
- 239000000945 filler Substances 0.000 claims description 6
- 229910001220 stainless steel Inorganic materials 0.000 claims description 6
- 239000010935 stainless steel Substances 0.000 claims description 6
- 239000010936 titanium Substances 0.000 claims description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 5
- LGQLOGILCSXPEA-UHFFFAOYSA-L nickel sulfate Chemical compound [Ni+2].[O-]S([O-])(=O)=O LGQLOGILCSXPEA-UHFFFAOYSA-L 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- 239000011701 zinc Substances 0.000 claims description 5
- AEQDJSLRWYMAQI-UHFFFAOYSA-N 2,3,9,10-tetramethoxy-6,8,13,13a-tetrahydro-5H-isoquinolino[2,1-b]isoquinoline Chemical compound C1CN2CC(C(=C(OC)C=C3)OC)=C3CC2C2=C1C=C(OC)C(OC)=C2 AEQDJSLRWYMAQI-UHFFFAOYSA-N 0.000 claims description 4
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 claims description 4
- KRKNYBCHXYNGOX-UHFFFAOYSA-K Citrate Chemical compound [O-]C(=O)CC(O)(CC([O-])=O)C([O-])=O KRKNYBCHXYNGOX-UHFFFAOYSA-K 0.000 claims description 4
- 238000005275 alloying Methods 0.000 claims description 4
- 150000003839 salts Chemical class 0.000 claims description 4
- 239000001509 sodium citrate Substances 0.000 claims description 4
- NLJMYIDDQXHKNR-UHFFFAOYSA-K sodium citrate Chemical compound O.O.[Na+].[Na+].[Na+].[O-]C(=O)CC(O)(CC([O-])=O)C([O-])=O NLJMYIDDQXHKNR-UHFFFAOYSA-K 0.000 claims description 4
- 239000000176 sodium gluconate Substances 0.000 claims description 4
- 229940005574 sodium gluconate Drugs 0.000 claims description 4
- 235000012207 sodium gluconate Nutrition 0.000 claims description 4
- 229910000680 Aluminized steel Inorganic materials 0.000 claims description 3
- 229910001369 Brass Inorganic materials 0.000 claims description 3
- 229910000906 Bronze Inorganic materials 0.000 claims description 3
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- BFNBIHQBYMNNAN-UHFFFAOYSA-N ammonium sulfate Chemical compound N.N.OS(O)(=O)=O BFNBIHQBYMNNAN-UHFFFAOYSA-N 0.000 claims description 3
- 229910052921 ammonium sulfate Inorganic materials 0.000 claims description 3
- 239000001166 ammonium sulphate Substances 0.000 claims description 3
- 235000011130 ammonium sulphate Nutrition 0.000 claims description 3
- JHXKRIRFYBPWGE-UHFFFAOYSA-K bismuth chloride Chemical compound Cl[Bi](Cl)Cl JHXKRIRFYBPWGE-UHFFFAOYSA-K 0.000 claims description 3
- 239000010951 brass Substances 0.000 claims description 3
- 239000010974 bronze Substances 0.000 claims description 3
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 3
- 229910001000 nickel titanium Inorganic materials 0.000 claims description 3
- 238000007493 shaping process Methods 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- KKMOSYLWYLMHAL-UHFFFAOYSA-N 2-bromo-6-nitroaniline Chemical compound NC1=C(Br)C=CC=C1[N+]([O-])=O KKMOSYLWYLMHAL-UHFFFAOYSA-N 0.000 claims description 2
- 238000004070 electrodeposition Methods 0.000 claims description 2
- 230000008018 melting Effects 0.000 claims description 2
- 238000002844 melting Methods 0.000 claims description 2
- 238000003892 spreading Methods 0.000 claims description 2
- 230000007480 spreading Effects 0.000 claims description 2
- 238000004090 dissolution Methods 0.000 claims 1
- 238000009713 electroplating Methods 0.000 abstract description 6
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 15
- 239000000463 material Substances 0.000 description 11
- 230000004907 flux Effects 0.000 description 9
- 230000008569 process Effects 0.000 description 9
- 239000003517 fume Substances 0.000 description 8
- 229910021529 ammonia Inorganic materials 0.000 description 7
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 6
- 238000004140 cleaning Methods 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 229910021586 Nickel(II) chloride Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000005253 cladding Methods 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 238000000151 deposition Methods 0.000 description 4
- QMMRZOWCJAIUJA-UHFFFAOYSA-L nickel dichloride Chemical compound Cl[Ni]Cl QMMRZOWCJAIUJA-UHFFFAOYSA-L 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 238000004381 surface treatment Methods 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 230000000712 assembly Effects 0.000 description 3
- 239000012141 concentrate Substances 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 238000005530 etching Methods 0.000 description 3
- 238000007654 immersion Methods 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 238000002203 pretreatment Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 239000011856 silicon-based particle Substances 0.000 description 3
- 239000010802 sludge Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- VHUUQVKOLVNVRT-UHFFFAOYSA-N Ammonium hydroxide Chemical compound [NH4+].[OH-] VHUUQVKOLVNVRT-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- FEWJPZIEWOKRBE-JCYAYHJZSA-N Dextrotartaric acid Chemical compound OC(=O)[C@H](O)[C@@H](O)C(O)=O FEWJPZIEWOKRBE-JCYAYHJZSA-N 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- KFZMGEQAYNKOFK-UHFFFAOYSA-N Isopropanol Chemical compound CC(C)O KFZMGEQAYNKOFK-UHFFFAOYSA-N 0.000 description 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 2
- 239000000908 ammonium hydroxide Substances 0.000 description 2
- 235000011114 ammonium hydroxide Nutrition 0.000 description 2
- 229940043379 ammonium hydroxide Drugs 0.000 description 2
- 150000001622 bismuth compounds Chemical class 0.000 description 2
- WMWLMWRWZQELOS-UHFFFAOYSA-N bismuth(iii) oxide Chemical compound O=[Bi]O[Bi]=O WMWLMWRWZQELOS-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 238000010924 continuous production Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229940046892 lead acetate Drugs 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910017604 nitric acid Inorganic materials 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 229940095064 tartrate Drugs 0.000 description 2
- NWONKYPBYAMBJT-UHFFFAOYSA-L zinc sulfate Chemical compound [Zn+2].[O-]S([O-])(=O)=O NWONKYPBYAMBJT-UHFFFAOYSA-L 0.000 description 2
- QYIGOGBGVKONDY-UHFFFAOYSA-N 1-(2-bromo-5-chlorophenyl)-3-methylpyrazole Chemical compound N1=C(C)C=CN1C1=CC(Cl)=CC=C1Br QYIGOGBGVKONDY-UHFFFAOYSA-N 0.000 description 1
- MIMUSZHMZBJBPO-UHFFFAOYSA-N 6-methoxy-8-nitroquinoline Chemical compound N1=CC=CC2=CC(OC)=CC([N+]([O-])=O)=C21 MIMUSZHMZBJBPO-UHFFFAOYSA-N 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 1
- 229910001152 Bi alloy Inorganic materials 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- VEQPNABPJHWNSG-UHFFFAOYSA-N Nickel(2+) Chemical compound [Ni+2] VEQPNABPJHWNSG-UHFFFAOYSA-N 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- MQRWBMAEBQOWAF-UHFFFAOYSA-N acetic acid;nickel Chemical compound [Ni].CC(O)=O.CC(O)=O MQRWBMAEBQOWAF-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000002378 acidificating effect Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000012190 activator Substances 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 239000012670 alkaline solution Substances 0.000 description 1
- 229940077464 ammonium ion Drugs 0.000 description 1
- 150000003863 ammonium salts Chemical class 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- KHTPCDDBDQRIRX-UHFFFAOYSA-N azane;hydrate Chemical compound N.[NH4+].[OH-] KHTPCDDBDQRIRX-UHFFFAOYSA-N 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 239000013527 degreasing agent Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000003599 detergent Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000000839 emulsion Substances 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- HEPLMSKRHVKCAQ-UHFFFAOYSA-N lead nickel Chemical compound [Ni].[Pb] HEPLMSKRHVKCAQ-UHFFFAOYSA-N 0.000 description 1
- 238000009996 mechanical pre-treatment Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 150000002815 nickel Chemical class 0.000 description 1
- 229940078494 nickel acetate Drugs 0.000 description 1
- KERTUBUCQCSNJU-UHFFFAOYSA-L nickel(2+);disulfamate Chemical compound [Ni+2].NS([O-])(=O)=O.NS([O-])(=O)=O KERTUBUCQCSNJU-UHFFFAOYSA-L 0.000 description 1
- 229910000363 nickel(II) sulfate Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 238000005240 physical vapour deposition Methods 0.000 description 1
- 235000021110 pickles Nutrition 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- SKFYTVYMYJCRET-UHFFFAOYSA-J potassium;tetrafluoroalumanuide Chemical compound [F-].[F-].[F-].[F-].[Al+3].[K+] SKFYTVYMYJCRET-UHFFFAOYSA-J 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000009718 spray deposition Methods 0.000 description 1
- 229940071182 stannate Drugs 0.000 description 1
- 125000005402 stannate group Chemical group 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 239000001117 sulphuric acid Substances 0.000 description 1
- 235000011149 sulphuric acid Nutrition 0.000 description 1
- 238000002230 thermal chemical vapour deposition Methods 0.000 description 1
- 238000007751 thermal spraying Methods 0.000 description 1
- 239000012808 vapor phase Substances 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/56—Electroplating: Baths therefor from solutions of alloys
- C25D3/562—Electroplating: Baths therefor from solutions of alloys containing more than 50% by weight of iron or nickel or cobalt
-
- 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
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0233—Sheets, foils
- B23K35/0238—Sheets, foils layered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/017—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of aluminium or an aluminium alloy, another layer being formed of an alloy based on a non ferrous metal other than aluminium
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/42—Pretreatment of metallic surfaces to be electroplated of light metals
- C25D5/44—Aluminium
-
- 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
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/28—Selection of soldering or welding materials proper with the principal constituent melting at less than 950 degrees C
- B23K35/286—Al as the principal constituent
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
- E04C2002/3411—Dimpled spacer sheets
- E04C2002/3433—Dimpled spacer sheets with dimples extending from both sides of the spacer sheet
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
- E04C2002/3444—Corrugated sheets
- E04C2002/3455—Corrugated sheets with trapezoidal corrugations
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
- E04C2002/3444—Corrugated sheets
- E04C2002/3466—Corrugated sheets with sinusoidal corrugations
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/3405—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets
- E04C2002/3472—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by profiled spacer sheets with multiple layers of profiled spacer sheets
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/934—Electrical process
- Y10S428/935—Electroplating
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/12764—Next to Al-base component
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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12785—Group IIB metal-base component
- Y10T428/12792—Zn-base component
Definitions
- the invention relates to a method of manufacturing an Al or Al alloy workpiece, such as a brazing sheet product, comprising the steps of providing an Al or Al alloy workpiece, pre-treating of the outersurface of the Al or Al alloy workpiece, and plating a metal layer comprising nickel onto the outersurface of the pre-treated workpiece.
- the invention also relates to a brazed assembly comprising at least one component made of the workpiece obtained by the method of this invention.
- the invention further relates to an aqueous plating bath for use in the method of this invention.
- brazing sheet is to be understood as a core sheet, for example of aluminum or aluminum alloy, having on at least one side a brazeable aluminum alloy.
- Typical brazeable aluminum alloys useful as a clad layer are the Aluminum Association (AA) 4xxx-series alloys, typically having Si in the range of 2 to 18 weight %, and preferably in the range of 7 to 14%.
- the brazeable aluminum alloys may be coupled to the core alloy in various ways known in the art, for example by means of roll bonding, cladding, spray-forming or semi-continuous or continuous casting.
- Controlled Atmosphere Brazing (“CAB”) and Vacuum Brazing (“VB”) are the two main processes used for industrial scale aluminum brazing.
- Industrial vacuum brazing has been used since the 1950's, while CAB became popular in the early 1980's after the introduction of the Nocolok (trade mark) brazing flux.
- Vacuum brazing is an essentially discontinuous process and puts high demands on material cleanliness. The disruption of the oxide layer present is mainly caused by the evaporation of magnesium from the clad alloy. There is always more magnesium present in the furnace then necessary. The excess magnesium condenses on the cold spots in the furnace and has to be removed frequently. The capital investment for suitable equipment is relatively high.
- CAB requires an additional process step prior to brazing as compared to VB, since a brazing flux has to be applied prior to brazing.
- CAB is essentially a continuous process in which, if the proper brazing flux is being used, high volumes of brazed assemblies can be manufactured.
- the brazing flux dissolves the oxide layer at brazing temperature allowing the clad alloy to flow properly.
- the Nocolok flux is used the surface needs to be cleaned thoroughly prior to flux application.
- the brazing flux has to be applied on the total surface of the brazed assembly. This can cause difficulties with certain types of assemblies because of their design. For example, because evaporator type heat exchangers have a large internal surface, problems can arise because of poor access to the interior.
- the flux has to adhere to the aluminum surface before brazing.
- the brazing flux after drying can easily fall off due to small mechanical vibrations.
- corrosive fumes such as HF are generated. This puts a high demand on the corrosion resistance of the materials applied for the furnace.
- a material should be available that can be used for CAB but does not have the requirements and defects of the brazing flux application.
- Such a material can be supplied to a manufacturer of brazed assemblies and is ready to use directly after forming of the assembly parts. No additional brazing fluxing operations have to be carried out.
- the material for this process can be for example standard brazing sheet made from an AA3xxx-series core alloy clad on both sides with a cladding of an AA4xxx-series alloy. Before the brazing sheet can be used the surface has to be modified in such a way that the naturally occurring oxide layer does not interfere during the brazing cycle.
- the method of achieving good brazing is to deposit a specific amount of nickel on the surface of the aluminum clad alloy. If properly applied, the nickel reacts with the underlying aluminum.
- the nickel can be applied by using a shim of nickel between the two parts to be joined or can be deposited by electroplating. When electroplating is used the adherence of the nickel should be sufficient to withstand typical shaping operations being used in for example heat exchanger manufacture.
- the clad alloy should contain a relatively large number of silicon particles to act as nuclei for the nickel deposition. It is believed that to obtain sufficient nucleation sites before pickling a part of the aluminum in which the silicon particles are embedded should be removed by chemical and/or mechanical pre-treatment. This is believed a necessary condition to obtain a sufficient nickel coverage to serve as nuclei for the plating action of the brazing or clad alloy. On a microscopic scale the surface of the Si-containing cladding of the brazing sheet is covered with nickel globules.
- the use of lead for the production of a suitable nickel and/or cobalt layer on brazing sheet has several disadvantages.
- the plating baths for electroplating are rather complex and due to the presence of lead comprising components such as salts thereof, these baths are much more environmentally unfriendly than plating baths comprising nickel- or cobalt-components alone.
- the use of lead for manufacturing products, such as automotive products is undesirable and it is envisaged that in the very near future there might possibly even be a ban on lead comprising products or products manufactured via one or more intermediate processing steps comprising lead or lead-based components.
- a further disadvantage of the plating bath described in U.S. Pat. No. 4,028,200 is the considerable generation of ammonia fumes on the workshop floor due to the use of significant amounts of ammonia in the plating bath used.
- It is another object of the present invention to provide a method of manufacturing a brazing sheet product comprising the steps of (a) providing a sheet comprising a core sheet coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, (b) pre-treating of the outersurface of the aluminum clad layer, and (c) plating a metal layer comprising nickel onto the outersurface of the pre-treated aluminum clad layer, by which method a brazing sheet product is obtained having good brazeability without the mandatory addition of lead to the nickel-layer.
- a method of manufacturing an aluminum or aluminum alloy workpiece comprising the sequential steps of (a) providing an Al or Al alloy workpiece, (b) pre-treating of the outersurface of the aluminum workpiece, and (c) plating a metal layer comprising nickel onto said outersurface of the pre-treated aluminum or aluminum alloy workpiece.
- This method is characterized in that during step (c) said layer comprising nickel being deposited by plating both nickel and bismuth using an aqueous bath having:
- [0015] comprising a nickel-ion concentration in a range of 10 to 100 g/l, and preferably in a range of 20 to 70 g/l,
- a bismuth-ion concentration in the range of 0.01 to 10 g/l, and preferably in the range of 0.02 to 5 g/l,
- a citrate-ion concentration in the range of 40 to 150 g/l, and preferably in the range of 80 to 110 g/l,
- a gluconate-ion concentration in the range of 2 to 80 g/l, and preferably in the range of 4 to 50 g/l,
- a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l, and preferably in the range of 1 to 30 g/l.
- the nickel layer does not need to comprise any lead as a mandatory alloying addition in order to achieve good brazeability when using the aluminum workpiece in a brazing operation.
- bismuth is added to the nickel layer, such that said nickel layer can be kept essentially lead-free and simultaneously also in the plating bath used for the deposition of this Ni—Bi layer.
- This aqueous plating bath demonstrated to be operational in a very wide pH range, and can be used on industrial scale coil plating lines using a high current density, which in turn allows for fairly high line speeds. Further advantages of this plating bath are that it does not generate any ammonia fumes, it can be composed using standard and readily available chemicals, and bismuth can easily be replenished to the plating bath from a bismuth concentrate or otherwise.
- said layer comprising nickel being deposited by plating both nickel and bismuth using an aqueous bath comprising a nickel-ion concentration in a range of 20 to 70 g/l and a bismuth-ion concentration in the range of 0.02 to 5 g/l.
- the nickel-ion concentration to the aqueous bath can be added via the addition of nickel chloride, nickel fluoborate, nickel sulfamate, nickel acetate or nickel suplhate.
- nickel sulfate NiSO 4 .6H 2 O.
- Bi-ion in the concentration set out above can be added in various ways to the aqueous bath.
- many bismuth compounds could be used for this purpose.
- many bismuth compounds have been tried out but only a very few appear to provide reliable and reproducible results.
- the addition of bismuth acetate has been tried, but it has been found that this compound did not dissolve in the plating bath used, whereas the addition of lead acetate did not result in any problems with respect to having this compound dissolved.
- the combination of a bath of nickel-ions and bismuth-ions and a tartrate at a pH in the range of more than 8 resulted in the formation of an undesirable Ni containing sludge.
- the resultant deposit has a undesired high Bi-concentration.
- the Bi-concentration in the resultant Ni—Bi layer on the brazing sheet product is not more than 5 percent by weight, and preferably not more than 3 percent by weight. At too low levels the resultant bath becomes uneconomical due to too long plating times and low current density.
- the layer comprising nickel and bismuth has a thickness up to 2.0 ⁇ m, preferably in the range of 0.03 to 1.0 ⁇ m, and more preferably in the range of 0.05 to 0.5 ⁇ m.
- a coating thickness of greater than 2.0 ⁇ m requires a prolonged treatment time for plating, and may result in wrinkling of the molten filler material during subsequent brazing operations.
- a preferred thickness for this Ni—Bi containing layer is 0.3 ⁇ m.
- other techniques such as roll bonding, thermal spraying, Chemical Vapor Deposition and Physical Vapor Deposition or other techniques for depositing of metal or metal alloys from a gas or vapor phase may be used.
- Nickel sulphate in a range of 45 to 450 g/l, and preferably 90 to 315 g/l
- Chloride-ion concentration in a range of 1 to 50 g/l, and preferably 1 to 30 g/l,
- Bismuth oxide in a range of 0.02 to 22 g/l, and preferably 0.05 to 11 g/l, or Bismuth carbonate in a range of 0.03 to 29 g/l, and preferably 0.06 to 14 g/l.
- an ion from the group consisting of chloride and fluoride is required for inducing anode corrosion.
- a suitable source of chloride-ion concentration can be done by the addition of nickel chloride (NiCl 2 .6H 2 O) in a range of up to 415 g/l, and preferably in a range up to 250 g/l.
- (H+) or (OH—) can be added to regulate the pH in a range of 2.5 to 10.
- the use of ammonium hydroxide should preferably be avoided in view of the generation of ammonia fumes.
- an ammonium-ion concentration in a range up to 40 g/l, and preferably in range of 1 to 25 g/l, or a triethenalamine-ion concentration in a range of up to 40 g/l, or combinations thereof, or other equivalent components may be added to the aqueous bath.
- Any soluble ammonium salt can be used as a source of NH 4 + .
- the plating bath used in the method according to the invention can operate in a wide pH range of 2.5 to 10, and preferably in the range of 4 to 8, without affecting the properties of the bath and without dissolving the aluminum clad layer or any other metal layer thereon.
- the aluminum workpiece such as a brazing sheet product having an aluminum clad layer
- the pH is preferably in the range of 5 to 8, and more preferably in the range of 5.4 to 7.5.
- the layer has a thickness up to 0.5 ⁇ m, more preferably up to 0.3 ⁇ m (300 nm), and most preferably in the range of 0.01 to 0.15 ⁇ m (10-150 nm). In the best results obtained a thickness of about 30 nm has been used.
- a coating thickness of greater than 0.5 ⁇ m requires a prolonged treatment time, e.g. for displacement plating, and is thought to have no further advantages for improving the adhesion.
- zinc instead of zinc also tin may be used.
- the method according to the invention is preferably employed using a plating bath having a temperature in the rang of 30 to 70° C., and more preferably in the range of 40 to 65° C. In this temperature range the ion-mobility increases and there is no need to cool the plating bath to compensate for the heat generation during plating.
- the invention further relates to an aqueous bath for the electro-deposition of a layer comprising both nickel and bismuth on a brazing sheet product having:
- [0040] comprising a nickel-ion concentration in the range of 10 to 100 g/l, and preferably in a range of 20 to 70 g/l,
- a bismuth-ion concentration in the range of 0.01 to 10 g/l, and preferably in a range of 0.02 to 5 g/l,
- a citrate-ion concentration in the range of 50 to 150 g/l, and preferably in a range of 80 to 110 g/l,
- a gluconate-ion concentration in the range of 2 to 80 g/l, and preferably in a range of 4 to 50 g/l,
- a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l, and preferably in a range of 1 to 30 g/l.
- This aqueous plating bath demonstrated to be operational in a very wide pH range, and at a wide temperature range, and further can be used on industrial scale coil plating lines using a high current density, which in turn allows for fairly high line speeds. Further advantages of this plating bath are that it does not generate any ammonia fumes, it can be composed used standard and readily available chemicals, and the bismuth concentration can easily be replenished to the plating bath from a bismuth concentrate or otherwise.
- the adhesion of the layer comprising both nickel and bismuth to the aluminum workpiece, such as the cladding of a brazing sheet product is fairly good, but may be further improved by a proper pre-treatment of the outersurface of the aluminum workpiece on which the Ni—Bi layer is being deposited, such as the clad layer of a brazing sheet product.
- the pre-treatment comprises a preliminary cleaning step during which the surface is made free from grease, oil, or buffing compounds. This can be accomplished in many ways, and can be accomplished amongst others by vapor degreasing, solvent washing, or solvent emulsion cleaning. Also a mild etching may be employed. Following the preliminary cleaning, the surface should preferably be conditioned.
- nitric acid typically 25-50%
- a fluoride and/or chromic acid and/or sulphuric acid optionally in combination with a fluoride and/or chromic acid and/or sulphuric acid.
- Suitable sources for the fluoride can be, for example, hydrofluoric acid or ammonium bifluoride, see also e.g. “The surface treatment and finishing of aluminum and its alloys”, by S. Wernick et al., ASM international, 5th edition, 1987, Vol.1, pp.181-182.
- the Al or Al alloy workpiece is an aluminum alloy sheet or aluminum alloy wire or aluminum alloy rod.
- various aluminum alloys may be applied, e.g. those within the Aluminum Association (AA)3xxx- and AA6xxx-series aluminum alloys.
- Particular suitable aluminum alloys are those within the AA4xxx-series alloys, typically having Si as the most important alloying element in the range of 2 to 18% by weight, more preferably 7 to 14% by weight.
- Other alloying elements may be present to improve specific properties, the balance is made by iron up to 0.8%, and impurities each up to 0.05 wt. %, total up to 0.20 wt. %, and aluminum.
- An AA4xxx-series aluminum alloy sheet can be plated with Ni—Bi alloy in accordance with the method of the invention, and may be employed in subsequent brazing operations, in particular in an inert atmosphere brazing (CAB) operation in the absence of a brazing-flux material.
- aluminum alloy wire or rods being made of an AA4xxx-series alloy may be plated with a Ni—Bi layer, and subsequently employed in brazing operations in particular in an inert atmosphere brazing (CAB) operations in the absence of a brazing-flux material, and may also be employed as weld filler wire or weld filler rod in a welding operation.
- the aluminum alloy workpiece is a brazing sheet product comprising a core sheet coupled at least one surface of said core sheet to n aluminum clad layer, the aluminum clad layer being made of an aluminum AA4xxx-series alloy comprising silicon in the range of 2 to 18% by weight, preferably in the range of 7 to 14%.
- the core sheet is made of an aluminum alloy, in particular those within the AA3xxx, AA5xxx, or AA6xxx-series alloys.
- the invention further provides a brazed assembly comprising at least one component made of the aluminum alloy workpiece, in particular a brazing sheet product, obtained by the method in accordance with the invention described above.
- a brazing sheet product Preferably the resultant brazing sheet product has a Ni—Bi layer comprising Bi, by weight percent, in a range of up to 5%, preferably not more than 3%, and more preferably up to 1.0%, and most preferably in a range of 0.01 to 0.05%.
- a brazed assembly wherein at least one of the parts to be joined by brazing is made of the aluminum alloy workpiece, in particular a brazing sheet product, produced by the method in accordance with the invention described above, and at least one other part is made of steel, aluminized steel, stainless steel, plated or coated stainless steel, bronze, brass, nickel, nickel alloy, titanium, or plated or coated titanium.
- cooling the brazed assembly to below 100° C.
- the cooling rate may be in the range of typical brazing furnace cooling rates.
- Typical cooling rates are cooling rates of at least 10° C./min or more.
- the process may include the further processing step (e) of aging of the brazed and cooled assembly in order to optimize the mechanical and/or corrosion properties of the resultant assembly.
- the use of the brazing sheet product obtained from the method according to the invention set out above has been found to result in a lower brazing temperature by at least 10° C. This reduced brazing temperature allows a significant reduction of the industrial scale processing time of a complete brazing cycle, typically a time reduction of 15% or more has been found.
- At least one of the parts to be joined by brazing is made of the brazing sheet product produced by the method in accordance with the invention described above, and at least one other part is made of steel, aluminized steel, stainless steel, plated or coated stainless steel, bronze, brass, nickel, nickel alloy, titanium, or plated or coated titanium.
- the nickel plating bath used has the composition of Table 1 and having a pH of 5.5.
- the Bi-ion concentration has been added to the plating bath using a Bi-ion concentrate of 160 g/l sodium hydroxide, 300 g/l sodium gluconate and 110 g/l bismuth oxide.
- the bismuth oxide could have been replaced also by bismuth carbonate.
- the electroplating of a Ni—Bi layer was performed at 57° C. using three different current densities and plating times.
- the composition of the resultant layer was measured using ICP and is given in Table 2.
- ICP stands for Induced Coupled Plasma. The results given are for the sum of both plated sides.
- Similar brazing sheet material has been Ni-plated with Ni—Pb.
- the plating bath comprised 50 g/l nickel sulphate, 50 g/l nickel chloride, 100 g/l/sodium citrate, 1 g/l lead acetate, and 75 ml/l ammonium hydroxide (30%).
- the plating conditions at 26° C. were such that a plating time of 200s resulted in a nickel-lead plated layer of 2.0 microns using a current density of 3 A/dm 2 . Due to the presence of ammonium-hydroxide ammonia fumes are being generated.
- the strip-on-the-coupon samples were heated under flowing nitrogen, with heating from room temperature to 580° C., dwell time at 580° C. for 1 minute, cooling from 580° C. to room temperature.
- the brazing process was judged on possible formation of wrinkles, capillary depression and fillet formation.
- the results obtained are summarized in Table 2.
- This example shows how an electroplated nickel layer containing Bi, but comprising no Pb, may be applied and resulting in a product having at least a fair adhesion of the nickel layer and excellent brazeability. Normally bismuth is not easily maintained in a stable nickel-plating solution without sludge formation.
- Ni—Bi plating operations according to the invention may be applied also on one or both sides of an aluminum alloy sheet or strip made of an AA4xxx-series aluminum alloys, which aluminum alloy sheet is not being provided with a core sheet to form a brazing sheet product.
- a Ni—Bi plated sheet or strip typically having a gauge in the range of up to 3 mm, preferably in the range of 0.05 to 2 mm, may be employed also in a brazing operation as set out in this example.
- a similar approach can be used for plating aluminum alloy wires or rods.
- Such Ni—Bi plated wires or rods may be employed in a brazing operation as set out in this example or used as filler material in a welding operation, such as for laser welding operations.
- This plating bath has many advantages compared to the standard known Pb-containing baths:
- more practical operating temperatures typically 40 to 70° C.
- bismuth can easily be replenished to the plating bath.
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Abstract
The invention relates to a method of manufacturing an Al or Al alloy workpiece, including the steps of (a) providing an Al or Al alloy workpiece, (b) pre-treating of the outersurface of the Al or Al alloy workpiece, and (c) plating a metal layer including nickel onto the outersurface of the pre-treated Al or Al alloy workpiece. During step (c) the metal layer including nickel is deposited by electroplating both nickel and bismuth using an aqueous bath comprising a nickel-ion concentration in a range of 10 to 100 g/l and a bismuth-ion concentration in the range of 0.01 to 10 g/l. The invention further relates to an aqueous plating bath for use in the method of this invention.
Description
- This is a continuation-in-part of U.S. patent application Ser. No. 09/573,980, filed May 19, 2000, now pending, incorporated herein by reference in its entirety.
- The invention relates to a method of manufacturing an Al or Al alloy workpiece, such as a brazing sheet product, comprising the steps of providing an Al or Al alloy workpiece, pre-treating of the outersurface of the Al or Al alloy workpiece, and plating a metal layer comprising nickel onto the outersurface of the pre-treated workpiece. The invention also relates to a brazed assembly comprising at least one component made of the workpiece obtained by the method of this invention. The invention further relates to an aqueous plating bath for use in the method of this invention.
- For the purpose of this invention brazing sheet is to be understood as a core sheet, for example of aluminum or aluminum alloy, having on at least one side a brazeable aluminum alloy. Typical brazeable aluminum alloys useful as a clad layer are the Aluminum Association (AA) 4xxx-series alloys, typically having Si in the range of 2 to 18 weight %, and preferably in the range of 7 to 14%. The brazeable aluminum alloys may be coupled to the core alloy in various ways known in the art, for example by means of roll bonding, cladding, spray-forming or semi-continuous or continuous casting.
- Controlled Atmosphere Brazing (“CAB”) and Vacuum Brazing (“VB”) are the two main processes used for industrial scale aluminum brazing. Industrial vacuum brazing has been used since the 1950's, while CAB became popular in the early 1980's after the introduction of the Nocolok (trade mark) brazing flux. Vacuum brazing is an essentially discontinuous process and puts high demands on material cleanliness. The disruption of the oxide layer present is mainly caused by the evaporation of magnesium from the clad alloy. There is always more magnesium present in the furnace then necessary. The excess magnesium condenses on the cold spots in the furnace and has to be removed frequently. The capital investment for suitable equipment is relatively high.
- CAB requires an additional process step prior to brazing as compared to VB, since a brazing flux has to be applied prior to brazing. CAB is essentially a continuous process in which, if the proper brazing flux is being used, high volumes of brazed assemblies can be manufactured. The brazing flux dissolves the oxide layer at brazing temperature allowing the clad alloy to flow properly. When the Nocolok flux is used the surface needs to be cleaned thoroughly prior to flux application. To obtain good brazing results the brazing flux has to be applied on the total surface of the brazed assembly. This can cause difficulties with certain types of assemblies because of their design. For example, because evaporator type heat exchangers have a large internal surface, problems can arise because of poor access to the interior. For good brazing results the flux has to adhere to the aluminum surface before brazing. Unfortunately the brazing flux after drying can easily fall off due to small mechanical vibrations. During the brazing cycle, corrosive fumes such as HF are generated. This puts a high demand on the corrosion resistance of the materials applied for the furnace.
- Ideally, a material should be available that can be used for CAB but does not have the requirements and defects of the brazing flux application. Such a material can be supplied to a manufacturer of brazed assemblies and is ready to use directly after forming of the assembly parts. No additional brazing fluxing operations have to be carried out. Presently, only one process for flux-less brazing is used on an industrial scale. The material for this process can be for example standard brazing sheet made from an AA3xxx-series core alloy clad on both sides with a cladding of an AA4xxx-series alloy. Before the brazing sheet can be used the surface has to be modified in such a way that the naturally occurring oxide layer does not interfere during the brazing cycle. The method of achieving good brazing is to deposit a specific amount of nickel on the surface of the aluminum clad alloy. If properly applied, the nickel reacts with the underlying aluminum. The nickel can be applied by using a shim of nickel between the two parts to be joined or can be deposited by electroplating. When electroplating is used the adherence of the nickel should be sufficient to withstand typical shaping operations being used in for example heat exchanger manufacture.
- The processes for nickel-plating in an alkaline solution of aluminum brazing sheet are known from each of U.S. Pat. No. 3,970,237, U.S. Pat. No. 4,028,200, U.S. Pat. No. 4,164,454, and SAE-paper no. 880446 by B. E. Cheadle and K. F. Dockus. According to these documents, nickel or cobalt, or combinations thereof, are most preferably deposited in combination with lead. The lead addition is used to improve the wettability of the clad alloy during the brazing cycle. An important characteristic of these plating processes is that the nickel is preferentially deposited on the silicon particles of the clad alloy. To obtain sufficient nickel for brazing on the surface, the clad alloy should contain a relatively large number of silicon particles to act as nuclei for the nickel deposition. It is believed that to obtain sufficient nucleation sites before pickling a part of the aluminum in which the silicon particles are embedded should be removed by chemical and/or mechanical pre-treatment. This is believed a necessary condition to obtain a sufficient nickel coverage to serve as nuclei for the plating action of the brazing or clad alloy. On a microscopic scale the surface of the Si-containing cladding of the brazing sheet is covered with nickel globules.
- However, the use of lead for the production of a suitable nickel and/or cobalt layer on brazing sheet has several disadvantages. The plating baths for electroplating are rather complex and due to the presence of lead comprising components such as salts thereof, these baths are much more environmentally unfriendly than plating baths comprising nickel- or cobalt-components alone. The use of lead for manufacturing products, such as automotive products, is undesirable and it is envisaged that in the very near future there might possibly even be a ban on lead comprising products or products manufactured via one or more intermediate processing steps comprising lead or lead-based components. A further disadvantage of the plating bath described in U.S. Pat. No. 4,028,200 is the considerable generation of ammonia fumes on the workshop floor due to the use of significant amounts of ammonia in the plating bath used.
- It is an object of the present invention to provide a method of manufacturing an Al or Al alloy workpiece, comprising the steps of providing an Al or Al alloy workpiece, pretreating of the outersurface of the Al or Al alloy workpiece, and plating a metal layer comprising nickel onto the outersurface of the pre-treated Al or Al alloy workpiece, by which method a product is obtained having good brazeability and/or weldability without the mandatory addition of lead to the nickel-layer.
- It is another object of the present invention to provide a method of manufacturing a brazing sheet product comprising the steps of (a) providing a sheet comprising a core sheet coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, (b) pre-treating of the outersurface of the aluminum clad layer, and (c) plating a metal layer comprising nickel onto the outersurface of the pre-treated aluminum clad layer, by which method a brazing sheet product is obtained having good brazeability without the mandatory addition of lead to the nickel-layer.
- It is a further object of the present invention to provide a method of manufacturing an Al or Al alloy workpiece, ideally a brazing sheet product, the method comprising the steps of (a) providing an Al or Al alloy workpiece, in particular a brazing sheet comprising a core sheet coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy containing silicon in an amount in the range of 2 to 18% by weight, (b) pre-treating of the outersurface of the Al workpiece, in particular the aluminum clad layer, and (c) plating a metal layer comprising nickel onto the outersurface of the pre-treated workpiece, in particular of the pre-treated aluminum clad layer, by which method there is no generation of ammonia fumes originating from the plating bath when operated on an industrial scale.
- It is also an object of the invention to provide an aqueous plating bath for use in the method according to the invention and which can be employed in an industrial environment.
- In accordance with the invention in one aspect there is provided a method of manufacturing an aluminum or aluminum alloy workpiece, the method comprising the sequential steps of (a) providing an Al or Al alloy workpiece, (b) pre-treating of the outersurface of the aluminum workpiece, and (c) plating a metal layer comprising nickel onto said outersurface of the pre-treated aluminum or aluminum alloy workpiece. This method is characterized in that during step (c) said layer comprising nickel being deposited by plating both nickel and bismuth using an aqueous bath having:
- a pH in the range of 2.5 to 10, and
- comprising a nickel-ion concentration in a range of 10 to 100 g/l, and preferably in a range of 20 to 70 g/l,
- a bismuth-ion concentration in the range of 0.01 to 10 g/l, and preferably in the range of 0.02 to 5 g/l,
- a citrate-ion concentration in the range of 40 to 150 g/l, and preferably in the range of 80 to 110 g/l,
- a gluconate-ion concentration in the range of 2 to 80 g/l, and preferably in the range of 4 to 50 g/l,
- a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l, and preferably in the range of 1 to 30 g/l.
- In accordance with the invention it has been found surprisingly that the nickel layer does not need to comprise any lead as a mandatory alloying addition in order to achieve good brazeability when using the aluminum workpiece in a brazing operation. Surprisingly it has been found that equal or even better results can be obtained if bismuth is added to the nickel layer, such that said nickel layer can be kept essentially lead-free and simultaneously also in the plating bath used for the deposition of this Ni—Bi layer. By using this aqueous plating bath the need for the addition of lead has been overcome, which is a significant achievement from an enviromental point of view.
- This aqueous plating bath demonstrated to be operational in a very wide pH range, and can be used on industrial scale coil plating lines using a high current density, which in turn allows for fairly high line speeds. Further advantages of this plating bath are that it does not generate any ammonia fumes, it can be composed using standard and readily available chemicals, and bismuth can easily be replenished to the plating bath from a bismuth concentrate or otherwise.
- Preferably said layer comprising nickel being deposited by plating both nickel and bismuth using an aqueous bath comprising a nickel-ion concentration in a range of 20 to 70 g/l and a bismuth-ion concentration in the range of 0.02 to 5 g/l.
- The nickel-ion concentration to the aqueous bath can be added via the addition of nickel chloride, nickel fluoborate, nickel sulfamate, nickel acetate or nickel suplhate. However, there is a preference to use the addition of nickel sulfate (NiSO4.6H2O). At a too high level of nickel salt in the aqueous bath there is the risk of the crystallization of the salt in the solution, which might damage a continuous process. At too low levels the resultant bath becomes uneconomical due to too long plating times and low current density.
- Bi-ion in the concentration set out above can be added in various ways to the aqueous bath. In theory many bismuth compounds could be used for this purpose. However, many bismuth compounds have been tried out but only a very few appear to provide reliable and reproducible results. For example the addition of bismuth acetate has been tried, but it has been found that this compound did not dissolve in the plating bath used, whereas the addition of lead acetate did not result in any problems with respect to having this compound dissolved. For example also the combination of a bath of nickel-ions and bismuth-ions and a tartrate at a pH in the range of more than 8 resulted in the formation of an undesirable Ni containing sludge. This Ni containing sludge did not re-dissolve upon heating, indicating amongst others that Ni is unstable in the presence of a tartrate in the mentioned pH range. In accordance with the invention very good results have been obtained when Bi-ions are being added via the addition of one or more of the group consisting of bismuth carbonate ( Bi2(CO3)3 ), bismuth oxide ( Bi2O3 ), bismuth citrate (BiC6H5O7) and bismuth chloride (BiCl3 ). Optionally some sodium hydroxide may be added also to regulate the pH of the aqueous bath. By using bismuth carbonate or bismuth oxide in the presence of nickel a suitable plating bath has been obtained which is stable at a very wide pH range. At too high levels of Bi-ion concentration in the aqueous bath the resultant deposit has a undesired high Bi-concentration. Preferably the Bi-concentration in the resultant Ni—Bi layer on the brazing sheet product is not more than 5 percent by weight, and preferably not more than 3 percent by weight. At too low levels the resultant bath becomes uneconomical due to too long plating times and low current density.
- Preferably in the workpiece, in particular a brazing sheet product, the layer comprising nickel and bismuth has a thickness up to 2.0 μm, preferably in the range of 0.03 to 1.0 μm, and more preferably in the range of 0.05 to 0.5 μm. A coating thickness of greater than 2.0 μm requires a prolonged treatment time for plating, and may result in wrinkling of the molten filler material during subsequent brazing operations. A preferred thickness for this Ni—Bi containing layer is 0.3 μm. Also other techniques such as roll bonding, thermal spraying, Chemical Vapor Deposition and Physical Vapor Deposition or other techniques for depositing of metal or metal alloys from a gas or vapor phase may be used.
- Baths using the following salts have proved particularly effective, in grams per liter:
- Nickel sulphate in a range of 45 to 450 g/l, and preferably 90 to 315 g/l,
- Chloride-ion concentration in a range of 1 to 50 g/l, and preferably 1 to 30 g/l,
- Sodium citrate in a range of 55 to 180 g/l, and preferably 110 to 150 g/l,
- Sodium gluconate in range of 2 to 90 g/l, and preferably 5 to 55 g/l,
- Ammonium sulphate in a range up to 270 g/l,
- Bismuth oxide in a range of 0.02 to 22 g/l, and preferably 0.05 to 11 g/l, or Bismuth carbonate in a range of 0.03 to 29 g/l, and preferably 0.06 to 14 g/l.
- The addition of an ion from the group consisting of chloride and fluoride is required for inducing anode corrosion. A suitable source of chloride-ion concentration can be done by the addition of nickel chloride (NiCl2.6H2O) in a range of up to 415 g/l, and preferably in a range up to 250 g/l.
- (H+) or (OH—) can be added to regulate the pH in a range of 2.5 to 10. The use of ammonium hydroxide should preferably be avoided in view of the generation of ammonia fumes.
- Optionally for reducing stress in the deposit layer comprising the Ni and Bi an ammonium-ion concentration in a range up to 40 g/l, and preferably in range of 1 to 25 g/l, or a triethenalamine-ion concentration in a range of up to 40 g/l, or combinations thereof, or other equivalent components may be added to the aqueous bath. Any soluble ammonium salt can be used as a source of NH4 +.
- The plating bath used in the method according to the invention can operate in a wide pH range of 2.5 to 10, and preferably in the range of 4 to 8, without affecting the properties of the bath and without dissolving the aluminum clad layer or any other metal layer thereon. If the aluminum workpiece, such as a brazing sheet product having an aluminum clad layer, is provided with a thin intermediate zinc layer, e.g. by means of a zincate treatment via direct or immersion plating, prior to the plating of the Ni—Bi layer, the pH is preferably in the range of 5 to 8, and more preferably in the range of 5.4 to 7.5. In the embodiment of an applied intermediate layer comprising zinc, the layer has a thickness up to 0.5 μm, more preferably up to 0.3 μm (300 nm), and most preferably in the range of 0.01 to 0.15 μm (10-150 nm). In the best results obtained a thickness of about 30 nm has been used. A coating thickness of greater than 0.5 μm requires a prolonged treatment time, e.g. for displacement plating, and is thought to have no further advantages for improving the adhesion. Instead of zinc also tin may be used.
- The method according to the invention is preferably employed using a plating bath having a temperature in the rang of 30 to 70° C., and more preferably in the range of 40 to 65° C. In this temperature range the ion-mobility increases and there is no need to cool the plating bath to compensate for the heat generation during plating.
- The invention further relates to an aqueous bath for the electro-deposition of a layer comprising both nickel and bismuth on a brazing sheet product having:
- a pH in the range of 2.5 to 10, and
- comprising a nickel-ion concentration in the range of 10 to 100 g/l, and preferably in a range of 20 to 70 g/l,
- a bismuth-ion concentration in the range of 0.01 to 10 g/l, and preferably in a range of 0.02 to 5 g/l,
- a citrate-ion concentration in the range of 50 to 150 g/l, and preferably in a range of 80 to 110 g/l,
- a gluconate-ion concentration in the range of 2 to 80 g/l, and preferably in a range of 4 to 50 g/l,
- a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l, and preferably in a range of 1 to 30 g/l. This aqueous plating bath demonstrated to be operational in a very wide pH range, and at a wide temperature range, and further can be used on industrial scale coil plating lines using a high current density, which in turn allows for fairly high line speeds. Further advantages of this plating bath are that it does not generate any ammonia fumes, it can be composed used standard and readily available chemicals, and the bismuth concentration can easily be replenished to the plating bath from a bismuth concentrate or otherwise.
- The adhesion of the layer comprising both nickel and bismuth to the aluminum workpiece, such as the cladding of a brazing sheet product, is fairly good, but may be further improved by a proper pre-treatment of the outersurface of the aluminum workpiece on which the Ni—Bi layer is being deposited, such as the clad layer of a brazing sheet product. The pre-treatment comprises a preliminary cleaning step during which the surface is made free from grease, oil, or buffing compounds. This can be accomplished in many ways, and can be accomplished amongst others by vapor degreasing, solvent washing, or solvent emulsion cleaning. Also a mild etching may be employed. Following the preliminary cleaning, the surface should preferably be conditioned. Several methods can be applied successfully, such as, but not limited thereto:
- (a) acid desmutting in an solution comprising nitric acid (typically 25-50%), optionally in combination with a fluoride and/or chromic acid and/or sulphuric acid. Suitable sources for the fluoride can be, for example, hydrofluoric acid or ammonium bifluoride, see also e.g. “The surface treatment and finishing of aluminum and its alloys”, by S. Wernick et al., ASM international, 5th edition, 1987, Vol.1, pp.181-182.
- (b) mechanical preparation such as polishing, abrasion or brushing. These may also be applied while the surface is in contact with a lower alcohol, such as for example isopropanol, see e.g. also U.S. Pat. No. 4,388,159.
- (c) alkaline etching, see e.g. “The surface treatment and finishing of aluminum and its alloys”, by S. Wernick et al., ASM international, 5th edition, 1987, Vol.1, pp.191-203.
- (d) aqueous detergent cleaning;
- (e) anodic oxidation, see e.g. “The surface treatment and finishing of aluminum and its alloys”, by S. Wernick et al., ASM International, 5th edition, 1987, Vol.2, pp.1006 ff.
- (f) electrograining.
- (g) pre-treatments described in for example U.S. Pat. No. 4,741,811, U.S. Pat. No. 5,245,847, U.S. Pat. No. 5,643,434.
- (h) immersion processes such as zincate and stannate, see “The surface treatment and finishing of aluminum and its alloys”, by S. Wernick et al., ASM international, 5th edition, 1987, Vol.2, Chapter 14 and 15.
- Also combinations of one or more conditioning steps set out above can be applied successfully.
- In an embodiment the Al or Al alloy workpiece is an aluminum alloy sheet or aluminum alloy wire or aluminum alloy rod. Although various aluminum alloys may be applied, e.g. those within the Aluminum Association (AA)3xxx- and AA6xxx-series aluminum alloys. Particular suitable aluminum alloys are those within the AA4xxx-series alloys, typically having Si as the most important alloying element in the range of 2 to 18% by weight, more preferably 7 to 14% by weight. Other alloying elements may be present to improve specific properties, the balance is made by iron up to 0.8%, and impurities each up to 0.05 wt. %, total up to 0.20 wt. %, and aluminum. An AA4xxx-series aluminum alloy sheet can be plated with Ni—Bi alloy in accordance with the method of the invention, and may be employed in subsequent brazing operations, in particular in an inert atmosphere brazing (CAB) operation in the absence of a brazing-flux material. Also aluminum alloy wire or rods being made of an AA4xxx-series alloy may be plated with a Ni—Bi layer, and subsequently employed in brazing operations in particular in an inert atmosphere brazing (CAB) operations in the absence of a brazing-flux material, and may also be employed as weld filler wire or weld filler rod in a welding operation.
- In a preferred embodiment the aluminum alloy workpiece is a brazing sheet product comprising a core sheet coupled at least one surface of said core sheet to n aluminum clad layer, the aluminum clad layer being made of an aluminum AA4xxx-series alloy comprising silicon in the range of 2 to 18% by weight, preferably in the range of 7 to 14%. In an embodiment of the aluminum brazing sheet product, the core sheet is made of an aluminum alloy, in particular those within the AA3xxx, AA5xxx, or AA6xxx-series alloys.
- The invention further provides a brazed assembly comprising at least one component made of the aluminum alloy workpiece, in particular a brazing sheet product, obtained by the method in accordance with the invention described above. Preferably the resultant brazing sheet product has a Ni—Bi layer comprising Bi, by weight percent, in a range of up to 5%, preferably not more than 3%, and more preferably up to 1.0%, and most preferably in a range of 0.01 to 0.05%.
- In an embodiment there is provided a brazed assembly wherein at least one of the parts to be joined by brazing is made of the aluminum alloy workpiece, in particular a brazing sheet product, produced by the method in accordance with the invention described above, and at least one other part is made of steel, aluminized steel, stainless steel, plated or coated stainless steel, bronze, brass, nickel, nickel alloy, titanium, or plated or coated titanium.
- In a further aspect of the invention there is provided in a method of manufacturing a brazed assembly using the aluminum alloy workpiece, in particular a brazing sheet product, produced by the method in accordance with this invention, comprising the steps of:
- (a) shaping or forming parts of which at least one is made from the aluminum alloy workpiece, ideally a brazing sheet product, obtained by the method in accordance with this invention as set out above;
- (b) assembling the parts into the assembly;
- (c) brazing the assembly under a vacuum or in an inert atmosphere (CAB) in the absence of a brazing-flux at elevated temperature for a period long enough for melting and spreading of the molten filler alloy;
- (d) cooling the brazed assembly to below 100° C. The cooling rate may be in the range of typical brazing furnace cooling rates. Typical cooling rates are cooling rates of at least 10° C./min or more.
- In dependence on the material, particularly aluminum alloy, of the cores sheet the process may include the further processing step (e) of aging of the brazed and cooled assembly in order to optimize the mechanical and/or corrosion properties of the resultant assembly. The use of the brazing sheet product obtained from the method according to the invention set out above has been found to result in a lower brazing temperature by at least 10° C. This reduced brazing temperature allows a significant reduction of the industrial scale processing time of a complete brazing cycle, typically a time reduction of 15% or more has been found.
- In an embodiment of the method of manufacturing a brazed assembly in step (a) at least one of the parts to be joined by brazing is made of the brazing sheet product produced by the method in accordance with the invention described above, and at least one other part is made of steel, aluminized steel, stainless steel, plated or coated stainless steel, bronze, brass, nickel, nickel alloy, titanium, or plated or coated titanium.
- On a laboratory scale of testing aluminum brazing sheets manufactured from an AA3003 core alloy clad on both sides with an AA4045 clad alloy, and having a total thickness of 0.5 mm and a clad layer thickness of 50 microns each, was treated using the following sequential process steps:
- cleaning by immersion for 180 sec. in ChemTec 30014 (a commercial available alkaline (etch) degreaser), followed by rinsing;
- alkaline etching for 20 sec. in ChemTec 30203 (a commercial available alkaline etch cleaner) at ambient temperature, followed by rinsing;
- desmutting for 4 sec. in an acidic oxidizing bath, typically 25-50 vol. % nitric acid, comprising ChemTec 11093 (a commercial available pickle activator) at ambient temperature, followed by rinsing;
- nickel electroplating, and rinsing.
- The nickel plating bath used has the composition of Table 1 and having a pH of 5.5. The Bi-ion concentration has been added to the plating bath using a Bi-ion concentrate of 160 g/l sodium hydroxide, 300 g/l sodium gluconate and 110 g/l bismuth oxide. The bismuth oxide could have been replaced also by bismuth carbonate. The electroplating of a Ni—Bi layer was performed at 57° C. using three different current densities and plating times. The composition of the resultant layer was measured using ICP and is given in Table 2. ICP stands for Induced Coupled Plasma. The results given are for the sum of both plated sides. For comparison similar brazing sheet material has been Ni-plated with Ni—Pb. The plating bath comprised 50 g/l nickel sulphate, 50 g/l nickel chloride, 100 g/l/sodium citrate, 1 g/l lead acetate, and 75 ml/l ammonium hydroxide (30%). The plating conditions at 26° C. were such that a plating time of 200s resulted in a nickel-lead plated layer of 2.0 microns using a current density of 3 A/dm2. Due to the presence of ammonium-hydroxide ammonia fumes are being generated.
- The nickel plated specimens have been tested for adhesion using the Erichsen dome test (5 mm), and the T-bend test. A value assessment is then given to the adhesion where: (−)=poor, (±)=fair, and (+)=good. The results are given in Table 2. Further the brazeability has been assessed. On a laboratory scale of testing the brazing tests were carried out in a small quartz furnace. Small coupons of 25 mm×25 mm were cut from the nickel-plated sheets. A small strip of an AA3003 alloy measuring 30 mm×7 mm×1 mm was bent in the center to an angle of 45° and laid on the coupons. The strip-on-the-coupon samples were heated under flowing nitrogen, with heating from room temperature to 580° C., dwell time at 580° C. for 1 minute, cooling from 580° C. to room temperature. The brazing process was judged on possible formation of wrinkles, capillary depression and fillet formation. An overall assessment was given where: (−)=poor brazeability, (−/±)=fair brazeability, (±)=good brazeability, and (+)=excellent brazeability. The results obtained are summarized in Table 2.
- This example shows how an electroplated nickel layer containing Bi, but comprising no Pb, may be applied and resulting in a product having at least a fair adhesion of the nickel layer and excellent brazeability. Normally bismuth is not easily maintained in a stable nickel-plating solution without sludge formation.
- It will be apparent to the skilled person that the Ni—Bi plating operations according to the invention may be applied also on one or both sides of an aluminum alloy sheet or strip made of an AA4xxx-series aluminum alloys, which aluminum alloy sheet is not being provided with a core sheet to form a brazing sheet product. Such a Ni—Bi plated sheet or strip, typically having a gauge in the range of up to 3 mm, preferably in the range of 0.05 to 2 mm, may be employed also in a brazing operation as set out in this example. A similar approach can be used for plating aluminum alloy wires or rods. Such Ni—Bi plated wires or rods may be employed in a brazing operation as set out in this example or used as filler material in a welding operation, such as for laser welding operations.
- The current efficiency of Ni deposition appears to be 100%.
- The samples plated with Ni—Bi at 3 A/dm−2 showed some black spots, but the samples plated at the higher current densities have excellent appearance. About 0.5 g.m−2 bismuth was deposited. The bismuth content of the deposited alloy layer can easily be varied, e.g. by lowering the bismuth concentration in the plating bath, to give a lower Bi content.
- This plating bath has many advantages compared to the standard known Pb-containing baths:
- no ammonia fumes
- more practical operating temperatures, typically 40 to 70° C.
- high current density
- bismuth can easily be replenished to the plating bath.
- Further, standard chemicals were employed.
TABLE 1 Compound Concentration [g/l] Nickel sulphate 142 Ammonium sulphate 34 Nickel chloride 30 Sodium citrate 140 Sodium gluconate 30 Bismuth ions 1 -
TABLE 2 Current Density Time Ni Bi Invention [A/dm2] [sec.] [g/m2] [g/m2] Adhesion Brazeability yes 3 50 9.1 0.66 ± + yes 6 25 10.4 0.50 ± + yes 10 15 9.5 0.46 ± + no 3 50 9.4 — ± + - Having now fully described the invention, it will be apparent to one of ordinary skill in the art that many changes and modifications can be made without departing from the spirit or scope of the invention as herein described.
Claims (26)
1. A method of manufacturing an Al or Al alloy workpiece, which method comprises the steps of (a) providing an Al or Al alloy workpiece, (b) pre-treating of the outersurface of the Al or Al alloy workpiece, and (c) plating a metal layer comprising nickel onto said outersurface of the Al or Al alloy workpiece, wherein during step (c) said metal layer comprising nickel is deposited by plating both nickel and bismuth using an aqueous bath having
a pH in the range of 2.5 to 10, and comprising
a nickel-ion concentration in a range of 10 to 100 g/l,
a bismuth-ion concentration in the range of 0.01 to 10 g/l,
a citrate-ion concentration in the range of 40 to 150 g/l,
a gluconate-ion concentration in the range of 2 to 80 g/l,
a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l.
2. A method according to claim 1 , wherein the nickel-ion concentration is in the range of 20 to 70 g/l.
3. A method according to claim 1 , wherein the bismuth-ion concentration is in the range of 0.02 to 5 g/l.
4. A method according to claim 1 , wherein the aqueous bath and the resultant metal layer comprising nickel are essentially lead-free.
5. A method according to claim 1 , wherein the gluconate-ion concentration is in the range of 4 to 50 g/l.
6. A method according to any of claims 1, wherein said layer comprising nickel has a thickness of not more than 2.0 microns.
7. A method according to any of claims 1, wherein said layer comprising nickel has a thickness in the range of 0.03 to 1.0 micron.
8. A method according to any of claims 1, wherein said layer comprising nickel has a thickness in the range of 0.05 to 0.5 micron.
9. A method according to any one of claims 1, wherein the Bi-ion concentration results from the dissolution of one or more from the group consisting of bismuth carbonate, bismuth oxide, bismuth citrate and bismuth chloride.
10. A method according to any one of claims 1, wherein the temperature of the aqueous bath during plating is in the range of 30 to 70° C.
11. A method according to any one of claims 1, wherein the workpiece is aluminum alloy sheet or aluminum alloy wire or rod.
12. A method according to claim 1 , wherein the aluminum alloy comprises silicon as an alloying element in the range of 2 to 18% by weight.
13. A method according to claim 1 , wherein the workpiece is a brazing sheet product comprising a core sheet coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, and wherein during step (b) at least the outersurface of the aluminum clad alloy is being pre-treated.
14. A method according to claim 1 , wherein the workpiece is a brazing sheet product comprising a core sheet being made of an AA3xxx, AA5xxx, or AA6xxx-series alloy coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, and wherein during step (b) at least the outersurface of the aluminum clad alloy is being pre-treated.
15. A method according to claim 1 , wherein the workpiece is a brazing sheet product comprising a core sheet being made of an AA3xxx, AA5xxx, or AA6xxx-series alloy coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, and wherein during step (b) at least the outersurface of the aluminum clad alloy is being pre-treated by applying a thin zinc layer having a thickness of not more than 0.3 micron.
16. A method according to claim 1 , wherein the workpiece is a brazing sheet product comprising a core sheet being made of an AA3xxx, AA5xxx, or AA6xxx-series alloy coupled on at least one surface of said core sheet to an aluminum clad layer, the aluminum clad layer being made of an aluminum alloy comprising silicon in an amount in the range of 2 to 18% by weight, and wherein during step (b) at least the outersurface of the aluminum clad alloy is being pre-treated by applying a thin zinc layer having a thickness in the range of 10 to 150 nm.
17. An aqueous bath for the electrodeposition of a layer of nickel and bismuth on an Al or Al alloy workpiece, having a pH in the range of 2.5 to 10, and comprising a nickel-ion concentration in a range of 10 to 100 g/l, a bismuth-ion concentration in the range of 0.01 to 10 g/l, a citrate-ion concentration in the range of 50 to 150 g/l, a gluconate-ion concentration in the range of 2 to 80 g/l, a chloride- or fluoride-ion concentration in the range of 1 to 50 g/l.
18. An aqueous bath according to claim 17 , wherein the nickel-ion concentration is in the range of 20 to 70 g/l.
19. An aqueous bath according to claim 17 , wherein the bismuth-ion concentration is in the range of 0.02 to 5 g/l.
20. An aqueous bath according to claim 17 , wherein the gluconate-ion concentration is in the range of 4 to 50 g/l.
21. An aqueous bath according to claim 17 , wherein the following salts have been used, in grams per liter: nickel sulphate in a range of 45 to 450 g/l, chloride-ion concentration in a range of 1 to 50 g/l, sodium citrate in a range of 55 to 180 g/l, sodium gluconate in range of 2 to 90 g/l, ammonium sulphate in a range up to 270 g/l, bismuth oxide in a range of 0.02 to 22 g/l, or bismuth carbonate in a range of 0.03 to 29 g/l.
22. A method of use of the aqueous bath of claim 17 for the manufacturing of Ni-plated products for use in a brazing operation, comprising plating a metal layer comprising nickel onto an outersurface of an Al or Al alloy workpiece, wherein during said plating said metal layer comprising nickel is deposited by plating both nickel and bismuth using the aqueous bath.
23. A method of use of the aqueous bath of claim 17 for the manufacturing of Ni-plated brazing sheet products, comprising plating a metal layer comprising nickel onto an outersurface of an Al or Al alloy workpiece, wherein during said plating said metal layer comprising nickel is deposited by plating both nickel and bismuth using the aqueous bath.
24. An assembly of components joined by brazing, at least one said components being an Al or Al alloy workpiece produced by the method in accordance with claim 1 .
25. Method of manufacturing an assembly of brazed components, comprising the steps of:
(a) shaping parts of which at least one is made from an Al or Al alloy workpiece obtained by the method according to claim 1;
(b) assembling the parts into the assembly;
(c) brazing the assembly in an inert atmosphere in the absence of a brazing-flux at elevated temperature for a period long enough for melting and spreading of the molten filler;
(d) cooling the brazed assembly to below 100° C.
26. Method according to claim 25 , wherein at least one other component is selected from the group comprising steel, aluminized steel, stainless steel, plated or coated stainless steel, bronze, brass, nickel, nickel alloy, titanium, or plated or coated titanium.
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CN (1) | CN1180132C (en) |
AR (1) | AR028103A1 (en) |
AU (2) | AU8176901A (en) |
BR (1) | BR0110836B8 (en) |
CA (1) | CA2346587C (en) |
HU (1) | HUP0300706A2 (en) |
MX (1) | MXPA02010705A (en) |
WO (1) | WO2001088226A2 (en) |
ZA (1) | ZA200207838B (en) |
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US20030098338A1 (en) * | 2001-11-21 | 2003-05-29 | Dockus Kostas F. | Methods for fluxless brazing |
US20040035911A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Fluxless brazing |
US20040038070A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Fluxless brazing |
US20040035910A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Low temperature fluxless brazing |
WO2004080640A1 (en) * | 2003-03-14 | 2004-09-23 | Hille & Müller GMBH | Aluminium layered brazing product and method of its manufacture |
US20060027625A1 (en) * | 2001-11-21 | 2006-02-09 | Dana Canada Corporation | Products for use in low temperature fluxless brazing |
US20060102696A1 (en) * | 2001-11-21 | 2006-05-18 | Graham Michael E | Layered products for fluxless brazing of substrates |
US7380698B2 (en) | 2002-11-01 | 2008-06-03 | Atotech Deutschland Gmbh | Method of connecting module layers suitable for the production of microstructure modules and a microstructure module |
CN102881756A (en) * | 2012-09-14 | 2013-01-16 | 上海华友金镀微电子有限公司 | Photovoltaic solder strip of aluminum material and manufacturing method for photovoltaic solder strip |
US20180274115A1 (en) * | 2017-03-23 | 2018-09-27 | Toyota Jidosha Kabushiki Kaisha | Method of forming nickel film and nickel solution used for the method |
US10150186B2 (en) | 2014-12-11 | 2018-12-11 | Uacj Corporation | Brazing method |
US10640852B2 (en) | 2017-03-30 | 2020-05-05 | Uacj Corporation | Aluminum-alloy clad material and method of manufacturing the same |
US10661395B2 (en) | 2014-07-30 | 2020-05-26 | Uacj Corporation | Aluminum-alloy brazing sheet |
US11007609B2 (en) | 2016-11-29 | 2021-05-18 | Uacj Corporation | Brazing sheet and manufacturing method thereof |
US11298779B2 (en) | 2017-11-08 | 2022-04-12 | Uacj Corporation | Brazing sheet and manufacturing method thereof |
US11320217B2 (en) | 2016-01-14 | 2022-05-03 | Uacj Corporation | Heat exchanger and method of manufacturing the same |
EP4491764A1 (en) * | 2023-07-12 | 2025-01-15 | The Boeing Company | Surface preparation for electrolytic inorganic finish coating |
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KR100672178B1 (en) * | 2000-11-07 | 2007-01-19 | 코루스 알루미늄 발쯔프로두크테 게엠베하 | Method for manufacturing assembly of brazed components and assembly of components |
US6796484B2 (en) | 2001-02-02 | 2004-09-28 | Corus Aluminum Walzprodukte Gmbh | Nickel-plated brazing product having improved corrosion performance |
EP1383943A1 (en) | 2001-04-20 | 2004-01-28 | Corus Aluminium Walzprodukte GmbH | Method of plating and pretreating aluminium workpieces |
US6994919B2 (en) | 2002-01-31 | 2006-02-07 | Corus Aluminium Walzprodukte Gmbh | Brazing product and method of manufacturing a brazing product |
US7294411B2 (en) | 2002-01-31 | 2007-11-13 | Aleris Aluminum Koblenz Gmbh | Brazing product and method of its manufacture |
US7056597B2 (en) | 2002-12-13 | 2006-06-06 | Corus Aluminium Walzprodukte Gmbh | Brazing sheet product and method of its manufacture |
US7078111B2 (en) | 2002-12-13 | 2006-07-18 | Corus Aluminium Walzprodukte Gmbh | Brazing sheet product and method of its manufacture |
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- 2001-04-27 HU HU0300706A patent/HUP0300706A2/en unknown
- 2001-04-27 BR BRPI0110836-0A patent/BR0110836B8/en not_active IP Right Cessation
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- 2001-04-27 EP EP01960213A patent/EP1290246A1/en not_active Ceased
- 2001-04-27 AU AU2001281769A patent/AU2001281769B2/en not_active Ceased
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- 2001-05-07 US US09/849,238 patent/US6383661B2/en not_active Expired - Lifetime
- 2001-05-08 CA CA002346587A patent/CA2346587C/en not_active Expired - Lifetime
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Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030098338A1 (en) * | 2001-11-21 | 2003-05-29 | Dockus Kostas F. | Methods for fluxless brazing |
US20060027625A1 (en) * | 2001-11-21 | 2006-02-09 | Dana Canada Corporation | Products for use in low temperature fluxless brazing |
US20030197050A1 (en) * | 2001-11-21 | 2003-10-23 | Graham Michael E. | Fluxless brazing method and compositions of layered material systems for brazing aluminum or dissimilar metals |
US20040035911A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Fluxless brazing |
US20040038070A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Fluxless brazing |
US20040035910A1 (en) * | 2001-11-21 | 2004-02-26 | Dockus Kostas F. | Low temperature fluxless brazing |
US20030155409A1 (en) * | 2001-11-21 | 2003-08-21 | Dockus Kostas F. | Fluxless brazing |
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US7380698B2 (en) | 2002-11-01 | 2008-06-03 | Atotech Deutschland Gmbh | Method of connecting module layers suitable for the production of microstructure modules and a microstructure module |
WO2004080640A1 (en) * | 2003-03-14 | 2004-09-23 | Hille & Müller GMBH | Aluminium layered brazing product and method of its manufacture |
CN102881756A (en) * | 2012-09-14 | 2013-01-16 | 上海华友金镀微电子有限公司 | Photovoltaic solder strip of aluminum material and manufacturing method for photovoltaic solder strip |
US10661395B2 (en) | 2014-07-30 | 2020-05-26 | Uacj Corporation | Aluminum-alloy brazing sheet |
US10150186B2 (en) | 2014-12-11 | 2018-12-11 | Uacj Corporation | Brazing method |
US11320217B2 (en) | 2016-01-14 | 2022-05-03 | Uacj Corporation | Heat exchanger and method of manufacturing the same |
US11007609B2 (en) | 2016-11-29 | 2021-05-18 | Uacj Corporation | Brazing sheet and manufacturing method thereof |
US20180274115A1 (en) * | 2017-03-23 | 2018-09-27 | Toyota Jidosha Kabushiki Kaisha | Method of forming nickel film and nickel solution used for the method |
US11168405B2 (en) * | 2017-03-23 | 2021-11-09 | Toyota Jidosha Kabushiki Kaisha | Method of forming nickel film and nickel solution used for the method |
US10640852B2 (en) | 2017-03-30 | 2020-05-05 | Uacj Corporation | Aluminum-alloy clad material and method of manufacturing the same |
US11298779B2 (en) | 2017-11-08 | 2022-04-12 | Uacj Corporation | Brazing sheet and manufacturing method thereof |
EP4491764A1 (en) * | 2023-07-12 | 2025-01-15 | The Boeing Company | Surface preparation for electrolytic inorganic finish coating |
Also Published As
Publication number | Publication date |
---|---|
AU8176901A (en) | 2001-11-26 |
AU2001281769B2 (en) | 2004-04-01 |
CA2346587C (en) | 2005-03-08 |
WO2001088226A3 (en) | 2002-07-18 |
US6383661B2 (en) | 2002-05-07 |
CN1180132C (en) | 2004-12-15 |
ZA200207838B (en) | 2003-09-30 |
CN1427901A (en) | 2003-07-02 |
BR0110836B8 (en) | 2013-04-09 |
BR0110836A (en) | 2003-12-30 |
HUP0300706A2 (en) | 2003-07-28 |
WO2001088226A2 (en) | 2001-11-22 |
JP2003533597A (en) | 2003-11-11 |
EP1290246A1 (en) | 2003-03-12 |
BR0110836B1 (en) | 2012-10-02 |
MXPA02010705A (en) | 2005-08-26 |
CA2346587A1 (en) | 2001-11-18 |
KR20030007520A (en) | 2003-01-23 |
AR028103A1 (en) | 2003-04-23 |
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