EP1675974A2 - Pieces a usiner enduites d'un alliage aluminium-magnesium - Google Patents
Pieces a usiner enduites d'un alliage aluminium-magnesiumInfo
- Publication number
- EP1675974A2 EP1675974A2 EP04766747A EP04766747A EP1675974A2 EP 1675974 A2 EP1675974 A2 EP 1675974A2 EP 04766747 A EP04766747 A EP 04766747A EP 04766747 A EP04766747 A EP 04766747A EP 1675974 A2 EP1675974 A2 EP 1675974A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- coated workpiece
- layer
- aluminum
- intermediate layer
- substrate
- 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.)
- Withdrawn
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 52
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 39
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 39
- 239000000758 substrate Substances 0.000 claims abstract description 29
- 238000004519 manufacturing process Methods 0.000 claims abstract description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 46
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 26
- 239000011777 magnesium Substances 0.000 claims description 24
- 229910052749 magnesium Inorganic materials 0.000 claims description 24
- 229910052759 nickel Inorganic materials 0.000 claims description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 22
- 229910052751 metal Inorganic materials 0.000 claims description 21
- 239000002184 metal Substances 0.000 claims description 21
- 239000003792 electrolyte Substances 0.000 claims description 19
- 229910052782 aluminium Inorganic materials 0.000 claims description 18
- 229910052742 iron Inorganic materials 0.000 claims description 11
- 229910045601 alloy Inorganic materials 0.000 claims description 9
- 239000000956 alloy Substances 0.000 claims description 9
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 150000002739 metals Chemical class 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 229910017052 cobalt Inorganic materials 0.000 claims description 6
- 239000010941 cobalt Substances 0.000 claims description 6
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 6
- 238000004512 die casting Methods 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 239000007864 aqueous solution Substances 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 239000011733 molybdenum Substances 0.000 claims description 3
- 239000011135 tin Substances 0.000 claims description 3
- 229910052718 tin Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- 229910000640 Fe alloy Inorganic materials 0.000 claims description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- -1 ferrous metals Chemical class 0.000 claims description 2
- 239000004615 ingredient Substances 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- 239000011701 zinc Substances 0.000 claims description 2
- 238000004873 anchoring Methods 0.000 claims 1
- 229910001092 metal group alloy Inorganic materials 0.000 claims 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims 1
- 239000010410 layer Substances 0.000 description 87
- 230000007797 corrosion Effects 0.000 description 27
- 238000005260 corrosion Methods 0.000 description 27
- 238000000576 coating method Methods 0.000 description 11
- 239000011248 coating agent Substances 0.000 description 10
- 239000011255 nonaqueous electrolyte Substances 0.000 description 10
- 239000002344 surface layer Substances 0.000 description 7
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 5
- 230000006378 damage Effects 0.000 description 4
- 238000004070 electrodeposition Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- KERTUBUCQCSNJU-UHFFFAOYSA-L nickel(2+);disulfamate Chemical compound [Ni+2].NS([O-])(=O)=O.NS([O-])(=O)=O KERTUBUCQCSNJU-UHFFFAOYSA-L 0.000 description 3
- 239000011241 protective layer Substances 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 150000004820 halides Chemical class 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 2
- POILWHVDKZOXJZ-ARJAWSKDSA-M (z)-4-oxopent-2-en-2-olate Chemical compound C\C([O-])=C\C(C)=O POILWHVDKZOXJZ-ARJAWSKDSA-M 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical group C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical group [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- CUJRVFIICFDLGR-UHFFFAOYSA-N acetylacetonate Chemical compound CC(=O)[CH-]C(C)=O CUJRVFIICFDLGR-UHFFFAOYSA-N 0.000 description 1
- 125000005595 acetylacetonate group Chemical group 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 239000002318 adhesion promoter Substances 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
- 125000000217 alkyl group Chemical group 0.000 description 1
- 239000000010 aprotic solvent Substances 0.000 description 1
- 239000012736 aqueous medium Substances 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000000536 complexating effect Effects 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 239000002659 electrodeposit Substances 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000001465 metallisation Methods 0.000 description 1
- CLDVQCMGOSGNIW-UHFFFAOYSA-N nickel tin Chemical compound [Ni].[Sn] CLDVQCMGOSGNIW-UHFFFAOYSA-N 0.000 description 1
- 238000002161 passivation Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229910052700 potassium Chemical group 0.000 description 1
- 239000011591 potassium Chemical group 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 150000003871 sulfonates Chemical class 0.000 description 1
- 150000003467 sulfuric acid derivatives Chemical class 0.000 description 1
- 238000004381 surface treatment Methods 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
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
-
- 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
-
- 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
- C25D5/36—Pretreatment of metallic surfaces to be electroplated of iron or steel
-
- 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
- Y10T428/12181—Composite powder [e.g., coated, etc.]
Definitions
- the present invention is directed to workpieces coated with an aluminum / magnesium alloy, and to a process for their production.
- the deposition of aluminum, magnesium or aluminum / magnesium alloys on workpieces which consist of base metal is a tried and tested means of protecting these workpieces from corrosion. At the same time, they are provided with a decorative coating.
- the protective metal layer is mainly electrodeposited on the workpiece. The deposited metal layer significantly improves the corrosion resistance of the workpiece. It turns out, however, that the corrosion resistance of the workpiece depends on the adhesion of the protective layer applied to the workpiece. If the protective layer does not adhere sufficiently to the workpiece, the protective layer is easily removed, e.g. B. at
- DE 31 12 919 A1 proposes to provide metal-coated iron workpieces with an adhesion-promoting intermediate layer made of cobalt, cobalt alloys or nickel-containing cobalt and to galvanically apply an aluminum layer thereon.
- the intermediate layer serving as an adhesion promoter is applied galvanically from an aqueous medium.
- the galvano-aluminum layer are chromated. This further improves the corrosion resistance.
- DE 38 04 303 proposes a method for improving the adhesion of galvanic aluminum layers to metal workpieces by applying an adhesion-promoting layer.
- a non-aqueous electrolyte is used to apply the adhesive layer made of iron, iron and nickel, nickel, cobalt, copper and alloys of the above-mentioned metals or tin-nickel alloys.
- a galvano-aluminum layer is applied to the intermediate layer.
- the application of the intermediate layer from a non-aqueous electrolyte is essential, since otherwise, when using an aqueous electrolyte, the metal workpiece becomes embrittled due to the hydrogen generated during the electrolysis. As a result, the often used low-alloy high-strength steels are adversely affected. Embrittlement of the workpieces is avoided by using a non-aqueous electrolyte to apply the metallic intermediate layer.
- EP 1 141 447 B1 describes electrolytes for coating
- Prior art layers are very hard and brittle.
- fasteners that are provided with an aluminum / magnesium layer, such as. B. screws, used to fasten components
- This risk is particularly so when the components are made of relatively soft or brittle materials, such as. B. made of magnesium. Due to the superficial destruction of the component, this can in turn be exposed to increased corrosion, which can lead to the destruction of the component.
- the above-described corrosion occurs increasingly at high pH values, so that in both of the aforementioned cases of destruction of the surface layer of the fastening means or of the component, the rate of corrosion increases at high pH values.
- the technical object of the present invention is to provide coated workpieces which have improved corrosion resistance, have in particular in the alkaline range and, in combination with other materials, show reduced corrosion, in particular if the coated workpieces are used as fastening means for fastening components.
- a coated workpiece comprising a substrate, a metallic intermediate layer applied to the substrate and a layer applied to the intermediate layer containing an aluminum / magnesium alloy.
- the surface of the substrate is electrically conductive. This can preferably be done by coating the substrate with graphite.
- the substrate preferably contains a metal and / or a metal
- the substrate can be a metallized substrate, wherein the substrate can be metallized over the entire surface or over part of the surface.
- Preferred substrates contain plastics.
- the substrate can furthermore be selected from the ingredients
- the metallic intermediate layer preferably contains iron, iron and nickel, tin and nickel, nickel, cobalt, copper, chromium, molybdenum, vanadium or alloys of the above-mentioned metals.
- the metallic intermediate layer preferably has a layer thickness of 0.1 ⁇ m to 30 ⁇ m.
- the Layer thickness of the metallic intermediate layer 0.5 ⁇ m to 20 ⁇ m, more preferably 1 ⁇ m to 10 ⁇ m and most preferably 1.5 ⁇ m to 8 ⁇ m
- the applied to the metallic intermediate layer containing an aluminum / magnesium alloy preferably contains 0.5 to 70 5 wt.% Magnesium. In a further preferred embodiment, 1 to 50% by weight, more preferably 2 to 40% by weight, in a further preferred embodiment 3 to 30% by weight, preferably 4 to 25% by weight and most preferably 5 to 20% by weight. % Magnesium contained in the aluminum / magnesium alloy.
- the layer containing an aluminum / magnesium alloy preferably has a layer thickness of 0.1 ⁇ m to 100 ⁇ m.
- the layer thickness is 0.5 ⁇ m to 70 ⁇ m, more preferably 1 ⁇ m to 50 ⁇ m, preferably 2 ⁇ m to 40 ⁇ m, more preferably 3 ⁇ m to 30 ⁇ m, more preferably 4 ⁇ m to 28 ⁇ m and most preferred 5 ⁇ m to
- the layer containing the aluminum / magnesium alloy is preferably the surface layer of the coated workpiece.
- at least one layer can also be applied to the layer containing the aluminum / magnesium alloy, which is preferably a passivation 2 o.
- the coated workpiece is preferably a rack, bulk goods or a continuous product, wherein the coated workpiece is preferably a wire, a sheet, a screw, a nut, a concrete anchor, a fastener or a machine component.
- the coated workpiece is preferably used in the automotive industry in the transmission, engine and body area. It can be an oil pan or a transmission oil pan.
- Another object of the present invention is to provide a method for producing a coated workpiece, comprising the steps of: a) applying a metallic intermediate layer to a substrate and b) applying a layer containing an aluminum / magnesium alloy to the metallic intermediate layer ,
- the metallic intermediate layer is deposited from an aqueous solution or a non-aqueous solution.
- the metallic intermediate layer is chemically deposited.
- the metallic intermediate layer can be electrodeposited from an aqueous electrolyte.
- electrolytes are solutions of the metal salts of iron, cobalt, nickel, copper or tin. These can be in the form of halides, sulfates, sulfonates or fluoroborates.
- the electrolytes can contain further additives, such as, for example. B. complexing substances.
- step a) it is also possible in step a) to electrodeposit the metallic intermediate layer from a non-aqueous electrolyte.
- Possible electrolytes contain compounds of molybdenum or vanadium or all other aforementioned metals, which the intermediate layer can contain.
- the metals are preferably in the form of halides which can be complexed or reacted with ether, in particular diethyl ether and / or acetylacetonate (acac), to give corresponding metal acetylacetonates.
- the layer containing an aluminum / magnesium alloy is preferably deposited from an anhydrous electrolyte.
- the layer containing an aluminum / magnesium alloy is electrodeposited from a water-free electrolyte in step b).
- Any electrolyte which is known to the person skilled in the art can be used as the electrolyte.
- the electrolyte contains organoaluminum compounds of the general formulas (I) and (II)
- n 0 or 1
- M is sodium or potassium and R 1 , R 2 , R 3 , R 4 may be the same or different, where R 1 , R 2 , R 3 , R 4 is a Ci to C Al- are alkyl group and a halogen-free, aprotic solvent is used as the solvent for the electrolyte.
- a mixture of the complexes K [AIEt 4 ], Na [AlEtJ and AIEt 3 can be used as the electrolyte.
- the molar ratio of the complexes to AIEt 3 is preferably 1: 0.5 to 1: 3 and more preferably 1: 2.
- the electrolytic deposition of the layer containing an aluminum / magnesium alloy on the workpiece is carried out using a soluble aluminum and a likewise soluble magnesium anode or using an anode made of an aluminum / magnesium alloy.
- the electrolytic coating is preferably carried out at a temperature of 80 to 105 ° C.
- a temperature of the electroplating bath of 91 to 100 ° C. is preferred
- a layer that conducts the electrical current is applied to the substrate before the metallic intermediate layer is applied in step a).
- the layer which conducts the electrical current can be applied to the substrate by any method which is known to the person skilled in the art.
- the layer that conducts the electrical current is preferably applied to the substrate by metallization.
- a sheet of size 100 x 25 x 1 mm made of St37 steel is provided with a nickel intermediate layer with a thickness of approx. 1 ⁇ m.
- the nickel layer is electrodeposited from an aqueous nickel sulfamate electrolyte.
- a layer of an aluminum / magnesium alloy with a magnesium content of 20% by weight and a layer thickness of 12 ⁇ m is subsequently deposited on the nickel layer by electrodeposition from a non-aqueous electrolyte.
- the coated sheet is bent lengthwise through an angle of 180 °, the applied metal layers remaining intact in the area of the bending edge.
- a sheet of size 100 x 25 x 1 mm made of St37 steel is provided with a layer of an aluminum / magnesium alloy with a magnesium content of 20% by weight and a layer thickness of 12 ⁇ m by electrodeposition from a non-aqueous electrolyte.
- the sheet coated in this way is bent lengthwise through an angle of 180 °, parts of the coating tearing open at the bending edge and flaking off in the form of the finest needles.
- Five M6 x 55 screws are provided with an aluminum / magnesium alloy with a magnesium content of 15% by weight and a layer thickness of 16 ⁇ m by electrodeposition from a non-aqueous electrolyte.
- Five additional M6 x 55 screws are covered with a nickel layer with a layer thickness of approx. 1 ⁇ m.
- the nickel layer is electrodeposited from an aqueous nickel sulfamate electrolyte.
- An aluminum / magnesium alloy with a magnesium content of 15% by weight and a layer thickness of 16 ⁇ m is subsequently applied to the nickel layer by electrodeposition from a non-aqueous electrolyte.
- M5 x 5 screws are electroplated in a drum with an aluminum / magnesium alloy with a magnesium content of 10% by weight and an average layer thickness of 14 ⁇ m from a non-aqueous electrolyte.
- Additional screws are provided with an intermediate nickel layer with a layer thickness of approx. 1-2 ⁇ m nickel.
- the nickel layer is electroplated from an aqueous nickel sulfamate electrolyte.
- a layer of an aluminum / magnesium alloy with a magnesium content of 10% by weight and an average layer thickness of 15 ⁇ m from a non-aqueous electrolyte is applied galvanically to the nickel layer in a drum.
- the metallic intermediate layer causes a significant improvement in the corrosion resistance.
- Coated workpieces comprising a substrate, a metallic intermediate layer applied to the substrate and a layer containing an aluminum / magnesium alloy applied to the intermediate layer show a superior property profile which the prior art workpieces do not have.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Electroplating Methods And Accessories (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Laminated Bodies (AREA)
- Electroplating And Plating Baths Therefor (AREA)
Abstract
L'invention concerne une pièce à usiner enduite, qui comprend un substrat, une couche intermédiaire métallique appliquée sur le substrat, ainsi qu'une couche appliquée sur cette couche intermédiaire et contenant un alliage aluminium-magnésium. L'invention concerne également un procédé pour la production d'une telle pièce à usiner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP04766747A EP1675974A2 (fr) | 2003-10-18 | 2004-09-09 | Pieces a usiner enduites d'un alliage aluminium-magnesium |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP03023454A EP1524336A1 (fr) | 2003-10-18 | 2003-10-18 | Pièces à usiner recouvertes d'un alliage aluminium-magnesium |
| EP04766747A EP1675974A2 (fr) | 2003-10-18 | 2004-09-09 | Pieces a usiner enduites d'un alliage aluminium-magnesium |
| PCT/EP2004/052097 WO2005035835A2 (fr) | 2003-10-18 | 2004-09-09 | Pieces a usiner enduites d'un alliage aluminium-magnesium |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1675974A2 true EP1675974A2 (fr) | 2006-07-05 |
Family
ID=34354482
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03023454A Withdrawn EP1524336A1 (fr) | 2003-10-18 | 2003-10-18 | Pièces à usiner recouvertes d'un alliage aluminium-magnesium |
| EP04766747A Withdrawn EP1675974A2 (fr) | 2003-10-18 | 2004-09-09 | Pieces a usiner enduites d'un alliage aluminium-magnesium |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03023454A Withdrawn EP1524336A1 (fr) | 2003-10-18 | 2003-10-18 | Pièces à usiner recouvertes d'un alliage aluminium-magnesium |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20070212563A1 (fr) |
| EP (2) | EP1524336A1 (fr) |
| JP (1) | JP2007509233A (fr) |
| KR (1) | KR20060097016A (fr) |
| CN (1) | CN1871375A (fr) |
| RU (1) | RU2353714C2 (fr) |
| WO (1) | WO2005035835A2 (fr) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007016126A1 (de) * | 2007-03-29 | 2008-10-02 | Robert Bosch Gmbh | Anordnung mit mindestens einem in Berührungskontakt mit mindestens einem Kunststoffbauelement stehenden Metallteil |
| DE102008051883A1 (de) | 2008-10-16 | 2010-04-22 | Nano-X Gmbh | Beschichtung zum kathodischen Korrosionsschutz von Metall, Verfahren zum Herstellen der Beschichtung und Verwendung der Beschichtung. |
| CN102383129A (zh) * | 2010-09-03 | 2012-03-21 | 鸿富锦精密工业(深圳)有限公司 | 壳体及其制造方法 |
| RU2519694C1 (ru) * | 2013-05-23 | 2014-06-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технологический университет "СТАНКИН" (ФГБОУ ВПО МГТУ "СТАНКИН") | Способ нанесения антикоррозийных покрытий на подложку из высокотвердых сплавов |
| KR102471961B1 (ko) * | 2017-07-12 | 2022-11-28 | 르노코리아자동차 주식회사 | 자동차용 이중 금속판재구조 및 이의 제조방법 |
| DE102017126590A1 (de) * | 2017-11-13 | 2019-05-16 | Doduco Solutions Gmbh | Verfahren zum Herstellen einer Bodenplatte für ein Elektronikmodul |
| RU2713771C1 (ru) * | 2019-10-23 | 2020-02-07 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Елецкий государственный университет им. И.А. Бунина" | Электролит для осаждения сплава Cr-V |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3112919A1 (de) * | 1981-03-31 | 1982-10-07 | Siemens AG, 1000 Berlin und 8000 München | "metallbeschichtete eisenwerkstoffe" |
| RU2023761C1 (ru) * | 1991-04-03 | 1994-11-30 | Институт неорганической химии АН Латвии | Способ подготовки поверхности алюминиевых сплавов перед нанесением оловянных покрытий |
| US4778575A (en) * | 1988-01-21 | 1988-10-18 | The United States Of America As Represented By The United States Department Of Energy | Electrodeposition of magnesium and magnesium/aluminum alloys |
| DE3804303A1 (de) * | 1988-02-12 | 1989-08-24 | Studiengesellschaft Kohle Mbh | Verfahren zur haftvermittlung zwischen metallwerkstoffen und glavanischen aluminiumschichten und hierbei eingesetzte nichtwaessrige elektrolyte |
| US5225291A (en) * | 1990-11-07 | 1993-07-06 | Alupower, Inc. | Deferred actuated battery assembly |
| RU2112086C1 (ru) * | 1996-10-28 | 1998-05-27 | Закрытое акционерное общество "Техно-ТМ" | Способ нанесения электролитического покрытия на поверхности металлов или сплавов и электролитическое покрытие |
| US6203936B1 (en) * | 1999-03-03 | 2001-03-20 | Lynntech Inc. | Lightweight metal bipolar plates and methods for making the same |
| DE19855666A1 (de) * | 1998-12-01 | 2000-06-08 | Studiengesellschaft Kohle Mbh | Aluminiumorganische Elektrolyte und Verfahren zur elektrolytischen Beschichtung mit Aluminium oder Aluminium-Magnesium Legierungen |
| WO2002088434A1 (fr) * | 2001-04-30 | 2002-11-07 | Alumiplate Incorporated | Formulations d'electrodeposition d'aluminium |
| EP1279751A1 (fr) * | 2001-07-28 | 2003-01-29 | Aluminal Oberflächtentechnik GmbH & Co. KG | Appareil pour la deposition d' aluminium ou d'alliage d'aluminium à partir des electrolytes contenant des alkyles d'aluminium |
| EP1403402A1 (fr) * | 2002-09-25 | 2004-03-31 | Aluminal Oberflächtentechnik GmbH & Co. KG | Procédé pour la déposition electrolytique des materiaux avec aluminium, magnesium ou les alliages d'aluminium et magnesium |
| EP1518945A1 (fr) * | 2003-09-27 | 2005-03-30 | Aluminal Oberflächtentechnik GmbH & Co. KG | Electrolyte pour la deposition galvanique d'alliages aluminium magnesium |
| EP1682697A2 (fr) * | 2003-11-07 | 2006-07-26 | Aluminal Oberflächtentechnik GmbH & Co. KG | Revetement de substrats |
-
2003
- 2003-10-18 EP EP03023454A patent/EP1524336A1/fr not_active Withdrawn
-
2004
- 2004-09-09 RU RU2006117025/02A patent/RU2353714C2/ru not_active IP Right Cessation
- 2004-09-09 US US10/576,284 patent/US20070212563A1/en not_active Abandoned
- 2004-09-09 CN CNA2004800307029A patent/CN1871375A/zh active Pending
- 2004-09-09 EP EP04766747A patent/EP1675974A2/fr not_active Withdrawn
- 2004-09-09 JP JP2006534735A patent/JP2007509233A/ja not_active Abandoned
- 2004-09-09 KR KR1020067007417A patent/KR20060097016A/ko not_active Ceased
- 2004-09-09 WO PCT/EP2004/052097 patent/WO2005035835A2/fr not_active Ceased
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2005035835A2 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2005035835A2 (fr) | 2005-04-21 |
| RU2353714C2 (ru) | 2009-04-27 |
| US20070212563A1 (en) | 2007-09-13 |
| WO2005035835A3 (fr) | 2005-06-23 |
| KR20060097016A (ko) | 2006-09-13 |
| RU2006117025A (ru) | 2007-11-27 |
| EP1524336A1 (fr) | 2005-04-20 |
| CN1871375A (zh) | 2006-11-29 |
| JP2007509233A (ja) | 2007-04-12 |
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