US2014342095A1PendingUtilityA1
Method for depositing an anticorrosive coating
Est. expiryMay 16, 2033(~6.8 yrs left)· nominal 20-yr term from priority
C23C 4/08C23C 4/125C23C 4/131
45
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Claims
Abstract
A method for depositing an anticorrosive coating on components, wherein an aluminum-zinc coating is used as an anticorrosive coating, and wherein the anticorrosive coating is deposited by thermal spraying, wherein an inert carrier gas with a reducing gas component is used for the thermal spraying.
Claims
exact text as granted — not AI-modifiedHaving thus described the invention, what we claim is:
1 . A method for depositing an anticorrosive coating on components, wherein an aluminium-zinc coating is used at least as a component part of an anticorrosive coating, characterised in that the aluminium-zinc coating is deposited by thermal spraying, wherein an inert gas with a reducing gas component is used for the thermal spraying.
2 . The method according to claim 1 , wherein a further coating is deposited on or under the aluminium-zinc layer.
3 . The method according to claim 2 , wherein the further coating comprises one or more coloured layers.
4 . The method according to claim 1 , wherein hydrogen is used as the reducing gas component.
5 . The method according to claim 1 , wherein nitrogen is used as the inert gas.
6 . The method according to claim 1 , wherein a hydrogen-nitrogen mixture is used for the thermal spraying.
7 . The method according so claim 1 , wherein arc spraying is used for the thermal spraying.
8 . The method according to claim 1 , wherein the aluminium-zinc coating layer alone or as a component part of an anticorrosive coating is deposited on areas subject to high mechanical load to reduce wear and corrosion.
9 . The method according to claim 1 , wherein a proportion of the reducing gas component in the inert gas amounts to between 0.1% and 10%
10 . The method according to claim 1 , wherein a proportion of the reducing gas component in the inert gas amounts to between 2% and 4%.
11 . The method according to claim 1 , wherein a thickness of the aluminium-zinc coating amounts to between 50 μm and 150 μm.
12 . The method according to claim 1 , wherein a thickness of the aluminum-zinc coating amounts to between 75 μm and 120 μm.
13 . The method according to claim 1 , wherein a thickness of the aluminium-zinc coating amounts to 100 μm.
14 . The method according to claim 1 , wherein the adhesiveness of the spray-metallised aluminium-zinc layer amounts on average to between 7.0 and 8.0 MPa.
15 . The method according to claim 2 , wherein the adhesiveness of the further layers to the spray-metallised aluminium-zinc layer itself or of the anticorrosive coating to the coated, material amounts on average to between 7.0 and 8.0 MPa.
16 . The method according to claim 1 , wherein the anticorrosive coating is deposited on components that are exposed to a corrosive atmosphere.
17 . The method according to claim 1 , wherein the corrosive atmosphere is selected from the group consisting of a sea water atmosphere, a marine atmosphere and a chemical atmosphere.
18 . The method according to claim 1 , wherein the anticorrosive coating is deposited on components of a wind energy plant.
19 . The method according to claim 1 , wherein the wind energy plant is an offshore wind energy plant.
20 . The method according to claim 1 , wherein the inert gas with the reducing gas component is nitrogen and hydrogen.Join the waitlist — get patent alerts
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