Zinc-cadmium alloy composite coating of aerospace electric appliance accessory and preparation method of zinc-cadmium alloy composite coating
A technology of electrical accessories and alloy coating, which is applied in the direction of superimposed layer plating, metal material coating process, coating, etc., can solve the problems of trivalent chromium passivation layer not having self-healing property, human health and natural environment damage, Corrosion resistance decline and other problems
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[0039] The present invention also provides a preparation method for the zinc-cadmium alloy composite coating of the aerospace electrical accessories described in the technical solution, comprising the following steps:
[0040] An electroless zinc-precipitated layer, a nickel coating, a zinc-cadmium alloy coating, a silane chromium-free passivation layer and a graphene sealing layer are sequentially prepared on the surface of the aluminum alloy substrate.
[0041] The invention prepares a chemical zinc-precipitated layer on the surface of an aluminum alloy substrate. In the present invention, the aluminum alloy substrate is preferably placed in the zinc-precipitating solution for zinc-precipitation. In the present invention, the aluminum alloy substrate is preferably pretreated before preparing the chemical zinc-precipitated layer. In the present invention, the pretreatment method preferably includes wax removal, oil removal and activation performed in sequence. The present i...
Embodiment 1
[0069] The structural representation of the zinc-cadmium alloy composite coating of the aerospace electrical accessories prepared in this embodiment is as follows figure 1 As shown, an electroless zinc-precipitated layer 2, a nickel coating 3, a zinc-cadmium alloy coating 4, a silane chromium-free passivation layer 5, and a graphene sealing layer 6 are sequentially prepared on an aluminum alloy substrate 1 from inside to outside.
[0070] In the invention, the aluminum alloy substrate is sequentially subjected to chemical wax removal, water washing, ultrasonic wax removal, water washing, chemical oil removal, water washing, activation and water washing steps to obtain the pretreated aluminum alloy substrate.
[0071] The pretreated aluminum alloy substrate is sequentially subjected to the first zinc precipitation, water washing, zinc stripping, water washing, second zinc precipitation and water washing to form a chemical zinc precipitation layer on the surface of the aluminum a...
Embodiment 2
[0084] The structural representation of the zinc-cadmium alloy composite coating of the aerospace electrical accessories prepared in this embodiment is as follows figure 1 As shown, an electroless zinc-precipitated layer 2, a nickel coating 3, a zinc-cadmium alloy coating 4, a silane chromium-free passivation layer 5, and a graphene sealing layer 6 are sequentially prepared on an aluminum alloy substrate 1 from inside to outside.
[0085] In the invention, the aluminum alloy substrate is sequentially subjected to chemical wax removal, water washing, ultrasonic wax removal, water washing, chemical oil removal, water washing, activation and water washing steps to obtain the pretreated aluminum alloy substrate.
[0086] The pretreated aluminum alloy substrate is sequentially subjected to the first zinc precipitation, water washing, zinc stripping, water washing, second zinc precipitation and water washing to form a chemical zinc precipitation layer on the surface of the aluminum a...
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