CN207313720U - High rigidity impact resistance plastics electroplating surface Rotating fields - Google Patents
High rigidity impact resistance plastics electroplating surface Rotating fields Download PDFInfo
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- CN207313720U CN207313720U CN201720533972.6U CN201720533972U CN207313720U CN 207313720 U CN207313720 U CN 207313720U CN 201720533972 U CN201720533972 U CN 201720533972U CN 207313720 U CN207313720 U CN 207313720U
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- microns
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- copper
- impact resistance
- high rigidity
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Abstract
It the utility model is related to polymer surface coating structure field; in particular it is high rigidity impact resistance plastics electroplating surface Rotating fields; including frosting, preplating layers of copper, electroplating copper tin alloy layer, nanometer composite layer, basic plating layers of copper, nickel-chrome alloy layer, solid chromium, plating silver layer and protective layer; using two kinds of materials of cerium oxide and zinc; corrosion resistance is good, wearability is good, hardness is big; being added into plastics can make plastics become very fine and close, and toughness, intensity also make moderate progress.The surface of frosting is disposed with preplating layers of copper, electroplating copper tin alloy layer, nanometer composite layer, basic plating layers of copper, nickel-chrome alloy layer, solid chromium, plating silver layer and protective layer from the inside to the outside.
Description
Technical field
Polymer surface coating structure field is the utility model is related to, is in particular high rigidity impact resistance plastics
Electroplating surface Rotating fields.
Background technology
The plastic part that automotive trim is used requires the appearance of light, wear-resistant, corrosion-resistant, especially requires resistance to punching
Hit.Prior art frosting coating includes electroless nickel layer, burnt layers of copper, bloom nickel layer and chrome layer, due to using in the structure
Nickel layer is as high photosphere, although fine with certain thickness nickel layer texture, nickel layer is different with the coefficient of expansion of layers of copper, leads
Pyrogenicity deformation is different, and the thermal stress of generation is easy to cause coming off for coating, under the vibration environment of running car, in substrate plastic
Under the induction of generating period miniature deformation, easily there is situation about departing from adjacent burnt layers of copper in thicker nickel layer, finally makes
Coating comes off, so designing high rigidity impact resistance plastics electroplating surface Rotating fields to solve the problems, such as this.
The content of the invention
The utility model uses mainly solving the technical problems that offer high rigidity impact resistance plastics electroplating surface Rotating fields
Two kinds of materials of cerium oxide and zinc, corrosion resistance is good, wearability is good, hardness is big, and being added into plastics can make plastics become to cause very much
Close, toughness, intensity also make moderate progress.
In order to solve the above technical problems, polymer surface coating structure field is the utility model is related to, more specifically
Say it is high rigidity impact resistance plastics electroplating surface Rotating fields, including frosting, preplating layers of copper, electroplating copper tin alloy layer, nanometer
Composite layer, basic plating layers of copper, nickel-chrome alloy layer, solid chromium, plating silver layer and protective layer, using cerium oxide and zinc two
Kind material, corrosion resistance is good, wearability is good, hardness is big, and being added into plastics can make plastics become very fine and close, toughness, intensity
Also make moderate progress.
The surface of frosting is disposed with preplating layers of copper, electroplating copper tin alloy layer, nanocomposite from the inside to the outside
Layer, basic plating layers of copper, nickel-chrome alloy layer, solid chromium, plating silver layer and protective layer.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the preplating layers of copper stated is 5 microns to 15 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the electroplating copper tin alloy layer stated is 20 microns to 50 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the nanometer composite layer stated is 10 microns to 20 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the basic plating layers of copper stated is 5 microns to 15 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the nickel-chrome alloy layer stated is 20 microns to 100 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the solid chromium stated is 15 microns to 20 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the plating silver layer stated is 20 microns to 30 microns.
As the further optimization of the technical program, the utility model high rigidity impact resistance plastics electroplating surface Rotating fields institute
The thickness for the protective layer stated is 15 microns to 25 microns.
The utility model high rigidity impact resistance plastics electroplating surface Rotating fields have the beneficial effect that：
The utility model high rigidity impact resistance plastics electroplating surface Rotating fields, it is anti-corrosion using two kinds of materials of cerium oxide and zinc
Property is good, wearability is good, hardness is big, and being added into plastics can make plastics become very fine and close, and toughness, intensity also make moderate progress.
Brief description of the drawings
The utility model is described in more detail with specific implementation method below in conjunction with the accompanying drawings.
Fig. 1 is the structure diagram of the utility model high rigidity impact resistance plastics electroplating surface Rotating fields.
In figure：Frosting 1；Preplating layers of copper 2；Electroplating copper tin alloy layer 3；Nanometer composite layer 4；Basic plating layers of copper
5；Nickel-chrome alloy layer 6；Solid chromium 7；Electroplate silver layer 8；Protective layer 9.
Embodiment
Embodiment one：
Illustrate present embodiment with reference to Fig. 1, the utility model is related to polymer surface coating structure field, more
Specifically high rigidity impact resistance plastics electroplating surface Rotating fields, including frosting 1, preplating layers of copper 2, electroplating copper tin alloy
Layer 3, nanometer composite layer 4, basic plating layers of copper 5, nickel-chrome alloy layer 6, solid chromium 7, plating silver layer 8 and protective layer 9, are adopted
With two kinds of materials of cerium oxide and zinc, corrosion resistance is good, wearability is good, hardness is big, and being added into plastics can be such that plastics become very
Densification, toughness, intensity also make moderate progress.
The surface of frosting 1 is disposed with preplating layers of copper 2, electroplating copper tin alloy layer 3, nano combined material from the inside to the outside
The bed of material 4, basic plating layers of copper 5, nickel-chrome alloy layer 6, solid chromium 7, plating silver layer 8 and protective layer 9, preplating layers of copper 2 can have
Effect alleviate coating and contact layer due to thermal coefficient of expansion mismatches and caused by thermal stress issues, nanometer composite layer 4 is anti-corrosion
Property is good, wearability is good, hardness is big, and being added into plastics can make plastics become very fine and close, and toughness, intensity also make moderate progress,
Solid chromium 7 is prepared using traditional Cr VI Hard Chromium Plating Technology.
Embodiment two：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, and described is pre-
The thickness of copper plate 2 is 5 microns to 15 microns.
Embodiment three：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, the electricity
The thickness of bronze (copper-tin alloy) electroplating layer 3 is 20 microns to 50 microns.
Embodiment four：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, and described receives
The thickness of nano composite material layer 4 is 10 microns to 20 microns.
Embodiment five：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, the alkali
Property copper electroplating layer 5 thickness be 5 microns to 15 microns.
Embodiment six：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, the nickel
The thickness of chromium alloy layer 6 is 20 microns to 100 microns.
Embodiment seven：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, and described is hard
The thickness of chrome layer 7 is 15 microns to 20 microns.
Embodiment eight：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, the electricity
The thickness of silver coating 8 is 20 microns to 30 microns.
Embodiment nine：
Illustrate present embodiment with reference to Fig. 1, present embodiment is described further embodiment one, the guarantor
The thickness of sheath 9 is 15 microns to 25 microns.
Certainly, described above is not limitation of the utility model, and the utility model is also not limited to the example above, this skill
The variations, modifications, additions or substitutions that the those of ordinary skill in art field is made in the essential scope of the utility model, also belong to
In the scope of protection of the utility model.
Claims (9)
1. high rigidity impact resistance plastics electroplating surface Rotating fields, including frosting（1）, preplating layers of copper（2）, electroplating copper tin alloy
Layer（3）, nanometer composite layer（4）, basic plating layers of copper（5）, nickel-chrome alloy layer（6）, solid chromium（7）, plating silver layer（8）
And protective layer（9）, it is characterised in that：Frosting（1）Surface be disposed with preplating layers of copper from the inside to the outside（2）, electro-coppering
Tin alloy layers（3）, nanometer composite layer（4）, basic plating layers of copper（5）, nickel-chrome alloy layer（6）, solid chromium（7）, plating
Silver layer（8）And protective layer（9）.
2. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The preplating
Layers of copper（2）Thickness be 5 microns to 15 microns.
3. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The plating
Signal bronze layer（3）Thickness be 20 microns to 50 microns.
4. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The nanometer
Composite layer（4）Thickness be 10 microns to 20 microns.
5. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The alkalescence
Copper electroplating layer（5）Thickness be 5 microns to 15 microns.
6. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The nickel chromium triangle
Alloy-layer（6）Thickness be 20 microns to 100 microns.
7. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The hard plating
Layers of chrome（7）Thickness be 15 microns to 20 microns.
8. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The plating
Silver layer（8）Thickness be 20 microns to 30 microns.
9. high rigidity impact resistance plastics electroplating surface Rotating fields according to claim 1, it is characterised in that：The protection
Layer（9）Thickness be 15 microns to 25 microns.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720533972.6U CN207313720U (en) | 2017-05-15 | 2017-05-15 | High rigidity impact resistance plastics electroplating surface Rotating fields |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720533972.6U CN207313720U (en) | 2017-05-15 | 2017-05-15 | High rigidity impact resistance plastics electroplating surface Rotating fields |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207313720U true CN207313720U (en) | 2018-05-04 |
Family
ID=62436196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720533972.6U Expired - Fee Related CN207313720U (en) | 2017-05-15 | 2017-05-15 | High rigidity impact resistance plastics electroplating surface Rotating fields |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207313720U (en) |
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2017
- 2017-05-15 CN CN201720533972.6U patent/CN207313720U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180504 Termination date: 20200515 |