CN104558652A - Surface deposition method of cockpit for aircraft - Google Patents
Surface deposition method of cockpit for aircraft Download PDFInfo
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- CN104558652A CN104558652A CN201410804649.9A CN201410804649A CN104558652A CN 104558652 A CN104558652 A CN 104558652A CN 201410804649 A CN201410804649 A CN 201410804649A CN 104558652 A CN104558652 A CN 104558652A
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- moulding
- driving cabin
- cockpit
- aircraft cockpit
- baking
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Abstract
The invention discloses a surface deposition method of a cockpit for an aircraft. The surface deposition method comprises the following steps: S01, pretreating, preparing to prepare a substrate raw material of the cockpit of the aircraft, and baking for a period of time; S02, treating by tinting and injection molding, adding tinting powder into the substrate raw material after baking, uniformly stirring, pouring into a hopper of an injection molding machine, carrying out tinting and injection molding to obtain an injection part of the cockpit; S03, carrying out hardening treatment on the injection part, putting the injection part of the cockpit into a hardening liquid for a period of time to obtain a hardened injection part of the cockpit, and carrying out solidification treatment on the hardened injection part of the cockpit; and S04, carrying out optical coating treatment, putting the hardened injection part of the cockpit into an optical coating work station, adding a solid oxide into the optical coating work station, and enabling the solid oxide to be adhered to the outer surface of the injection part of the cockpit by virtue of coating treatment to form a coated cockpit. The cockpit has the advantages of high surface hardness, translucency, good metal texture and difficulty in color losing.
Description
Technical field
The present invention relates to a kind of method for plating film on surface, particularly relate to a kind of aircraft cockpit method for plating film on surface.
Background technology
Now all consumer products are of a great variety on the market, and technique is had nothing in common with each other, and all attract clients with different-effects such as bright, bright-coloured, minute surface, half minute surfaces, consumer's eyeball, increase its desire to purchase.The transparent plastic material surface treatment such as PC, PMMA had the techniques such as spraying, Vacuum Deposition, optics plating in the past.Surface uses that spraying coating process is more difficult reaches semi-transparent effect, and metal sense is poor; Use its process flow of Vacuum Deposition technique more, as accomplished semi-transparent effect, its metal sense is poor, and color is bright-coloured not; Use optics depositing process, metal sense is comparatively strong, but transparency is higher, and color is dark not.In view of this, be necessary to be further improved above-mentioned film plating process.
Summary of the invention
Technical problem to be solved by this invention is: provide a kind of translucent, case hardness is high, and metal-like is good, the aircraft cockpit method for plating film on surface not easily faded.
In order to solve the problems of the technologies described above, the technical solution used in the present invention is: provide a kind of aircraft cockpit method for plating film on surface, comprise the steps:
S01, pretreatment, prepare the substrate material of manufacture aircraft cockpit and carry out toasting and continuing for some time;
S02, toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding;
S03, stiffened process is carried out to moulding, driving cabin moulding is put into hardening liquid and obtains driving cabin stiffened moulding after continuing for some time, and process is cured to driving cabin stiffened moulding;
S04, optical coating process, driving cabin moulding after stiffened process is put into optical coating station, and soild oxide is added in optical coating station, the outer surface making soild oxide be attached to driving cabin moulding through coating film treatment forms plated film driving cabin.
Beneficial effect of the present invention is: be different from film plating process of the prior art and adopt that surface spray coating process is more difficult reaches semi-transparent effect, and metal sense is poor or use its process flow of Vacuum Deposition technique more, as semi-transparent effect will be accomplished, its metal sense is poor or use optics depositing process, metal sense is stronger, but transparency is higher, the problem that color is dark not, the invention provides a kind of aircraft cockpit method for plating film on surface, adopt toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding, driving cabin moulding can be made to have translucent effect, adopt stiffened process, plastic surface defect can be modified, there is provided one smooth, smooth plane, be beneficial to optical coating process, and can case hardness be increased, improve surface adhesion force, adopt optical coating process, form film plating layer on the surface of driving cabin, increase metal-like.
Accompanying drawing explanation
Fig. 1 is the flow chart of a kind of aircraft cockpit method for plating film on surface of the present invention.
Detailed description of the invention
By describing technology contents of the present invention in detail, realized object and effect, accompanying drawing is coordinated to be explained below in conjunction with embodiment.
The design of most critical of the present invention is: adopt toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding, driving cabin moulding can be made to have translucent effect, adopt stiffened process, plastic surface defect can be modified, the plane that smooth, smooth is provided, is beneficial to optical coating process, and can case hardness be increased, improve surface adhesion force; Adopt optical coating process, form film plating layer on the surface of driving cabin, increase metal-like.
Please refer to Fig. 1, a kind of aircraft cockpit method for plating film on surface, comprises the steps:
S01, pretreatment, prepare the substrate material of manufacture aircraft cockpit and carry out toasting and continuing for some time;
S02, toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding; Injection moulding product is out translucent coloured effect, and concrete color can be mixed colours as required.
S03, stiffened process is carried out to moulding, driving cabin moulding is put into hardening liquid and obtains driving cabin stiffened moulding after continuing for some time, and process is cured to driving cabin stiffened moulding; Plastic surface defect is mainly modified in stiffened process, makes that product surface is smooth, smooth, hardness increases, be beneficial to optical coating process;
S04, optical coating process, driving cabin moulding after stiffened process is put into optical coating station, and soild oxide is added in optical coating station, the outer surface making soild oxide be attached to driving cabin moulding through coating film treatment forms plated film driving cabin.
From foregoing description, beneficial effect of the present invention is: be different from film plating process of the prior art and adopt that surface spray coating process is more difficult reaches semi-transparent effect, and metal sense is poor or use its process flow of Vacuum Deposition technique more, as semi-transparent effect will be accomplished, its metal sense is poor or use optics depositing process, metal sense is stronger, but transparency is higher, the problem that color is dark not, the invention provides a kind of aircraft cockpit method for plating film on surface, adopt toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding, driving cabin moulding can be made to have translucent effect, adopt stiffened process, plastic surface defect can be modified, there is provided one smooth, smooth plane, be beneficial to optical coating process, and can case hardness be increased, improve surface adhesion force, adopt optical coating process, form film plating layer on the surface of driving cabin, increase metal-like.
Further, before " driving cabin moulding being put into hardening liquid " in described step S03, also comprise the steps:
S31, Quenching Treatment, toast driving cabin moulding, and the temperature of baking is 70-75 DEG C, and the duration is 0.5h;
S32, Ultrasonic Cleaning process, utilize the surface of ultrasonic wave to the driving cabin moulding through Quenching Treatment to carry out first time cleaning treatment; Ultrasonic Cleaning process is utilized driving cabin moulding surface and oil contaminant, dirty, finger-marks, foreign material etc. to be washed.
S33, alcohol washes process, utilize alcohol to carry out second time cleaning treatment to the surface of driving cabin moulding.Alcohol washes process is utilized to be washed off by the organic impurities on driving cabin moulding surface.
Further, the substrate material in described step S01 is PC or PMMA.Iting is noted that except PC or PMMA material, can also be other similar material.
Further, in described step S01, be 4h to the time of substrate material baking, the baking temperature being PC to substrate material is 110 DEG C, and the baking temperature being PMMA to substrate material is 80 DEG C.Baking temperature can be different according to different Material selec-tion temperature.This raw material can be put into baking box during baking or oven toasts.
Further, in described step S03, the duration that driving cabin moulding puts into hardening liquid is 2min, and the temperature of hardening liquid is 18-23 DEG C.Wherein the concrete composition of hardening liquid is form primarily of late resin.
Further, in described step S03, the temperature that driving cabin stiffened moulding is cured process is 80-85 DEG C, and the duration is 2h.During solidification process driving cabin stiffened moulding put into baking box or oven toasts.
Further, in described step S04, the air pressure in described optical coating station is 0.02pa, and plated film electric current is 100A, and the plated film time is 0.5h, and the thickness of film plating layer is 10nm.Hardness after optical coating can reach more than 2H, meets hardness requirement, sustainable durable use.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every equivalents utilizing description of the present invention and accompanying drawing content to do, or be directly or indirectly used in relevant technical field, be all in like manner included in scope of patent protection of the present invention.
Claims (7)
1. an aircraft cockpit method for plating film on surface, is characterized in that, comprises the steps:
S01, pretreatment, prepare the substrate material of manufacture aircraft cockpit and carry out toasting and continuing for some time;
S02, toning injection process, add in substrate material after baking to inject in injection machine hopper after chromatic timing powder stirs and carry out toning injection moulding and obtain driving cabin moulding;
S03, stiffened process is carried out to moulding, driving cabin moulding is put into hardening liquid and obtains driving cabin stiffened moulding after continuing for some time, and process is cured to driving cabin stiffened moulding;
S04, optical coating process, driving cabin moulding after stiffened process is put into optical coating station, and soild oxide is added in optical coating station, the outer surface making soild oxide be attached to driving cabin moulding through coating film treatment forms plated film driving cabin.
2. a kind of aircraft cockpit method for plating film on surface according to claim 1, is characterized in that, before " driving cabin moulding being put into hardening liquid ", also comprises the steps: in described step S03
S31, Quenching Treatment, toast driving cabin moulding, and the temperature of baking is 70-75 DEG C, and the duration is 0.5h;
S32, Ultrasonic Cleaning process, utilize the surface of ultrasonic wave to the driving cabin moulding through Quenching Treatment to carry out first time cleaning treatment;
S33, alcohol washes process, utilize alcohol to carry out second time cleaning treatment to the surface of driving cabin moulding.
3. a kind of aircraft cockpit method for plating film on surface according to claim 1, is characterized in that, the substrate material in described step S01 is PC or PMMA.
4. a kind of aircraft cockpit method for plating film on surface according to claim 2, it is characterized in that, in described step S01, be 4h to the time of substrate material baking, the baking temperature being PC to substrate material is 110 DEG C, and the baking temperature being PMMA to substrate material is 80 DEG C.
5. a kind of aircraft cockpit method for plating film on surface according to claim 1, is characterized in that, in described step S03, the duration that driving cabin moulding puts into hardening liquid is 2min, and the temperature of hardening liquid is 18-23 DEG C.
6. a kind of aircraft cockpit method for plating film on surface according to claim 1, is characterized in that, in described step S03, the temperature that driving cabin stiffened moulding is cured process is 80-85 DEG C, and the duration is 2h.
7. a kind of aircraft cockpit method for plating film on surface according to claim 1, is characterized in that, in described step S04, the air pressure in described optical coating station is 0.02pa, and plated film electric current is 100A, and the plated film time is 0.5h, and the thickness of film plating layer is 10nm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410804649.9A CN104558652A (en) | 2014-12-22 | 2014-12-22 | Surface deposition method of cockpit for aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410804649.9A CN104558652A (en) | 2014-12-22 | 2014-12-22 | Surface deposition method of cockpit for aircraft |
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| CN104558652A true CN104558652A (en) | 2015-04-29 |
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| CN201410804649.9A Pending CN104558652A (en) | 2014-12-22 | 2014-12-22 | Surface deposition method of cockpit for aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107949203A (en) * | 2017-11-07 | 2018-04-20 | 北京小米移动软件有限公司 | Preparation method, housing and the electronic equipment of housing |
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| CN101561519A (en) * | 2009-03-27 | 2009-10-21 | 东莞劲胜精密组件股份有限公司 | Method for preparing high metallic texture high transmission lens |
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Application publication date: 20150429 |