CN107523176A - A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof - Google Patents
A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof Download PDFInfo
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- CN107523176A CN107523176A CN201710752847.9A CN201710752847A CN107523176A CN 107523176 A CN107523176 A CN 107523176A CN 201710752847 A CN201710752847 A CN 201710752847A CN 107523176 A CN107523176 A CN 107523176A
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- parts
- titanium alloy
- coating material
- plasticizer
- dispersant
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D161/00—Coating compositions based on condensation polymers of aldehydes or ketones; Coating compositions based on derivatives of such polymers
- C09D161/04—Condensation polymers of aldehydes or ketones with phenols only
- C09D161/06—Condensation polymers of aldehydes or ketones with phenols only of aldehydes with phenols
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/02—Elements
- C08K3/08—Metals
- C08K2003/0812—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/03—Polymer mixtures characterised by other features containing three or more polymers in a blend
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- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Wood Science & Technology (AREA)
- Organic Chemistry (AREA)
- Paints Or Removers (AREA)
Abstract
The invention discloses a kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof, includes following component according to mass fraction：10.5 15.5 parts of phenolic resin, 35 parts of polyethylene, 35 parts of organic siliconresin, 5 10 parts of aluminium powder, 35 parts of anticorrosive packing, 13 parts of lubricant, 36 parts of thixotropic agent, 13 parts of plasticizer, 1.5 2.5 parts of dispersant, 28 parts of solvent, a kind of Titanium Alloy Aircraft fastener coating material of the present invention, Titanium Alloy Aircraft fastener coating can have good intensity, toughness and greasy property, meet the requirement of fastener use environment, there is good stability.
Description
Technical field
The present invention relates to a kind of composite, in particular to a kind of Titanium Alloy Aircraft fastener coating material and its system
Preparation Method.
Background technology
Titanium alloy fastener has that in light weight, intensity is big, the excellent comprehensive performance such as antifatigue, corrosion-resistant, widely should
For each part of aircraft, however, titanium and aluminum be there is higher potential difference, when these parts are in the influence of medium
Under, it may occur that galvanic corrosion and cause to fail, it is therefore desirable to take safeguard procedures to ensure the security of aircraft flying for long time,
The development of present generation aircraft part proposes higher requirement to the heat-resisting of coating, toughness, greasy property, in the effect of higher condition
Under can cause former cated failure, currently without all good Titanium Alloy Aircraft fastener coating material of heat-resisting, toughness, lubricity
Material, therefore all good Titanium Alloy Aircraft fastener coating material of a kind of heat-resisting, toughness, lubricity is researched and developed as being badly in need of solving at present
The problem of.
The content of the invention
The invention provides a kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof.
To achieve the above object, the present invention provides following technical scheme：
A kind of Titanium Alloy Aircraft fastener coating material, include following component according to mass fraction：
Phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, aluminium powder 5-10 parts, anticorrosive packing 3-
5 parts, lubricant 1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts.
Further, following composition is included according to mass fraction：
10.5 parts of phenolic resin, 3 parts of polyethylene, 3 parts of organic siliconresin, 5 parts of aluminium powder, 3 parts of anticorrosive packing, 1 part of lubricant,
3 parts of thixotropic agent, 1 part of plasticizer, 1.5 parts of dispersant, 2 parts of solvent.
Further, following composition is included according to mass fraction：
13 parts of phenolic resin, 4 parts of polyethylene, 4 parts of organic siliconresin, 7 parts of aluminium powder, 4 parts of anticorrosive packing, 2 parts of lubricant, touch
Become 5 parts of agent, 2 parts of plasticizer, 2 parts of dispersant, 5 parts of solvent.
Further, following composition is included according to mass fraction：
15.5 parts of phenolic resin, 5 parts of polyethylene, 5 parts of organic siliconresin, 10 parts of aluminium powder, 5 parts of anticorrosive packing, lubricant 3
Part, 6 parts of thixotropic agent, 3 parts of plasticizer, 2.5 parts of dispersant, 8 parts of solvent.
Further, the preparation method of Titanium Alloy Aircraft fastener coating material, is comprised the following steps：
1) by phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, anticorrosive packing 3-5 parts, profit
Lubrication prescription 1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts are added in dispersion machine,
Disperse 20-30min under 1000~1500r/min rotating speed, obtain mixture A；
2) the mixture A that step 1 is stirred evenly is added into aluminium powder 5-10 parts, side edged disperses, at 190~220 DEG C
Coating is can obtain after 50~60min of lower solidification.
The beneficial effects of the invention are as follows：
1st, thermosetting is good.
2nd, there is more preferable stability.
Embodiment
Below in conjunction with the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described,
Obviously, described embodiment, only part of the embodiment of the present invention, rather than whole embodiments.Based in the present invention
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made,
Belong to the scope of protection of the invention.
Embodiment one：
A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof, include following component according to mass fraction：
Phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, aluminium powder 5-10 parts, anticorrosive packing 3-
5 parts, lubricant 1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts.
The preparation method of above-mentioned formula：
1) by phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, anticorrosive packing 3-5 parts, profit
Lubrication prescription 1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts are added in dispersion machine,
Disperse 20-30min under 1000~1500r/min rotating speed, obtain mixture A；
2) the mixture A that step 1 is stirred evenly is added into aluminium powder 5-10 parts, side edged disperses, at 190~220 DEG C
Coating is can obtain after 50~60min of lower solidification.
Embodiment two：
A kind of Titanium Alloy Aircraft fastener coating material includes following component according to mass fraction：
10.5 parts of phenolic resin, 3 parts of polyethylene, 3 parts of organic siliconresin, 5 parts of aluminium powder, 3 parts of anticorrosive packing, 1 part of lubricant,
3 parts of thixotropic agent, 1 part of plasticizer, 1.5 parts of dispersant, 2 parts of solvent.
Embodiment three：
A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof, include following composition according to mass fraction：
13 parts of phenolic resin, 4 parts of polyethylene, 4 parts of organic siliconresin, 7 parts of aluminium powder, 4 parts of anticorrosive packing, 2 parts of lubricant, touch
Become 5 parts of agent, 2 parts of plasticizer, 2 parts of dispersant, 5 parts of solvent.
Example IV：
A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof, include following composition according to mass fraction：
15.5 parts of phenolic resin, 5 parts of polyethylene, 5 parts of organic siliconresin, 10 parts of aluminium powder, 5 parts of anticorrosive packing, lubricant 3
Part, 6 parts of thixotropic agent, 3 parts of plasticizer, 2.5 parts of dispersant, 8 parts of solvent.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
1. a kind of Titanium Alloy Aircraft fastener coating material, include following component according to mass fraction：
Phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, aluminium powder 5-10 parts, anticorrosive packing 3-5 parts,
Lubricant 1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts.
2. a kind of Titanium Alloy Aircraft fastener coating material according to claim 1, according to mass fraction include as follows into
Point：
10.5 parts of phenolic resin, 3 parts of polyethylene, 3 parts of organic siliconresin, 5 parts of aluminium powder, 3 parts of anticorrosive packing, 1 part of lubricant, thixotroping
3 parts of agent, 1 part of plasticizer, 1.5 parts of dispersant, 2 parts of solvent.
3. a kind of Titanium Alloy Aircraft fastener coating material according to claim 1, according to mass fraction include as follows into
Point：
13 parts of phenolic resin, 4 parts of polyethylene, 4 parts of organic siliconresin, 7 parts of aluminium powder, 4 parts of anticorrosive packing, 2 parts of lubricant, thixotropic agent
5 parts, 2 parts of plasticizer, 2 parts of dispersant, 5 parts of solvent.
4. a kind of Titanium Alloy Aircraft fastener coating material according to claim 1, according to mass fraction include as follows into
Point：
15.5 parts of phenolic resin, 5 parts of polyethylene, 5 parts of organic siliconresin, 10 parts of aluminium powder, 5 parts of anticorrosive packing, 3 parts of lubricant, touch
Become 6 parts of agent, 3 parts of plasticizer, 2.5 parts of dispersant, 8 parts of solvent.
A kind of 5. preparation method of Titanium Alloy Aircraft fastener coating material as described in claim 1-4 is any, comprising as follows
Step：
1) by phenolic resin 10.5-15.5 parts, polyethylene 3-5 parts, organic siliconresin 3-5 parts, anticorrosive packing 3-5 parts, lubricant
1-3 parts, thixotropic agent 3-6 parts, plasticizer 1-3 parts, dispersant 1.5-2.5 parts, solvent 2-8 parts are added in dispersion machine, 1000~
Disperse 20-30min under 1500r/min rotating speed, obtain mixture A；
2) the mixture A that step 1 is stirred evenly is added into aluminium powder 5-10 parts, side edged disperses, solid at 190~220 DEG C
Coating is can obtain after changing 50~60min.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710752847.9A CN107523176A (en) | 2017-08-28 | 2017-08-28 | A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof |
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| CN201710752847.9A CN107523176A (en) | 2017-08-28 | 2017-08-28 | A kind of Titanium Alloy Aircraft fastener coating material and preparation method thereof |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110922845A (en) * | 2019-12-18 | 2020-03-27 | 南通达克罗新材料科技有限公司 | Preparation method of titanium alloy fastener coating material |
| CN111575749A (en) * | 2020-05-19 | 2020-08-25 | 苏州联桓汽车紧固件有限公司 | Surface coating treatment process of high-strength fastener |
-
2017
- 2017-08-28 CN CN201710752847.9A patent/CN107523176A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110922845A (en) * | 2019-12-18 | 2020-03-27 | 南通达克罗新材料科技有限公司 | Preparation method of titanium alloy fastener coating material |
| CN111575749A (en) * | 2020-05-19 | 2020-08-25 | 苏州联桓汽车紧固件有限公司 | Surface coating treatment process of high-strength fastener |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171229 |
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| WD01 | Invention patent application deemed withdrawn after publication |