CN104927569A - High-hardness paint for pneumatic elements - Google Patents
High-hardness paint for pneumatic elements Download PDFInfo
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- CN104927569A CN104927569A CN201510311064.8A CN201510311064A CN104927569A CN 104927569 A CN104927569 A CN 104927569A CN 201510311064 A CN201510311064 A CN 201510311064A CN 104927569 A CN104927569 A CN 104927569A
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- parts
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- silane
- hardness
- pneumatic element
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Abstract
The invention discloses high-hardness paint for pneumatic elements. The paint comprises raw materials in parts by mass as follows: 35-55 parts of epoxy resin, 10-15 parts of a diluent, 0.5-2 parts of a silane coupling agent, 15-20 parts of a curing agent, 2-3 parts of nano cerium oxide, 10-13 parts of a prepolymer, 15-23 parts of silane modified fine-mesh corundum, 20-35 parts of first polyester and 1-2 parts of hydroquinone. The high-hardness paint for the pneumatic elements has high hardness, good durability, better rubbing resistance and better adhesion.
Description
Technical field
The present invention relates to pneumatic element field of material technology, especially, relate to a kind of high rigidity pneumatic element coating.
Background technology
How pneumatic element shell, throughout the year by sun exposure, makes industrial machinery shell more durable, and to have more gloss be the problem that field of industrial machinery needs to solve at present.There is difference of hardness, poor durability, scuff degree difference and put forth effort the problems such as too late in current coating used.
Summary of the invention
The object of the invention is to provide a kind of high rigidity pneumatic element coating, there is difference of hardness, poor durability, scuff degree difference to solve coating in prior art and puts forth effort too late problem.
For achieving the above object, the invention provides a kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction:
Epoxy resin 35 ~ 55 parts;
Thinner 10 ~ 15 parts;
Silane coupling agent 0.5 ~ 2 part;
15 ~ 20 parts, solidifying agent;
Nano ceric oxide 2 ~ 3 parts;
Performed polymer 10 ~ 13 parts;
15 ~ 23 parts, silane-modified detailed catalogue corundum;
First polyester 20 ~ 35 parts; And
Resorcinol 1 ~ 2 part.
Further, the invention provides a kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction: epoxy resin 35 parts; Thinner 10 parts; Silane coupling agent 1 part; 15 parts, solidifying agent; Nano ceric oxide 2 parts; Performed polymer 10 parts; 18 parts, silane-modified detailed catalogue corundum; First polyester 25 parts; And Resorcinol 1 part.
Further, the invention provides a kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction: epoxy resin 55 parts; Thinner 15 parts; Silane coupling agent 2 parts; 20 parts, solidifying agent; Nano ceric oxide 3 parts; Performed polymer 13 parts; 23 parts, silane-modified detailed catalogue corundum; First polyester 35 parts; And Resorcinol 2 parts.
The present invention has following beneficial effect: the invention provides a kind of high rigidity pneumatic element coating, hardness is strong, wearing quality good, and scuff degree and coating are puted forth effort relatively good.
Embodiment
A kind of high rigidity pneumatic element coating that this preferred embodiment provides, its specific implementation process is as follows:
A kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction:
Epoxy resin 35 ~ 55 parts;
Thinner 10 ~ 15 parts;
Silane coupling agent 0.5 ~ 2 part;
15 ~ 20 parts, solidifying agent;
Nano ceric oxide 2 ~ 3 parts;
Performed polymer 10 ~ 13 parts;
15 ~ 23 parts, silane-modified detailed catalogue corundum;
First polyester 20 ~ 35 parts; And
Resorcinol 1 ~ 2 part.
Embodiment 1:
The invention provides a kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction: epoxy resin 35 parts; Thinner 10 parts; Silane coupling agent 1 part; 15 parts, solidifying agent; Nano ceric oxide 2 parts; Performed polymer 10 parts; 18 parts, silane-modified detailed catalogue corundum; First polyester 25 parts; And Resorcinol 1 part.
Embodiment 2:
The invention provides a kind of high rigidity pneumatic element coating, wherein, this coating is made up of the raw material of following massfraction: epoxy resin 55 parts; Thinner 15 parts; Silane coupling agent 2 parts; 20 parts, solidifying agent; Nano ceric oxide 3 parts; Performed polymer 13 parts; 23 parts, silane-modified detailed catalogue corundum; First polyester 35 parts; And Resorcinol 2 parts.
As can be seen from the above description, the above embodiments of the present invention achieve following technique effect:
The invention provides a kind of high rigidity pneumatic element coating, hardness is strong, wearing quality good, and scuff degree and coating are puted forth effort relatively good.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention; For a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.
Claims (3)
1. a high rigidity pneumatic element coating, is characterized in that, this coating is made up of the raw material of following massfraction:
Epoxy resin 35 ~ 55 parts;
Thinner 10 ~ 15 parts;
Silane coupling agent 0.5 ~ 2 part;
15 ~ 20 parts, solidifying agent;
Nano ceric oxide 2 ~ 3 parts;
Performed polymer 10 ~ 13 parts;
15 ~ 23 parts, silane-modified detailed catalogue corundum;
First polyester 20 ~ 35 parts; And
Resorcinol 1 ~ 2 part.
2. a kind of high rigidity pneumatic element coating according to claim 1, is characterized in that: this coating is made up of the raw material of following massfraction: epoxy resin 35 parts; Thinner 10 parts; Silane coupling agent 1 part; 15 parts, solidifying agent; Nano ceric oxide 2 parts; Performed polymer 10 parts; 18 parts, silane-modified detailed catalogue corundum; First polyester 25 parts; And Resorcinol 1 part.
3. a kind of high rigidity pneumatic element coating according to claim 1, is characterized in that: this coating is made up of the raw material of following massfraction: epoxy resin 55 parts; Thinner 15 parts; Silane coupling agent 2 parts; 20 parts, solidifying agent; Nano ceric oxide 3 parts; Performed polymer 13 parts; 23 parts, silane-modified detailed catalogue corundum; First polyester 35 parts; And Resorcinol 2 parts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510311064.8A CN104927569A (en) | 2015-06-09 | 2015-06-09 | High-hardness paint for pneumatic elements |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510311064.8A CN104927569A (en) | 2015-06-09 | 2015-06-09 | High-hardness paint for pneumatic elements |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104927569A true CN104927569A (en) | 2015-09-23 |
Family
ID=54115005
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510311064.8A Pending CN104927569A (en) | 2015-06-09 | 2015-06-09 | High-hardness paint for pneumatic elements |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104927569A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108264788A (en) * | 2017-12-19 | 2018-07-10 | 苏州牛麦田新材料科技有限公司 | A kind of anticorrosion coating material and preparation method thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110086174A1 (en) * | 2009-10-12 | 2011-04-14 | Han To Industry Co., Ltd | Paint composition including nano-ceramic and polymer resin against neutralization and salt damage of concrete and method for waterproof and anticorrosion using the same |
| CN102417786A (en) * | 2011-09-30 | 2012-04-18 | 杭州市萧山区党山新世纪装饰卫浴研发中心 | Nano-modified man-made stone surface composite functional coating material |
| CN102898913A (en) * | 2012-10-24 | 2013-01-30 | 江苏纽克莱涂料有限公司 | Aqueous inorganic zinc rich paint |
| CN103290401A (en) * | 2013-05-10 | 2013-09-11 | 安徽工业大学 | Chromium-free self-lubricating passivation solution and preparation method thereof |
| CN104449237A (en) * | 2014-12-14 | 2015-03-25 | 天津美士邦涂料化工有限公司 | Epoxy wear-resistant coating |
-
2015
- 2015-06-09 CN CN201510311064.8A patent/CN104927569A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110086174A1 (en) * | 2009-10-12 | 2011-04-14 | Han To Industry Co., Ltd | Paint composition including nano-ceramic and polymer resin against neutralization and salt damage of concrete and method for waterproof and anticorrosion using the same |
| CN102417786A (en) * | 2011-09-30 | 2012-04-18 | 杭州市萧山区党山新世纪装饰卫浴研发中心 | Nano-modified man-made stone surface composite functional coating material |
| CN102898913A (en) * | 2012-10-24 | 2013-01-30 | 江苏纽克莱涂料有限公司 | Aqueous inorganic zinc rich paint |
| CN103290401A (en) * | 2013-05-10 | 2013-09-11 | 安徽工业大学 | Chromium-free self-lubricating passivation solution and preparation method thereof |
| CN104449237A (en) * | 2014-12-14 | 2015-03-25 | 天津美士邦涂料化工有限公司 | Epoxy wear-resistant coating |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108264788A (en) * | 2017-12-19 | 2018-07-10 | 苏州牛麦田新材料科技有限公司 | A kind of anticorrosion coating material and preparation method thereof |
| CN108264788B (en) * | 2017-12-19 | 2020-09-29 | 南京悠谷知识产权服务有限公司 | Anticorrosive coating material and preparation method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150923 |