CN107964216A - A kind of press bolster composite material and preparation method thereof - Google Patents
A kind of press bolster composite material and preparation method thereof Download PDFInfo
- Publication number
- CN107964216A CN107964216A CN201711247646.XA CN201711247646A CN107964216A CN 107964216 A CN107964216 A CN 107964216A CN 201711247646 A CN201711247646 A CN 201711247646A CN 107964216 A CN107964216 A CN 107964216A
- Authority
- CN
- China
- Prior art keywords
- parts
- composite material
- powder
- press bolster
- preparation
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
- B29C39/02—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor for making articles of definite length, i.e. discrete articles
-
- 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
- C08K2201/00—Specific properties of additives
- C08K2201/002—Physical properties
- C08K2201/003—Additives being defined by their diameter
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/08—Stabilised against heat, light or radiation or oxydation
-
- 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
- C08L2205/02—Polymer mixtures characterised by other features containing two or more polymers of the same C08L -group
- C08L2205/025—Polymer mixtures characterised by other features containing two or more polymers of the same C08L -group containing two or more polymers of the same hierarchy C08L, and differing only in parameters such as density, comonomer content, molecular weight, structure
-
- 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
- C08L2205/035—Polymer mixtures characterised by other features containing three or more polymers in a blend containing four or more polymers in a blend
-
- 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
- C08L2205/14—Polymer mixtures characterised by other features containing polymeric additives characterised by shape
- C08L2205/16—Fibres; Fibrils
Abstract
The present invention provides a kind of press bolster composite material and preparation method thereof.Preparation method is as follows:Step 1:Glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic anhydride and isopropanol are mixed, heating stirring;Step 2:Gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl Aluminate and turpentine oil are mixed;Step 3:Filtering, is put into baking oven after being cleaned with deionized water and dries;Step 4:All components are mixed, is put into water-bath and stirs evenly;Step 5:Pour into mould, cure at room temperature;Step 6:The demoulding, is put into baking oven and cures;Step 7:Continue to cure 7 days at room temperature to obtain the final product.Material of the present invention has good mechanical property, and hot property is stablized, while has the damping performance of brilliance.
Description
Technical field
The present invention relates to mechanical material field, and in particular to a kind of press bolster composite material and preparation method thereof.
Background technology
Punching machine, is exactly a punching type forcing press, in national product, Sheet Metal Forming Technology due to being processed than tradition machinery for
Have and save material and the energy, it is efficient, it is not high to operator's technical requirements and by various mould applications can make machinery plus
These advantages of the product that work is unable to reach, thus its purposes is more and more extensive.At the same time, with the continuous hair of science and technology
Exhibition, requirement of the every profession and trade to mechanical equipment is also higher and higher, also higher and higher to the quality requirement of punching machine in itself, the table top of punching machine
It is exactly a portion, table top is mechanically operated main place, has very high want for its puncture and damping property
Ask.And used press bolster material is with manufacturing cycle is longer, damping vibration attenuation performance is poor, production can produce pollution etc. at present
Shortcoming, therefore, researchs and develops a kind of mechanical property is good and damping performance is good press bolster material for promoting whole mechanical row
The development of industry has great importance.
The content of the invention
Technical problems to be solved:The object of the present invention is to provide a kind of press bolster composite material, has good power
Performance is learned, hot property is stablized, while has the damping performance of brilliance.
Technical solution:A kind of press bolster composite material, is prepared by following component:30-50 parts of glycolylurea epoxide resin,
20-30 parts of phenolic resin, 5-10 parts of polymethylacrylic acid, 5-10 parts of gneiss powder, 10-15 parts of conglomerate powder, fiberglass 2-5
Part, 1-2 parts of copper ammonia fiber, 5-10 parts of silicon titanium valve, 2-5 parts of graphene, 1-2 parts of polyanion cellulose, isopropyl palmitate
0.4-0.8 parts, it is 0.2-0.4 parts of cetostearyl alcohol, 4-8 parts of distearyl acyl-oxygen isopropyl Aluminate, 2-5 parts of starch phosphate, poly-
Four 0.2-0.5 parts of fluorine ethylenes, 6-10 parts of diethylenetriamine, 4-8 parts of trimellitic anhydride, 5-10 parts of isopropanol, methylisothiozoline
0.1-0.3 parts of ketone, 50-70 parts of turpentine oil.
It is further preferred that a kind of press bolster composite material, is prepared by following component:Hydantoin epoxy tree
40 parts of fat, 25 parts of phenolic resin, 7.5 parts of polymethylacrylic acid, 7.5 parts of gneiss powder, 13 parts of conglomerate powder, fiberglass 3.5
Part, 1.5 parts of copper ammonia fiber, 7 parts of silicon titanium valve, 3 parts of graphene, 1.5 parts of polyanion cellulose, 0.6 part of isopropyl palmitate, whale
0.3 part of wax stearyl alcohol, 6 parts of distearyl acyl-oxygen isopropyl Aluminate, 4 parts of starch phosphate, 0.3 part of polytetrafluoroethylene, divinyl
8 parts of triamine, 6 parts of trimellitic anhydride, 7 parts of isopropanol, 0.2 part of methylisothiazolinone, 60 parts of turpentine oil.
Further, the gneiss powder and conglomerate powder diameter are 0.1-5mm.
The preparation method of above-mentioned press bolster composite material comprises the following steps:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 60-70 DEG C, stir 20-40min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
50-60min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80-90 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80-90 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 24-26h at 80-90 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
It is further preferred that 65 DEG C are heated in step 1, mixing time 30min.
It is further preferred that mixing time is 55min in step 2.
It is further preferred that temperature is 85 DEG C in step 6, time 25h.
Beneficial effect:The press bolster composite material of the present invention has good mechanical property, its compression strength highest can
Up to 154.2MPa, impact strength 80.7KJ/m2, thermal coefficient of expansion is low, and when in 90 DEG C of temperature, its thermal coefficient of expansion is minimum only
For 9.03 × 10-6/ DEG C, hot property is stablized, while its damping ratio has reached 0.42, has remarkable damping performance.
Embodiment
Embodiment 1
A kind of press bolster composite material, is prepared by following component:30 parts of glycolylurea epoxide resin, 20 parts of phenolic resin, gather
5 parts of methacrylic acid, 5 parts of gneiss powder, 10 parts of conglomerate powder, 2 parts of fiberglass, 1 part of copper ammonia fiber, 5 parts of silicon titanium valve, graphite
2 parts of alkene, 1 part of polyanion cellulose, 0.4 part of isopropyl palmitate, 0.2 part of cetostearyl alcohol, distearyl acyl-oxygen isopropyl aluminium
4 parts of acid esters, 2 parts of starch phosphate, 0.2 part of polytetrafluoroethylene, 6 parts of diethylenetriamine, 4 parts of trimellitic anhydride, 5 parts of isopropanol,
0.1 part of methylisothiazolinone, 50 parts of turpentine oil.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 60 DEG C, stir 20min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
50min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 24h at 80 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Embodiment 2
A kind of press bolster composite material, is prepared by following component:35 parts of glycolylurea epoxide resin, 25 parts of phenolic resin, gather
6 parts of methacrylic acid, 6 parts of gneiss powder, 11 parts of conglomerate powder, 3 parts of fiberglass, 1.5 parts of copper ammonia fiber, 6 parts of silicon titanium valve, stone
Black 3 parts of alkene, 1.5 parts of polyanion cellulose, 0.5 part of isopropyl palmitate, 0.3 part of cetostearyl alcohol, distearyl acyl-oxygen isopropyl
5 parts of base Aluminate, 3 parts of starch phosphate, 0.3 part of polytetrafluoroethylene, 7 parts of diethylenetriamine, 5 parts of trimellitic anhydride, isopropanol 6
Part, 0.2 part of methylisothiazolinone, 55 parts of turpentine oil.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 65 DEG C, stir 25min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
55min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 85 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 85 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 25h at 85 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Embodiment 3
A kind of press bolster composite material, is prepared by following component:40 parts of glycolylurea epoxide resin, 25 parts of phenolic resin, gather
7.5 parts of methacrylic acid, 7.5 parts of gneiss powder, 13 parts of conglomerate powder, 3.5 parts of fiberglass, 1.5 parts of copper ammonia fiber, silicon titanium valve
7 parts, 3 parts of graphene, 1.5 parts of polyanion cellulose, 0.6 part of isopropyl palmitate, 0.3 part of cetostearyl alcohol, distearyl
6 parts of oxygen isopropyl Aluminate, 4 parts of starch phosphate, 0.3 part of polytetrafluoroethylene, 8 parts of diethylenetriamine, 6 parts of trimellitic anhydride,
7 parts of isopropanol, 0.2 part of methylisothiazolinone, 60 parts of turpentine oil.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 65 DEG C, stir 30min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
55min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 85 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 85 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 25h at 85 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Embodiment 4
A kind of press bolster composite material, is prepared by following component:50 parts of glycolylurea epoxide resin, 30 parts of phenolic resin, gather
10 parts of methacrylic acid, 10 parts of gneiss powder, 15 parts of conglomerate powder, 5 parts of fiberglass, 2 parts of copper ammonia fiber, 10 parts of silicon titanium valve,
5 parts of graphene, 2 parts of polyanion cellulose, 0.8 part of isopropyl palmitate, 0.4 part of cetostearyl alcohol, distearyl acyl-oxygen isopropyl
8 parts of base Aluminate, 5 parts of starch phosphate, 0.5 part of polytetrafluoroethylene, 6-10 parts of diethylenetriamine, 8 parts of trimellitic anhydride, isopropyl
10 parts of alcohol, 0.3 part of methylisothiazolinone, 70 parts of turpentine oil.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 70 DEG C, stir 40min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
60min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 90 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 90 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 26h at 90 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Comparative example 1
Difference lies in do not contain gneiss powder and conglomerate powder with embodiment 1 for the present embodiment.Specifically:
A kind of press bolster composite material, is prepared by following component:30 parts of glycolylurea epoxide resin, 20 parts of phenolic resin, gather
5 parts of methacrylic acid, 2 parts of fiberglass, 1 part of copper ammonia fiber, 5 parts of silicon titanium valve, 2 parts of graphene, 1 part of polyanion cellulose, palm fibre
0.4 part of palmitic acid isopropyl propionate, 0.2 part of cetostearyl alcohol, 4 parts of distearyl acyl-oxygen isopropyl Aluminate, 2 parts of starch phosphate, poly- four
0.2 part of fluorine ethylene, 6 parts of diethylenetriamine, 4 parts of trimellitic anhydride, 5 parts of isopropanol, 0.1 part of methylisothiazolinone, turpentine oil
50 parts.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 60 DEG C, stir 20min;
Step 2:Fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl Aluminate and turpentine oil are mixed
Stir 50min;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 24h at 80 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Comparative example 2
Difference lies in do not contain fiberglass and copper ammonia fiber with embodiment 1 for the present embodiment.Specifically:
A kind of press bolster composite material, is prepared by following component:30 parts of glycolylurea epoxide resin, 20 parts of phenolic resin, gather
5 parts of methacrylic acid, 5 parts of gneiss powder, 10 parts of conglomerate powder, 5 parts of silicon titanium valve, 2 parts of graphene, polyanion cellulose 1
Part, 0.4 part of isopropyl palmitate, 0.2 part of cetostearyl alcohol, 4 parts of distearyl acyl-oxygen isopropyl Aluminate, 2 parts of starch phosphate,
0.2 part of polytetrafluoroethylene, 6 parts of diethylenetriamine, 4 parts of trimellitic anhydride, 5 parts of isopropanol, 0.1 part of methylisothiazolinone, pine
50 parts of fuel-economizing.
The preparation method of above-mentioned press bolster composite material is:
Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid
Acid anhydride and isopropanol mixing, are heated to 60 DEG C, stir 20min;
Step 2:By gneiss powder, conglomerate powder, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl Aluminate and turpentine oil
50min is mixed;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 24h at 80 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Comparative example 3
Difference lies in replace polymethylacrylic acid with phenolic resin with embodiment 1 for the present embodiment.Specifically:
A kind of press bolster composite material, is prepared by following component:30 parts of glycolylurea epoxide resin, 25 parts of phenolic resin, piece
5 parts of paragneiss powder, 10 parts of conglomerate powder, 2 parts of fiberglass, 1 part of copper ammonia fiber, 5 parts of silicon titanium valve, 2 parts of graphene, polyanion are fine
1 part of dimension element, 0.4 part of isopropyl palmitate, 0.2 part of cetostearyl alcohol, 4 parts of distearyl acyl-oxygen isopropyl Aluminate, starch phosphate
2 parts of ester, 0.2 part of polytetrafluoroethylene, 6 parts of diethylenetriamine, 4 parts of trimellitic anhydride, 5 parts of isopropanol, methylisothiazolinone 0.1
Part, 50 parts of turpentine oil.
The preparation method of above-mentioned press bolster composite material is:
Step 1:Glycolylurea epoxide resin, phenolic resin, starch phosphate, diethylenetriamine, trimellitic anhydride and isopropanol are mixed
Close, be heated to 60 DEG C, stir 20min;
Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl
50min is mixed in base Aluminate and turpentine oil;
Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80 DEG C of temperature;
Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80 DEG C of temperature;
Step 5:Pour into mould, when curing 24 is small at room temperature;
Step 6:The demoulding, is put into baking oven, cures 24h at 80 DEG C of temperature;
Step 7:Continue to cure 7 days at room temperature to obtain the final product.
Following table is the partial properties index of material of the present invention, it will be seen that material of the present invention has good mechanics
Performance, its compression strength reach as high as 154.2MPa, impact strength 80.7KJ/m2, thermal coefficient of expansion is low, when in 90 DEG C of temperature
When, its minimum thermal coefficient of expansion is only 9.03 × 10-6/ DEG C, hot property is stablized, while its damping ratio has reached 0.42, has Zhuo
Damping performance more.
The partial properties index of 1 press bolster composite material of table
Embodiment 1 | Embodiment 2 | Embodiment 3 | Embodiment 4 | Comparative example 1 | Comparative example 2 | Comparative example 3 | |
Compression strength(MPa) | 153.7 | 153.9 | 154.2 | 153.8 | 146.3 | 143.3 | 150.8 |
Impact strength(KJ/m2) | 80.2 | 80.4 | 80.7 | 80.6 | 76.4 | 74.1 | 76.9 |
Thermal coefficient of expansion × 10-6(/℃) | 9.13 | 9.10 | 9.03 | 9.07 | 9.56 | 9.72 | 9.53 |
Damping ratio | 0.37 | 0.39 | 0.42 | 0.39 | 0.37 | 0.36 | 0.31 |
Note:MEASURING THE THERMAL EXPANSION COEFFICIENT temperature is 90 DEG C.
Claims (7)
- A kind of 1. press bolster composite material, it is characterised in that:It is prepared by following component:30-50 parts of glycolylurea epoxide resin, 20-30 parts of phenolic resin, 5-10 parts of polymethylacrylic acid, 5-10 parts of gneiss powder, 10-15 parts of conglomerate powder, fiberglass 2-5 Part, 1-2 parts of copper ammonia fiber, 5-10 parts of silicon titanium valve, 2-5 parts of graphene, 1-2 parts of polyanion cellulose, isopropyl palmitate 0.4-0.8 parts, it is 0.2-0.4 parts of cetostearyl alcohol, 4-8 parts of distearyl acyl-oxygen isopropyl Aluminate, 2-5 parts of starch phosphate, poly- Four 0.2-0.5 parts of fluorine ethylenes, 6-10 parts of diethylenetriamine, 4-8 parts of trimellitic anhydride, 5-10 parts of isopropanol, methylisothiozoline 0.1-0.3 parts of ketone, 50-70 parts of turpentine oil.
- A kind of 2. press bolster composite material according to claim 1, it is characterised in that:By following component with parts by weight system It is standby to form:40 parts of glycolylurea epoxide resin, 25 parts of phenolic resin, 7.5 parts of polymethylacrylic acid, 7.5 parts of gneiss powder, conglomerate powder 13 parts of end, 3.5 parts of fiberglass, 1.5 parts of copper ammonia fiber, 7 parts of silicon titanium valve, 3 parts of graphene, 1.5 parts of polyanion cellulose, palm 0.6 part of isopropyl propionate, 0.3 part of cetostearyl alcohol, 6 parts of distearyl acyl-oxygen isopropyl Aluminate, 4 parts of starch phosphate, polytetrafluoro Second is 0.3 part dilute, 8 parts of diethylenetriamine, 6 parts of trimellitic anhydride, 7 parts of isopropanol, 0.2 part of methylisothiazolinone, turpentine oil 60 Part.
- A kind of 3. press bolster composite material as claimed in claim 1, it is characterised in that:The gneiss powder and conglomerate powder Last particle diameter is 0.1-5mm.
- A kind of 4. preparation method of press bolster composite material of claim 1 to 2 any one of them, it is characterised in that:Including Following steps:Step 1:By glycolylurea epoxide resin, phenolic resin, polymethylacrylic acid, starch phosphate, diethylenetriamine, trimellitic acid Acid anhydride and isopropanol mixing, are heated to 60-70 DEG C, stir 20-40min;Step 2:By gneiss powder, conglomerate powder, fiberglass, copper ammonia fiber, silicon titanium valve, graphene, distearyl acyl-oxygen isopropyl 50-60min is mixed in base Aluminate and turpentine oil;Step 3:Filtering, is put into baking oven after being cleaned with deionized water and is dried at 80-90 DEG C of temperature;Step 4:All components are mixed, is put into water-bath and is stirred evenly at 80-90 DEG C of temperature;Step 5:Pour into mould, when curing 24 is small at room temperature;Step 6:The demoulding, is put into baking oven, cures 24-26h at 80-90 DEG C of temperature;Step 7:Continue to cure 7 days at room temperature to obtain the final product.
- A kind of 5. preparation method of press bolster composite material according to claim 4, it is characterised in that:The step 1 In be heated to 65 DEG C, mixing time 30min.
- A kind of 6. preparation method of press bolster composite material according to claim 4, it is characterised in that:The step 2 Middle mixing time is 55min.
- A kind of 7. preparation method of press bolster composite material according to claim 4, it is characterised in that:The step 6 Middle temperature is 85 DEG C, time 25h.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711247646.XA CN107964216A (en) | 2017-12-01 | 2017-12-01 | A kind of press bolster composite material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711247646.XA CN107964216A (en) | 2017-12-01 | 2017-12-01 | A kind of press bolster composite material and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107964216A true CN107964216A (en) | 2018-04-27 |
Family
ID=61999399
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711247646.XA Pending CN107964216A (en) | 2017-12-01 | 2017-12-01 | A kind of press bolster composite material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107964216A (en) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105623196A (en) * | 2016-03-22 | 2016-06-01 | 苏州捷德瑞精密机械有限公司 | Composite material of metal cutting machine tool and preparation method for composite material |
-
2017
- 2017-12-01 CN CN201711247646.XA patent/CN107964216A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105623196A (en) * | 2016-03-22 | 2016-06-01 | 苏州捷德瑞精密机械有限公司 | Composite material of metal cutting machine tool and preparation method for composite material |
Non-Patent Citations (1)
Title |
---|
H.李: "《环氧树脂》", 31 December 1965, 中国工业出版社 * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105648830A (en) | Composite plant fiber aramid paper and preparation method thereof | |
CN106987123B (en) | Graphene/boron nitride loaded nano-silver heat-conducting special high polymer material and preparation method thereof | |
CN107674349A (en) | A kind of fluoropolymer composite of low-k and preparation method thereof | |
CN105255108A (en) | High-temperature-resistant epoxy resin mold and preparation method thereof | |
CN102936466A (en) | Modified bisphthalonitrile resin structure glue film and preparation method thereof | |
CN113861806A (en) | Low-temperature curing epoxy anticorrosive powder coating and preparation method thereof | |
CN107964216A (en) | A kind of press bolster composite material and preparation method thereof | |
CN106830969A (en) | A kind of preparation method of rigid chopped carbon fiber precast body | |
CN106589547A (en) | PE-RT (polyethylene of raised temperature resistance) floor heating pipe and production method and application thereof | |
CN108975322A (en) | The method for preparing graphene slurry | |
CN100415820C (en) | Process for preparing teflon expanded sealing plate used for space air vehicles | |
CN103554835A (en) | Method for preparing reinforcing epoxy resin material capable of being fast cured at medium/low temperature | |
CN103554511A (en) | Preparation method for polymer emulsifier | |
CN105440388A (en) | Heat-preservation heat-insulation rubber plate and preparation method thereof | |
CN102876255A (en) | Method for preparing modified maize starch glue | |
CN105001750A (en) | Inner-wall coating for slurry pump and preparation method thereof | |
CN112143145B (en) | Low dielectric loss type polytetrafluoroethylene microwave board and preparation method thereof | |
CN106045516A (en) | Process for preparing environment-friendly lignin ceramics | |
CN107955323A (en) | A kind of friction material and preparation method thereof | |
KR102140469B1 (en) | Method for manufacturing electromagnetic wave shielding material using acid-treated carbon nanotube/pitch carbon paper | |
RU2584013C1 (en) | Nano-modified epoxy binder for composite materials | |
CN106279922A (en) | A kind of Environment-friendlyplastic plastic wood composite pallet and preparation method thereof | |
CN102153708B (en) | Vacuum pressure impregnating resin based on interpenetrating network technology and preparation method thereof | |
CN108395751A (en) | A kind of preparation method of mechanical equipment weatherability coating | |
CN114381107B (en) | SMC composite sheet for pig house leak boards and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180427 |
|
WD01 | Invention patent application deemed withdrawn after publication |