CN112477320B - High-temperature-resistant composite board - Google Patents

High-temperature-resistant composite board Download PDF

Info

Publication number
CN112477320B
CN112477320B CN202011257733.5A CN202011257733A CN112477320B CN 112477320 B CN112477320 B CN 112477320B CN 202011257733 A CN202011257733 A CN 202011257733A CN 112477320 B CN112477320 B CN 112477320B
Authority
CN
China
Prior art keywords
parts
layer
temperature
resistant
fire
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.)
Active
Application number
CN202011257733.5A
Other languages
Chinese (zh)
Other versions
CN112477320A (en
Inventor
段佳巍
包行飞
克磊
陈雅露
李欣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangsu Entc Nuclear Technology Joint Stock Co ltd
Original Assignee
Jiangsu Entc Nuclear Technology Joint Stock Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiangsu Entc Nuclear Technology Joint Stock Co ltd filed Critical Jiangsu Entc Nuclear Technology Joint Stock Co ltd
Priority to CN202011257733.5A priority Critical patent/CN112477320B/en
Publication of CN112477320A publication Critical patent/CN112477320A/en
Application granted granted Critical
Publication of CN112477320B publication Critical patent/CN112477320B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B25/00Layered products comprising a layer of natural or synthetic rubber
    • B32B25/10Layered products comprising a layer of natural or synthetic rubber next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/14Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/18Layered products comprising a layer of metal comprising iron or steel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B25/00Layered products comprising a layer of natural or synthetic rubber
    • B32B25/20Layered products comprising a layer of natural or synthetic rubber comprising silicone rubber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L83/00Compositions of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon only; Compositions of derivatives of such polymers
    • C08L83/04Polysiloxanes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/20Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/206Insulating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • B32B2307/3065Flame resistant or retardant, fire resistant or retardant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/552Fatigue strength
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20Oxides; Hydroxides
    • C08K3/22Oxides; Hydroxides of metals
    • C08K2003/2227Oxides; Hydroxides of metals of aluminium
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L2201/00Properties
    • C08L2201/02Flame or fire retardant/resistant
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L2205/00Polymer mixtures characterised by other features
    • C08L2205/02Polymer mixtures characterised by other features containing two or more polymers of the same C08L -group
    • C08L2205/025Polymer 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Laminated Bodies (AREA)

Abstract

A high-temperature resistant composite board comprises a fire-resistant layer, a reinforcing layer and a metal board layer; the thickness of the metal plate layer is 0.3-0.5 mm; the refractory layer comprises: 100 parts of silicon rubber, 5-10 parts of methyl silicone oil, 5-15 parts of silicon carbide, 10-25 parts of aluminum oxide, 65-85 parts of silicon micropowder and 5-15 parts of phenyltributylketoxime silane, wherein 1-3 parts of a tin catalyst reinforcing layer is prepared by soaking high-temperature-resistant fiber mesh cloth in a high-temperature-resistant adhesive, and the thickness of the reinforcing layer is 1-2 mm. The high-temperature resistant adhesive has excellent high-temperature resistance, a hard ceramic body can be formed by the fire-resistant layer at the temperature of 400-500 ℃, the high-temperature resistant adhesive of the reinforcing layer can be hardened and transformed at the temperature of 800-900 ℃, and the high-temperature resistance is obviously improved to 1100-1200 ℃, so that the fire resistance is improved.

Description

High-temperature-resistant composite board
Technical Field
The invention relates to a high-temperature-resistant composite board.
Background
In the joints, openings or holes of electric cabinets, cable ducts, cable wells and buildings, wires, cables and various communication cables are often numerous and complicated. In case of fire, the fire rapidly spreads through the places, and the toxic gas is rapidly diffused. In particular, in the petrochemical industry, the hydrocarbon substances in the petrochemical industry are heated more quickly during combustion, and the deflagration phenomenon is easy to generate. Under the condition, the places are effectively blocked by the fireproof plates, so that the fire can be effectively controlled within a certain range, the loss is reduced, and valuable time is saved for fire extinguishment.
The existing fireproof plate mainly used uses rock wool as a base material, the highest bearing temperature of the fireproof plate is 700-800 ℃, and the strength of the plate is lower. When encountering impact generated by high temperature and deflagration, the fireproof plate can not meet the requirement of fireproof plugging.
Disclosure of Invention
Aiming at the problems, the invention provides a high-temperature-resistant composite board.
The specific technical scheme is as follows:
a high-temperature resistant composite board is characterized by comprising at least one layer of flame retardant coating, reinforcing layers arranged on two sides of the flame retardant coating and a metal board layer arranged on the outer side of each reinforcing layer; the number of the metal plate layers is at least two.
Further, the metal plate layer is one of a stainless steel plate and a galvanized steel plate, and the thickness of the metal plate layer is 0.3-0.5 mm.
Further, the flame retardant coating is made of an organic silicon material and comprises the following components in parts by mass:
100 parts of silicon rubber, 5-10 parts of methyl silicone oil, 5-15 parts of silicon carbide, 10-25 parts of aluminum oxide, 65-85 parts of silicon micropowder, 5-15 parts of phenyltributyl ketoxime silane and 1-3 parts of tin catalyst.
Further, the tin catalyst is one or more of dibutyltin dilaurate, dibutyltin diacetate and dibutyltin dioctoate.
Further, the thickness of the fire-resistant layer is 6-8 mm.
Furthermore, the reinforcing layer is made by soaking high-temperature resistant fiber mesh cloth in a high-temperature resistant adhesive, and the thickness of the reinforcing layer is 1-2 mm.
Furthermore, the high-temperature resistant adhesive of the reinforcing layer comprises the following components in parts by mass: 100 parts of silica sol, 2-5 parts of cellulose and 85-115 parts of aluminum oxide;
furthermore, the high-temperature resistant fiber mesh cloth of the reinforcing layer is calcium silicate fiber mesh cloth or aluminum silicate fiber mesh cloth.
The high-temperature-resistant composite board is characterized by comprising the following preparation methods:
(1) Preparing a reinforcing layer; stirring silica sol, cellulose and aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the high-temperature resistant fiber mesh cloth in a high-temperature resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 1-2 mm to obtain a reinforcing layer;
(2) Preparing a refractory layer; putting 107 silicon rubber, methyl silicone oil, silicon carbide, aluminum oxide and silicon micropowder into a high-temperature kneading machine for vacuum kneading for 30-50 min, adding phenyltributylketoxime silane for vacuum kneading for 15-20 min, finally adding a tin catalyst for vacuum kneading for 10-15 min, and discharging to obtain a flame retardant coating;
(3) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid, after the fire-resistant layer is evenly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
Compared with the prior art, the invention has the beneficial effects that:
the invention aims to overcome the defects of the traditional fireproof plugging plate and develops a high-temperature resistant composite plate, which takes an inorganic/organic composite fireproof layer and a metal plate as a base material. The composite board has the characteristics of fire impact resistance, high temperature resistance, long-acting effect, environmental protection and the like.
1. The high temperature resistance is excellent, the fire-resistant layer can form a hard ceramic body at 400-500 ℃, the high temperature resistant adhesive of the reinforcing layer can be hardened and transformed at 800-900 ℃, and the high temperature resistance is obviously improved to 1100-1200 ℃, so that the fire resistance is improved.
2. The plate has stable structure and can resist deflagration shock waves.
3. The cable and the pipeline are easy to pass through for the second time during installation, the operation is convenient, and the operation process is simplified;
4. no toxic gas is generated during combustion, the environment is protected, no pollution is caused, and the electric insulation, the oxidation resistance and the aging resistance are good;
drawings
FIG. 1 is a schematic cross-sectional view of the present invention.
Description of the reference numerals
A metal plate layer 1; a reinforcing layer 2; a refractory layer 4.
Detailed Description
In order to make the technical solution of the present invention clearer and more clear, the present invention is further described below, and any solution obtained by substituting technical features of the technical solution of the present invention with equivalents and performing conventional reasoning falls within the scope of the present invention.
The silicon rubber adopted by the embodiment of the invention is 107 silicon rubber, and the silica sol has the solubility of 40-45 wt%.
The cellulose used in the embodiments of the present invention is HHBR 250 hydroxyethyl cellulose.
Example 1
The preparation method of the high-temperature-resistant composite board comprises the following steps:
(1) Preparing a reinforcing layer: stirring 100 parts of silica sol with the solubility of 45wt%, 3 parts of cellulose and 95 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the calcium silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally drying, and soaking for multiple times until the thickness is 1mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a stainless steel plate with the thickness of 0.3mm as the metal plate layer;
(3) Preparing a refractory layer; 100 parts of silicon rubber, 5 parts of methyl silicone oil, 10 parts of silicon carbide, 20 parts of aluminum oxide and 65 parts of silicon micropowder are put into a high-temperature kneader for vacuum kneading for 45min, 8 parts of phenyltributylketoxime silane is added, vacuum kneading is carried out for 18min, finally 2 parts of dibutyltin dilaurate is added, and discharging is carried out after vacuum kneading is carried out for 15 min; obtaining a refractory layer with the thickness of 6mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid, after the fire-resistant layer is evenly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
Example 2
The preparation method of the high-temperature-resistant composite board comprises the following steps:
(1) Preparing a reinforcing layer: stirring 100 parts of silica sol with the solubility of 40wt%, 3 parts of cellulose and 85 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the aluminum silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 2mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a stainless steel plate with the thickness of 0.5mm as the metal plate layer;
(3) Preparing a refractory layer; 100 parts of silicon rubber, 10 parts of methyl silicone oil, 15 parts of silicon carbide, 10 parts of aluminum oxide and 70 parts of silicon micropowder are put into a high-temperature kneading machine for vacuum kneading for 30min, 5 parts of phenyltributyl ketoxime silane is added, vacuum kneading is carried out for 20min, finally 1 part of dibutyltin diacetate is added, and discharging is carried out after vacuum kneading is carried out for 12 min; obtaining a fire-resistant layer with the thickness of 8mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid thereon, after the fire-resistant layer is uniformly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
Example 3
The preparation method of the high-temperature-resistant composite board comprises the following steps:
(1) Preparing a reinforcing layer: stirring 100 parts of silica sol with the solubility of 43wt%, 5 parts of cellulose and 115 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the aluminum silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 1.5mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a galvanized steel plate with the thickness of 0.4mm as the metal plate layer;
(3) Preparing a refractory layer; 100 parts of silicon rubber, 7 parts of methyl silicone oil, 5 parts of silicon carbide, 25 parts of aluminum oxide and 85 parts of silicon micropowder are put into a high-temperature kneading machine for vacuum kneading for 50min, 15 parts of phenyltributyl ketoxime silane is added, vacuum kneading is carried out for 15min, finally 3 parts of dibutyltin dioctoate is added, and discharging is carried out after vacuum kneading is carried out for 10 min; obtaining a fire-resistant layer with the thickness of 7mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid thereon, after the fire-resistant layer is uniformly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
Example 4
The preparation method of the high-temperature-resistant composite board comprises the following steps:
(1) Preparing a reinforcing layer: stirring 100 parts of silica sol with the solubility of 43wt%, 5 parts of cellulose and 115 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the aluminum silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 2mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a galvanized steel plate with the thickness of 0.5mm as the metal plate layer;
(3) Preparing a refractory layer; 100 parts of silicon rubber, 7 parts of methyl silicone oil, 5 parts of silicon carbide, 25 parts of aluminum oxide and 85 parts of silicon micropowder are placed into a high-temperature kneading machine for vacuum kneading for 50min, 15 parts of phenyltributylketoxime silane is added, vacuum kneading is carried out for 15min, finally, 1 part of dibutyltin dilaurate and 2 parts of dibutyltin diacetate are added, and discharging is carried out after vacuum kneading is carried out for 10 min; obtaining a fire-resistant layer with the thickness of 7mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid, after the fire-resistant layer is evenly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
Example 5
The preparation method of the high-temperature-resistant composite board comprises the following steps:
(1) Preparing a reinforcing layer: stirring 100 parts of silica sol with the solubility of 40wt%, 2 parts of cellulose and 100 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the calcium silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally drying, and soaking for multiple times until the thickness is 1.5mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a galvanized steel plate with the thickness of 0.4mm as the metal plate layer;
(3) Preparing a refractory layer; 100 parts of silicon rubber, 5 parts of methyl silicone oil, 10 parts of silicon carbide, 15 parts of aluminum oxide and 76 parts of silicon micro powder are placed in a high-temperature kneading machine for vacuum kneading for 35min, 12 parts of phenyltributylketoxime silane is added, vacuum kneading is carried out for 13min, finally, 1 part of dibutyltin dioctoate and 1 part of dibutyltin diacetate are added, and discharging is carried out after vacuum kneading is carried out for 12 min; obtaining a fire-resistant layer with the thickness of 8mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming grinding tool with the metal plate layer and the reinforcing layer laid thereon, after the fire-resistant layer is uniformly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature resistant composite board is obtained after the hydraulic press is started for press forming.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that are within the spirit and principle of the present invention are intended to be included in the scope of the present invention.

Claims (3)

1. The high-temperature-resistant composite board is characterized by comprising the following preparation methods:
(1) Preparing a reinforcing layer, wherein the reinforcing layer comprises the following components in parts by mass: stirring 100 parts of silica sol with the solubility of 45wt%, 3 parts of cellulose and 95 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the calcium silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally drying, and soaking for multiple times until the thickness is 1mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a stainless steel plate with the thickness of 0.3mm as the metal plate layer;
(3) Preparing a refractory layer; according to the mass parts, 100 parts of silicone rubber, 5 parts of methyl silicone oil, 10 parts of silicon carbide, 20 parts of aluminum oxide and 65 parts of silicon micro powder are placed into a high-temperature kneading machine for vacuum kneading for 45min, 8 parts of phenyltributyl ketoxime silane is added, vacuum kneading is carried out for 18min, finally 2 parts of dibutyltin dilaurate is added, and discharging is carried out after vacuum kneading is carried out for 15 min; obtaining a refractory layer with the thickness of 6mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming die with the metal plate layer and the reinforcing layer laid, after the fire-resistant layer is evenly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature-resistant composite board is obtained after the hydraulic press is started for press forming.
2. The high-temperature-resistant composite board is characterized by comprising the following preparation methods:
(1) Preparing a reinforcing layer, wherein the reinforcing layer comprises the following components in parts by mass: stirring 100 parts of silica sol with the solubility of 40wt%, 3 parts of cellulose and 85 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the aluminum silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 2mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a stainless steel plate with the thickness of 0.5mm as the metal plate layer;
(3) Preparing a refractory layer; according to the mass parts, 100 parts of silicone rubber, 10 parts of methyl silicone oil, 15 parts of silicon carbide, 10 parts of aluminum oxide and 70 parts of silicon micropowder are placed into a high-temperature kneading machine for vacuum kneading for 30min, 5 parts of phenyltributyl ketoxime silane is added, vacuum kneading is carried out for 20min, finally 1 part of dibutyltin diacetate is added, and discharging is carried out after vacuum kneading is carried out for 12 min; obtaining a fire-resistant layer with the thickness of 8mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming die with the metal plate layer and the reinforcing layer laid, after the fire-resistant layer is evenly paved, the hydraulic press is started for press forming, then the metal plate layer and the reinforcing layer are laid, and the high-temperature-resistant composite board is obtained after the hydraulic press is started for press forming.
3. The high-temperature-resistant composite board is characterized by comprising the following preparation methods:
(1) Preparing a reinforcing layer, wherein the reinforcing layer comprises the following components in parts by mass: stirring 100 parts of silica sol with the solubility of 43wt%, 5 parts of cellulose and 115 parts of aluminum oxide, and uniformly stirring to obtain a high-temperature-resistant adhesive; soaking the aluminum silicate fiber mesh cloth in a high-temperature-resistant adhesive, naturally airing, and soaking for multiple times until the thickness is 1.5mm to obtain a reinforcing layer;
(2) Selecting a metal plate layer, and selecting a galvanized steel plate with the thickness of 0.4mm as the metal plate layer;
(3) Preparing a refractory layer; according to the mass parts, 100 parts of silicone rubber, 7 parts of methyl silicone oil, 5 parts of silicon carbide, 25 parts of aluminum oxide and 85 parts of silicon micropowder are placed into a high-temperature kneading machine for vacuum kneading for 50min, 15 parts of phenyltributyl ketoxime silane is added, vacuum kneading is carried out for 15min, finally 3 parts of dibutyltin dioctoate is added, and discharging is carried out after vacuum kneading is carried out for 10 min; obtaining a refractory layer with the thickness of 7mm;
(4) After the preparation of the fire-resistant layer is finished, the fire-resistant layer is rapidly placed into a hydraulic press forming die paved with the metal plate layer and the reinforcing layer, after the fire-resistant layer is evenly paved, the metal plate layer and the reinforcing layer are paved after the hydraulic press is started for press forming, and the high-temperature-resistant composite board is obtained after the hydraulic press is started for press forming.
CN202011257733.5A 2020-11-12 2020-11-12 High-temperature-resistant composite board Active CN112477320B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011257733.5A CN112477320B (en) 2020-11-12 2020-11-12 High-temperature-resistant composite board

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011257733.5A CN112477320B (en) 2020-11-12 2020-11-12 High-temperature-resistant composite board

Publications (2)

Publication Number Publication Date
CN112477320A CN112477320A (en) 2021-03-12
CN112477320B true CN112477320B (en) 2022-12-09

Family

ID=74929807

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011257733.5A Active CN112477320B (en) 2020-11-12 2020-11-12 High-temperature-resistant composite board

Country Status (1)

Country Link
CN (1) CN112477320B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203210695U (en) * 2013-03-26 2013-09-25 常州天晟新材料股份有限公司 Gelatinized fiberglass mesh for structural core material
CN105415816A (en) * 2015-12-29 2016-03-23 南京我乐家居股份有限公司 High temperature resistant and fireproof sheet material for producing cabinets
CN106633906A (en) * 2016-12-14 2017-05-10 湖北回天新材料股份有限公司 High-temperature-resistant deoximation single-ingredient room temperature vulcanized silicon rubber and preparation method thereof
CN108297507A (en) * 2017-12-29 2018-07-20 常州市沃科科技有限公司 A kind of superhigh temperature insulation heat shock resistance plate and its manufacturing method
CN108911576A (en) * 2018-06-22 2018-11-30 浙江阿路佑邦新材料科技有限公司 A2 grades of fireproof metal composite plates and its production method
CN109609067A (en) * 2018-12-13 2019-04-12 河北军辉安防科技股份有限公司 A kind of high-performance fire-resistant composite board and preparation method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203210695U (en) * 2013-03-26 2013-09-25 常州天晟新材料股份有限公司 Gelatinized fiberglass mesh for structural core material
CN105415816A (en) * 2015-12-29 2016-03-23 南京我乐家居股份有限公司 High temperature resistant and fireproof sheet material for producing cabinets
CN106633906A (en) * 2016-12-14 2017-05-10 湖北回天新材料股份有限公司 High-temperature-resistant deoximation single-ingredient room temperature vulcanized silicon rubber and preparation method thereof
CN108297507A (en) * 2017-12-29 2018-07-20 常州市沃科科技有限公司 A kind of superhigh temperature insulation heat shock resistance plate and its manufacturing method
CN108911576A (en) * 2018-06-22 2018-11-30 浙江阿路佑邦新材料科技有限公司 A2 grades of fireproof metal composite plates and its production method
CN109609067A (en) * 2018-12-13 2019-04-12 河北军辉安防科技股份有限公司 A kind of high-performance fire-resistant composite board and preparation method thereof

Also Published As

Publication number Publication date
CN112477320A (en) 2021-03-12

Similar Documents

Publication Publication Date Title
KR100566444B1 (en) Low Density Fire Barrier Material And Method Of Making
CN100370007C (en) Fire resistant polymeric compositions
CN112477320B (en) High-temperature-resistant composite board
KR101885583B1 (en) Binder composition, inorganic fiber insulator for refractory structure comprising the same and method for preparing inorganic fiber insulator
CN114249992B (en) Stepped melting high-temperature-resistant heat-insulating fireproof coating and preparation method and application thereof
CN107586415B (en) Rubber composite material capable of expanding under heat and being flame-retardant, and manufacturing method and application thereof
KR20170114930A (en) Core materials for building and method for manufacturing the same
CN114086678A (en) Fireproof heat-preservation rock wool board and preparation method thereof
CN102152553A (en) Method for processing silicon rubber composite material
CN116515299A (en) Ceramic silicon rubber composite material and preparation method and application thereof
KR102626994B1 (en) Non-combustible ceramic molded body for lightweight building interior and exterior materials and its manufacturing method
CN112175436B (en) Inorganic expansion type fire-proof paint
CN112778765A (en) Composite flame-retardant room-temperature vulcanized silicone rubber and preparation method thereof
EP1493543B1 (en) Method for manufacturing of non-combustible panels and non-combustible panels obtained thereby
CN209398272U (en) Spinning and weaving workshop heat-insulating flame-retardant fireproof door plate
CN211650823U (en) Heat exchanger and household appliance
CN111499315A (en) High-temperature-resistant fireproof material and preparation method and application thereof
CN118125753A (en) Plastic refractory heat insulation material and preparation method thereof
CN215106553U (en) Fireproof building board
CN113932609B (en) Silicon carbide furnace bottom structure
CN206142578U (en) Elevator manual -automatic switch
CN115073118B (en) Gypsum-based flame-retardant composite material and preparation method thereof
CN218814477U (en) Inorganic fiber composite flame-retardant heat-insulation belt
CN217634303U (en) Basalt fiber pipeline
CN216007522U (en) Homogeneous plate composite member

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
GR01 Patent grant
GR01 Patent grant