CN113698886A - Aerogel composite material for cooling ship pipeline and preparation method thereof - Google Patents

Aerogel composite material for cooling ship pipeline and preparation method thereof Download PDF

Info

Publication number
CN113698886A
CN113698886A CN202111023643.4A CN202111023643A CN113698886A CN 113698886 A CN113698886 A CN 113698886A CN 202111023643 A CN202111023643 A CN 202111023643A CN 113698886 A CN113698886 A CN 113698886A
Authority
CN
China
Prior art keywords
aerogel
layer
film
powder
composite material
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
Application number
CN202111023643.4A
Other languages
Chinese (zh)
Inventor
张忠伦
王明铭
辛志军
李桂金
刘振森
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.)
China Building Materials Science Innovation Technology Research Institute Shandong Co ltd
Original Assignee
China Building Materials Science Innovation Technology Research Institute Shandong 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 China Building Materials Science Innovation Technology Research Institute Shandong Co ltd filed Critical China Building Materials Science Innovation Technology Research Institute Shandong Co ltd
Priority to CN202111023643.4A priority Critical patent/CN113698886A/en
Publication of CN113698886A publication Critical patent/CN113698886A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00Adhesives in the form of films or foils
    • C09J7/20Adhesives in the form of films or foils characterised by their carriers
    • C09J7/29Laminated material
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/18Manufacture of films or sheets
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J163/00Adhesives based on epoxy resins; Adhesives based on derivatives of epoxy resins
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00Adhesives in the form of films or foils
    • C09J7/30Adhesives in the form of films or foils characterised by the adhesive composition
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2323/00Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers
    • C08J2323/02Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers not modified by chemical after treatment
    • C08J2323/04Homopolymers or copolymers of ethene
    • C08J2323/06Polyethene
    • 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
    • C08K2003/2217Oxides; Hydroxides of metals of magnesium
    • C08K2003/2224Magnesium hydroxide
    • 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
    • C08K2003/2237Oxides; Hydroxides of metals of titanium
    • C08K2003/2241Titanium dioxide
    • 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
    • C08K3/2279Oxides; Hydroxides of metals of antimony
    • 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
    • C08K7/00Use of ingredients characterised by shape
    • C08K7/22Expanded, porous or hollow particles
    • C08K7/24Expanded, porous or hollow particles inorganic
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/10Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet
    • C09J2301/12Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet by the arrangement of layers
    • C09J2301/122Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet by the arrangement of layers the adhesive layer being present only on one side of the carrier, e.g. single-sided adhesive tape
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/10Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet
    • C09J2301/16Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet by the structure of the carrier layer
    • C09J2301/162Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive tape or sheet by the structure of the carrier layer the carrier being a laminate constituted by plastic layers only
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2423/00Presence of polyolefin
    • C09J2423/04Presence of homo or copolymers of ethene
    • C09J2423/046Presence of homo or copolymers of ethene in the substrate
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2463/00Presence of epoxy resin

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Laminated Bodies (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Abstract

The invention relates to the technical field of aerogel, in particular to an aerogel composite material for cooling ship pipelines and a preparation method thereof. The aerogel composite material consists of an aerogel layer and a glue film, wherein the aerogel layer is prepared by mixing alumina aerogel with better heat insulation and cold insulation properties and polyethylene resin; the adhesive film comprises an adhesive layer and a film layer, wherein the adhesive layer is prepared by mixing epoxy resin and water-based acrylic acid, and the film layer comprises the following raw materials: polyethylene resin, fire-retardant powder, filler powder and tinting powder, in this marine pipeline keeps warm aerogel combined material and the preparation method, with viscose layer, aerogel layer and rete surface melting and blending, thereby form multilayer aerogel combined material, viscose layer can laminate with the pipeline lateral wall, but higher cohesiveness anti-drop, the rete can be used to viscose layer, aerogel layer protects, has higher intensity and toughness, and aerogel layer has the cold-proof effect, intensity and toughness are higher than ordinary aerogel simultaneously.

Description

Aerogel composite material for cooling ship pipeline and preparation method thereof
Technical Field
The invention relates to the technical field of aerogel, in particular to an aerogel composite material for cooling ship pipelines and a preparation method thereof.
Background
The ship pipeline is used for connecting various mechanical equipment on a ship and is used for conveying related working media such as water, oil, gas and the like; therefore, the aerogel material is needed to cool the pipeline; the aerogel is a light solid material which is formed by accumulating nano-scale particles and has nano-scale holes, has extremely high porosity and specific surface area, extremely low density and solid content, chemical inertness and incombustibility, shows excellent characteristics of light weight, heat preservation, heat insulation, fire prevention, sound insulation, shock absorption and energy absorption, and can be widely applied to military fields of national defense and military industry, security and antiterrorism and the like and civil fields of green buildings, heat transmission, public transportation, financial equipment protection and the like.
The general toughness of current aerogel is relatively poor, and intensity is low, when being applied to the pipeline surface, though can play cold insulation effect, nevertheless very easily suffer to break and damage, consequently needs a neotype aerogel combined material to improve prior art not enough.
Disclosure of Invention
The invention aims to provide an aerogel composite material for cooling ship pipelines and a preparation method thereof, so as to solve the problems in the background technology.
In order to achieve the above object, in one aspect, the present invention provides an aerogel composite material for cooling marine pipelines, the aerogel composite material is composed of an aerogel layer and a glue film, the aerogel layer is prepared by mixing alumina aerogel with good heat insulation and cold insulation properties and polyethylene resin;
the adhesive film comprises an adhesive layer and a film layer, wherein the adhesive layer is prepared by mixing epoxy resin and water-based acrylic acid, and the film layer comprises the following raw materials: 40-60% of polyethylene resin, 1-5% of flame-retardant powder, 20-30% of filler powder and 1-5% of coloring powder.
As a further improvement of the technical scheme, the flame-retardant powder is formed by mixing gas-phase antimony trioxide and gas-phase magnesium hydroxide in a ratio of 1:1, and the gas-phase flame-retardant powder is mixed with the adhesive film material, so that the flame retardance of the adhesive film is improved, and the strength of the adhesive film is improved.
As a further improvement of the technical scheme, the filler powder is selected from one or more of glass fiber, asbestos, diatomite, perlite powder, cork powder, talcum powder and calcium carbonate, and the added filler powder can not only enhance the toughness of the adhesive film, but also improve the heat insulation property of the adhesive film.
As a further improvement of the technical scheme, the coloring powder is selected from gas-phase titanium dioxide, is used for coloring the adhesive film and has a certain heat insulation effect.
In another aspect, the present invention provides a method for preparing the aerogel composite material for cooling ship pipelines, comprising the following steps:
s1, adding the alumina aerogel powder and the polyethylene resin into a stirring kettle, and heating and uniformly mixing to obtain a mixture;
s2, adding epoxy resin into a stirring kettle, heating and melting, adding water-based acrylic acid into the solution according to a proportion, mixing and stirring to obtain a glue solution;
s3, adding polyethylene resin into a stirring kettle for melting, then sequentially adding flame retardant powder, filler and dispersant for stirring and mixing, and then adding coloring powder for coloring to obtain a film material;
s4, respectively extruding the mixture, the glue solution and the film material through a film blowing machine to obtain an aerogel layer, a glue layer and a film layer;
and S5, downwards arranging the adhesive layer, sequentially laying the aerogel layer and the film layer, heating at high temperature to melt and blend the surfaces of the adhesive layer, the aerogel layer and the film layer, and finally flattening by a roller press to obtain the aerogel composite material.
Preferably, in S1, the mixing ratio of the alumina aerogel and the polyethylene resin is 1: 1.5.
Preferably, in S2, the mixing ratio of the epoxy resin to the aqueous acrylic acid is 2: 1.
Preferably, in the S4, the thickness of the aerogel layer is 0.03 to 0.05mm, the thickness of the glue layer is 0.05 to 0.1mm, and the thickness of the film layer is 0.2 to 0.3 mm.
Preferably, in the S5, the heating temperature is 300-1000 ℃.
Preferably, in the S5, the film pressing speed of the roller press is 0.5-1.0 m/S.
Compared with the prior art, the invention has the beneficial effects that:
in this marine pipeline keeps cold and uses aerogel combined material and preparation method, with viscose layer, aerogel layer and rete surface melting and blending to form multilayer aerogel combined material, the viscose layer can laminate with the pipeline lateral wall, but higher cohesiveness anti-drop, the rete can be used to protect viscose layer, aerogel layer, has higher intensity and toughness, and aerogel layer has the cold-keeping effect, and intensity and toughness are higher than ordinary aerogel simultaneously.
Drawings
FIG. 1 is an overall flow diagram of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Embodiment 1 a aerogel composite material for cooling ship pipelines and a preparation method thereof, including:
1. adding the alumina aerogel powder and the polyethylene resin into a stirring kettle according to the proportion of 1:1.5, and heating and uniformly mixing to obtain a mixture;
2. adding epoxy resin into a stirring kettle, heating and melting, adding aqueous acrylic acid into the solution according to the ratio of 2:1, and mixing and stirring to obtain a glue solution;
3. adding 60% of polyethylene resin into a stirring kettle for melting, then sequentially adding 1% of flame retardant powder, 20% of filler and a dispersing agent, stirring and mixing, and then adding 3% of coloring powder for coloring to prepare a film material;
4. respectively extruding the mixture, the glue solution and the film material through a film blowing machine to prepare an aerogel layer, an adhesive layer and a film layer, wherein the thickness of the aerogel layer is 0.03-0.05mm, the thickness of the adhesive layer is 0.05-0.1 mm, and the thickness of the film layer is 0.2-0.3 mm;
5. and (3) downwards arranging the adhesive layer, sequentially laying the aerogel layer and the film layer, heating to 300-1000 ℃ to melt and blend the surfaces of the adhesive layer, the aerogel layer and the film layer, and finally flattening by using a roller press to obtain the aerogel composite material, wherein the film pressing speed of the roller press is 0.5-1.0 m/S.
Embodiment 2 a marine pipeline cold insulation aerogel composite material and a preparation method thereof, including:
1. adding the alumina aerogel powder and the polyethylene resin into a stirring kettle according to the proportion of 1:1.5, and heating and uniformly mixing to obtain a mixture;
2. adding epoxy resin into a stirring kettle, heating and melting, adding aqueous acrylic acid into the solution according to the ratio of 2:1, and mixing and stirring to obtain a glue solution;
3. adding 50% of polyethylene resin into a stirring kettle for melting, then sequentially adding 3% of flame retardant powder, 25% of filler and a dispersing agent, stirring and mixing, and then adding 3% of coloring powder for coloring to prepare a film material;
4. respectively extruding the mixture, the glue solution and the film material through a film blowing machine to prepare an aerogel layer, an adhesive layer and a film layer, wherein the thickness of the aerogel layer is 0.03-0.05mm, the thickness of the adhesive layer is 0.05-0.1 mm, and the thickness of the film layer is 0.2-0.3 mm;
5. and (3) downwards arranging the adhesive layer, sequentially laying the aerogel layer and the film layer, heating to 300-1000 ℃ to melt and blend the surfaces of the adhesive layer, the aerogel layer and the film layer, and finally flattening by using a roller press to obtain the aerogel composite material, wherein the film pressing speed of the roller press is 0.5-1.0 m/S.
Embodiment 3 a marine pipeline cold insulation aerogel composite material and a preparation method thereof, including:
1. adding the alumina aerogel powder and the polyethylene resin into a stirring kettle according to the proportion of 1:1.5, and heating and uniformly mixing to obtain a mixture;
2. adding epoxy resin into a stirring kettle, heating and melting, adding aqueous acrylic acid into the solution according to the ratio of 2:1, and mixing and stirring to obtain a glue solution;
3. adding 40% of polyethylene resin into a stirring kettle for melting, then sequentially adding 5% of flame retardant powder, 30% of filler and dispersant, stirring and mixing, and then adding 5% of coloring powder for coloring to obtain a film material;
4. respectively extruding the mixture, the glue solution and the film material through a film blowing machine to prepare an aerogel layer, an adhesive layer and a film layer, wherein the thickness of the aerogel layer is 0.03-0.05mm, the thickness of the adhesive layer is 0.05-0.1 mm, and the thickness of the film layer is 0.2-0.3 mm;
5. and (3) downwards arranging the adhesive layer, sequentially laying the aerogel layer and the film layer, heating to 300-1000 ℃ to melt and blend the surfaces of the adhesive layer, the aerogel layer and the film layer, and finally flattening by using a roller press to obtain the aerogel composite material, wherein the film pressing speed of the roller press is 0.5-1.0 m/S.
In the above examples 1-3, the flame retardant powder is a mixture of gaseous antimony trioxide and gaseous magnesium hydroxide at a ratio of 1:1, and the flame retardant powder is mixed with the adhesive film material to improve the flame retardancy and strength of the adhesive film;
the filler powder is selected from one or more of glass fiber, asbestos, diatomite, perlite powder, cork powder, talcum powder and calcium carbonate, and the added filler powder can not only enhance the toughness of the adhesive film, but also improve the heat insulation property of the adhesive film;
the coloring powder is selected from gas-phase titanium dioxide, is used for coloring the adhesive film and has a certain heat insulation effect.
The indexes of the aerogel composite material for cold insulation of the ship pipeline prepared by the invention are shown in table 1:
TABLE 1
Compressive strength (Mpa) Breaking strength (Mpa) Coefficient of thermal conductivity (W/m. K) Tensile bond Strength (Mpa) Peel strength (Mpa)
Example 1 3.2 2.4 0.035 69 23
Example 2 3.5 2.9 0.033 74 27
Example 3 3.3 2.6 0.033 71 24
As shown in Table 1, the aerogel composites for cooling ship pipelines, prepared in examples 1 to 3 of the present invention, all had good strength and toughness, and at the same time, had excellent cooling performance.
Comparative example 1 an aerogel composite and method of making, comprising:
1. adding the alumina aerogel powder and the polyethylene resin into a stirring kettle according to the proportion of 1:1.5, and heating and uniformly mixing to obtain a mixture;
2. adding epoxy resin into a stirring kettle, heating and melting, adding aqueous acrylic acid into the solution according to the ratio of 2:1, and mixing and stirring to obtain a glue solution;
3. respectively extruding the mixture and the glue solution through a film blowing machine to prepare an aerogel layer and an adhesive layer, wherein the thickness of the aerogel layer is 0.03-0.05mm, and the thickness of the adhesive layer is 0.05-0.1 mm;
4. and (3) downwards placing the adhesive layer, laying the aerogel layer, melting and blending the surfaces of the adhesive layer and the aerogel layer by heating at the temperature of 300-1000 ℃, and finally flattening by using a roller press to obtain the aerogel composite material, wherein the film pressing speed of the roller press is 0.5-1.0 m/S.
Comparative example 2 an aerogel composite and method of making, comprising:
1. adding the alumina aerogel powder and the polyethylene resin into a stirring kettle according to the proportion of 1:1.5, and heating and uniformly mixing to obtain a mixture;
2. adding 50% of polyethylene resin into a stirring kettle for melting, then sequentially adding 3% of flame retardant powder, 25% of filler and a dispersing agent, stirring and mixing, and then adding 3% of coloring powder for coloring to prepare a film material;
3. respectively extruding the mixture and the membrane material through a membrane blowing machine to prepare an aerogel layer and a membrane layer, wherein the thickness of the aerogel layer is 0.03-0.05mm, and the thickness of the membrane layer is 0.2-0.3 mm;
5. and laying the film layer on the aerogel layer, heating to 300-1000 ℃ to melt and blend the aerogel layer and the film layer, and flattening by using a roller press to obtain the aerogel composite material, wherein the film pressing speed of the roller press is 0.5-1.0 m/S.
The aerogel composite material for cold insulation of the ship pipeline, prepared by the invention, has better strength and viscosity, and has a larger relation with an added adhesive layer and a film layer, and in order to verify the related technical scheme, the applicant performs the following tests:
comparative examples 1 to 2: by adopting the method of embodiment 2, the prepared aerogel composite material is detected under the condition of respectively removing the adhesive layer and the film layer, and the specific indexes are shown in table 2:
TABLE 2
Compressive strength (Mpa) Breaking strength (Mpa) Coefficient of thermal conductivity (W/m. K) Tensile bond Strength (Mpa) Peel strength (Mpa)
Comparative example 1 1.2 0.8 0.051 74 27
Comparative example 2 2.7 2.1 0.033 0 0
Example 2 3.5 2.9 0.033 74 27
According to table 2, when the film layer was removed, the thermal conductivity of the aerogel composite material increased, and both the compressive strength and the flexural strength decreased greatly, and when the adhesive layer was removed, the aerogel composite material lost the cohesiveness, and at the same time, the compressive strength and the flexural strength decreased, so it can be seen that the aerogel composite material prepared in the present invention had better strength and adhesiveness.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (10)

1. The utility model provides a marine vessel pipeline keeps cold and uses aerogel combined material which characterized in that: the aerogel composite material consists of an aerogel layer and a glue film, wherein the aerogel layer is prepared by mixing alumina aerogel and polyethylene resin;
the adhesive film comprises an adhesive layer and a film layer, wherein the adhesive layer is prepared by mixing epoxy resin and water-based acrylic acid, and the film layer comprises the following raw materials: 40-60% of polyethylene resin, 1-5% of flame-retardant powder, 20-30% of filler powder and 1-5% of coloring powder.
2. The aerogel composite for keeping marine pipelines cold as claimed in claim 1, wherein: the flame-retardant powder is formed by mixing gas-phase antimony trioxide and gas-phase magnesium hydroxide in a ratio of 1:1.
3. The aerogel composite for keeping marine pipelines cold as claimed in claim 1, wherein: the filler powder is selected from one or more of glass fiber, asbestos, diatomite, perlite powder, cork powder, talcum powder and calcium carbonate.
4. The aerogel composite for keeping marine pipelines cold as claimed in claim 1, wherein: the coloring powder is selected from vapor phase titanium dioxide.
5. A method for preparing the aerogel composite material for keeping the temperature of the ship pipeline as set forth in any one of claims 1 to 4, which comprises the steps of:
s1, adding the alumina aerogel powder and the polyethylene resin into a stirring kettle, and heating and uniformly mixing to obtain a mixture;
s2, adding epoxy resin into a stirring kettle, heating and melting, adding water-based acrylic acid into the solution according to a proportion, mixing and stirring to obtain a glue solution;
s3, adding polyethylene resin into a stirring kettle for melting, then sequentially adding flame retardant powder, filler and dispersant for stirring and mixing, and then adding coloring powder for coloring to obtain a film material;
s4, respectively extruding the mixture, the glue solution and the film material through a film blowing machine to obtain an aerogel layer, a glue layer and a film layer;
and S5, downwards arranging the adhesive layer, sequentially laying the aerogel layer and the film layer, heating at high temperature to melt and blend the surfaces of the adhesive layer, the aerogel layer and the film layer, and finally flattening by a roller press to obtain the aerogel composite material.
6. The method for preparing the aerogel composite material for cooling ship pipelines according to claim 5, wherein the method comprises the following steps: in S1, the mixing ratio of the alumina aerogel and the polyethylene resin is 1: 1.5.
7. The method for preparing the aerogel composite material for cooling ship pipelines according to claim 5, wherein the method comprises the following steps: in the S2, the mixing ratio of the epoxy resin to the water-based acrylic acid is 2: 1.
8. The method for preparing the aerogel composite material for cooling ship pipelines according to claim 5, wherein the method comprises the following steps: in the S4, the thickness of the aerogel layer is 0.03-0.05mm, the thickness of the glue layer is 0.05-0.1 mm, and the thickness of the film layer is 0.2-0.3 mm.
9. The method for preparing the aerogel composite material for cooling ship pipelines according to claim 5, wherein the method comprises the following steps: in the S5, the heating temperature is 300-1000 ℃.
10. The method for preparing the aerogel composite material for cooling ship pipelines according to claim 5, wherein the method comprises the following steps: in the S5, the film pressing speed of the roller press is 0.5-1.0 m/S.
CN202111023643.4A 2021-09-02 2021-09-02 Aerogel composite material for cooling ship pipeline and preparation method thereof Pending CN113698886A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111023643.4A CN113698886A (en) 2021-09-02 2021-09-02 Aerogel composite material for cooling ship pipeline and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111023643.4A CN113698886A (en) 2021-09-02 2021-09-02 Aerogel composite material for cooling ship pipeline and preparation method thereof

Publications (1)

Publication Number Publication Date
CN113698886A true CN113698886A (en) 2021-11-26

Family

ID=78657170

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111023643.4A Pending CN113698886A (en) 2021-09-02 2021-09-02 Aerogel composite material for cooling ship pipeline and preparation method thereof

Country Status (1)

Country Link
CN (1) CN113698886A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105256902A (en) * 2015-07-22 2016-01-20 卓达新材料科技集团有限公司 Instant aerogel composite heat isolation adhesive tape and preparing method of instant aerogel composite heat isolation adhesive tape
CN106079778A (en) * 2016-07-28 2016-11-09 南京纳世新材料有限责任公司 Aeroge sound insulation thermal insulation adhesive tape and preparation method thereof
CN110696453A (en) * 2019-11-15 2020-01-17 上海泉欣织造新材料股份有限公司 Aerogel-containing heat insulation cotton and production process thereof

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105256902A (en) * 2015-07-22 2016-01-20 卓达新材料科技集团有限公司 Instant aerogel composite heat isolation adhesive tape and preparing method of instant aerogel composite heat isolation adhesive tape
CN106079778A (en) * 2016-07-28 2016-11-09 南京纳世新材料有限责任公司 Aeroge sound insulation thermal insulation adhesive tape and preparation method thereof
CN110696453A (en) * 2019-11-15 2020-01-17 上海泉欣织造新材料股份有限公司 Aerogel-containing heat insulation cotton and production process thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
管蓉等: "《玻璃与陶瓷用胶黏剂及粘接技术》", 31 October 2004, 化学工业出版社 *

Similar Documents

Publication Publication Date Title
WO2011085531A1 (en) Flame retardant polymeric foam material and manufacturing method thereof
CN111138716B (en) Flame retardant and wood-plastic composite material
CN109503970A (en) A kind of high fire-retardance grade HIPS composite
CN1962746A (en) Expansion type flame-proof smoke-suppressing soft polyvinyl chloride composition and its preparation method
CN104031326A (en) Modified hard crosslinked polyvinyl chloride flame-retardant foam and preparation method thereof
CN103073795B (en) A kind of flame-retardant polypropylene membrane and preparation method thereof
CN103360667A (en) Halogen-free flame retarding macromolecule sandwich layer material for high strength light fireproofing aluminum-plastic panel and preparation method thereof
CN109867942B (en) Preparation method of flame-retardant micro-foaming polyphenyl ether composite material and product thereof
CN108912444A (en) A kind of environment friendly halogen-free fireproof master batch and preparation method thereof
CN103342845A (en) Novel fire-proof material and preparing method thereof, light fire-proof aluminium-plastic panel
CN110079008A (en) A kind of halogen-free intumescent flame-retardant special breathable membrane material and preparation method thereof
CN113698886A (en) Aerogel composite material for cooling ship pipeline and preparation method thereof
KR102143690B1 (en) A semi-inflammable insulation material and manufacturing method for it
CN103881231A (en) Thermal energy storage spacing bar based on ethylene-vinyl acetate copolymer and preparation method of spacing bar
CN106928648B (en) Whisker reinforced toughened halogen-free flame-retardant phenolic foam plastic and preparation method thereof
CN107140879A (en) A kind of heat insulation floor and preparation method thereof
CN107163466A (en) A kind of environment protecting thermal insulating material and preparation method thereof
CN105295253A (en) Sound absorption and noise reduction construction pipe and preparation method thereof
CN109437661B (en) Heat-insulating fireproof composite material and preparation and application methods thereof
CN114607841B (en) Preparation method of temperature-resistant impact-resistant high-strength PPR fiber composite pipe
CN105038155A (en) Composite enhanced PET (polyethylene terephthalate) material
CN109293295A (en) A kind of homogeneous complex material heat preservation template and its production method
CN108517087A (en) PVC board and its preparation method and application
CN217272475U (en) Fiber-reinforced random copolymerization polypropylene composite pipe with flame-retardant insulation layer
CN111269567A (en) Preparation method of nylon 66-based aerogel composite material

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
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20211126