阅读说明：本技术 一种各向异性的耐高温碳化硅气凝胶隔热材料制备方法 (Preparation method of anisotropic high-temperature-resistant silicon carbide aerogel heat insulation material ) 是由 程旭东 闫明远 张和平 潘月磊 龚伦伦 于 2021-10-28 设计创作，主要内容包括：本发明提供了一种各向异性的耐高温碳化硅气凝胶隔热材料制备方法,包括以下步骤：1)木材原料在酸性条件下进行脱木质素、半纤维素处理,随后通过冷冻干燥制备各向异性的木基气凝胶。该木基气凝胶用作碳化硅生成反应中的碳源和模板；2)将一氧化硅粉末铺于烧舟底部,将步骤1制备的木基气凝胶放置于一氧化硅粉末上方,并盖上烧舟盖；3)将步骤2的烧舟放于高温箱式炉中,在高温和惰性气体的环境下,制备得到各向异性的耐高温碳化硅气凝胶隔热材料。(The invention provides a preparation method of an anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material, which comprises the following steps: 1) wood raw materials are delignified and hemicellulose treated under acidic conditions, and then anisotropic wood-based aerogels are prepared by freeze-drying. The wood-based aerogel is used as a carbon source and a template in a silicon carbide generation reaction; 2) paving silicon monoxide powder at the bottom of the burning boat, placing the wood-based aerogel prepared in the step 1 above the silicon monoxide powder, and covering a burning boat cover; 3) and (3) placing the burning boat obtained in the step (2) in a high-temperature box type furnace, and preparing the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material under the environment of high temperature and inert gas.)

1. The preparation method of the anisotropic high-temperature-resistant silicon carbide aerogel heat insulation material is characterized by comprising the following steps of:

(1) soaking the wood in an aqueous solution containing an oxidation bleaching agent at 85-90 ℃ under an acidic condition, and replacing the aqueous solution containing the oxidation bleaching agent every 6-8 hours until the wood is completely white to obtain white wood; soaking the white wood in an aqueous solution of sodium hydroxide at the temperature of 90-95 ℃ to further remove residual lignin in the white wood, and then cooking the white wood with deionized water at the temperature of 90-95 ℃ to remove residual reagents to obtain lignin-removed wood; freeze-drying the delignified wood to obtain anisotropic wood-based aerogel;

(2) paving silicon monoxide powder at the bottom of a burning boat, placing the wood-based aerogel prepared in the step (1) above the silicon monoxide powder, and covering a burning boat cover; the mass ratio of the silicon monoxide powder to the wood-based aerogel is 1: 0.2-0.4; (3) placing the burning boat in the step (2) in a high-temperature box type furnace, and preparing the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material under the environment of high temperature and inert gas protection; the high-temperature environment is at a temperature of 1400-1600 ℃.

2. The method according to claim 1, wherein in the step (1), the wood is one of balsa wood, pine wood and paulownia wood.

3. The method according to claim 1, wherein in the step (1), the acidic condition is one of adding hydrochloric acid and acetic acid before or during the reaction to make the pH of the aqueous solution 4 to 4.5.

4. The method according to claim 1, wherein in the step (1), the oxidative bleaching agent is one or both of acetic acid and sodium chlorite.

5. The method according to claim 1, wherein the content of the oxidative bleaching agent in the step (1) is 1.5 to 4.5 wt%.

6. The method according to claim 1, wherein in the step (1), the content of the sodium hydroxide is 5 to 10 wt%.

7. The method according to claim 1, wherein the freeze-drying is carried out at a freezing temperature of-60 ℃ to-40 ℃ and a drying temperature of 20 ℃ to 30 ℃.

8. The method according to claim 1, wherein in the step (3), the inert gas is argon, nitrogen or a mixture of argon and hydrogen; preferably, the inert gas is high-purity argon, high-purity nitrogen or argon-hydrogen mixed gas; preferably, the volume fraction of argon in the high-purity argon gas is 99.99 percent; preferably the volume fraction of nitrogen in the high purity nitrogen gas is 99.99%; preferably, the volume fraction of hydrogen in the argon-hydrogen mixture is 5%.

9. The method according to claim 1, wherein the freeze-drying of step (1) is carried out for a freezing time of 12 to 24 hours; the drying time of freeze drying is 24-48 hours; the drying pressure of freeze drying is 10-20 Pa.

10. The preparation method according to claim 1, wherein the step (3) is specifically: carrying out vacuum-pumping and inert gas-filling scrubbing treatment on the high-temperature box-type furnace for at least 3 times to remove oxygen in the furnace; then, heating to 1400-1600 ℃ in a high-temperature box furnace at a heating rate of 5-10 ℃/min, and then preserving heat for 2-4 hours; and then naturally cooling, and cooling to room temperature in a high-temperature box type furnace to obtain the silicon carbide aerogel.

Technical Field

The invention belongs to the field of aerogel preparation, and particularly relates to a preparation method of an anisotropic high-temperature-resistant silicon carbide aerogel thermal insulation material.

Background

Aerogel, one of the lightest solid materials in the world, is known as the "fanciful material of the 21 st century" because of its ultra-high porosity and ultra-low density. The aerogel has a special porous structure, so that the aerogel has an extremely low heat conductivity coefficient, and therefore, the aerogel has a huge application scene in the field of heat preservation and insulation.

There are many types of aerogels at present, including silica aerogels which were studied at the earliest and organic polymer aerogels which have been studied widely in recent years, and the like. However, the above-mentioned aerogels all have the problems of high-temperature structural damage, failure and the like, and the application and development of the aerogels in the high-temperature field are severely limited by the problems. However, the light heat-insulating material with high temperature resistance and ablation resistance is urgently needed in the fields of aerospace, high-temperature smelting and the like, so that the development of the high-temperature resistant aerogel has great significance. At present, the research on the high-temperature resistant aerogel is few, and mainly focuses on carbide aerogel and oxide aerogel.

Among them, silicon carbide aerogel has the advantages of low thermal expansion coefficient, high temperature resistance, high wear resistance, stable chemical properties, etc., and is paid more and more attention by researchers. CN112607740A discloses a method for preparing silicon carbide nanofiber aerogel, which mainly utilizes carbothermic reduction reaction between silica sol and carbon fiber to prepare silicon carbide. Chinese patents CN112537964A and CN111484018A both adopt polycarbosilane pyrolysis reaction to prepare silicon carbide aerogel, but a large amount of organic solvent is used in the preparation process, which causes pollution to the environment. While the Chinese patent 108328617A uses CVD method to prepare silicon carbide nanowire aerogel in a tube furnace, the size of the aerogel prepared by the method is small, and the macroscopic size of the aerogel is not regulated and controlled. Meanwhile, the aerogel structure prepared by the method is isotropic, and when the aerogel structure is used as a heat insulation material, the problem of heat insulation failure caused by overhigh local temperature cannot be avoided.

Disclosure of Invention

In view of the above, the present invention provides a method for preparing an anisotropic high temperature resistant silicon carbide aerogel thermal insulation material. The preparation process of the method is simple. The prepared anisotropic silicon carbide aerogel has excellent high temperature resistance and heat insulation performance, and can be directly applied to the high temperature heat insulation field of aerospace and the like.

The invention provides a preparation method of an anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material, which comprises the following steps:

(1) and (2) soaking the wood in an aqueous solution containing an oxidation bleaching agent at 85-90 ℃ under an acidic condition, and replacing the aqueous solution containing the oxidation bleaching agent every 6-8 hours until the wood is completely white to obtain white wood. Soaking the white wood in an aqueous solution of sodium hydroxide at the temperature of 90-95 ℃ to further remove residual lignin in the white wood, and then cooking the white wood with deionized water at the temperature of 90-95 ℃ to remove residual reagents to obtain lignin-removed wood; and (3) freeze-drying the delignified wood to obtain the anisotropic wood-based aerogel. Preferably the wood is one of balsa wood, pine wood and paulownia wood. Preferably, the acidic condition is that one of hydrochloric acid and acetic acid is added before or during the reaction to ensure that the pH value of the aqueous solution is 4-4.5. Preferably the oxidative bleach is one or both of acetic acid and sodium chlorite. Preferably, the content of the oxidation bleaching agent is 1.5-4.5 wt%. Preferably, the content of the sodium hydroxide is 5-10 wt%. Preferably, the freezing temperature of the freeze drying is-60 ℃ to-40 ℃, and the drying temperature is 20 ℃ to 30 ℃.

(2) Paving silicon monoxide powder at the bottom of a burning boat, placing the wood-based aerogel prepared in the step (1) above the silicon monoxide powder, and covering a burning boat cover; the mass ratio of the silicon monoxide powder to the wood-based aerogel is 1: 0.2-0.4. Preferably, the burning boat is one of an alumina burning boat and a graphite burning boat.

(3) Placing the burning boat in the step (2) in a high-temperature box type furnace, and preparing the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material under the environment of high temperature and inert gas protection; the high-temperature environment is at a temperature of 1400-1600 ℃. Preferably, the inert gas is argon, nitrogen or argon-hydrogen mixture gas. Preferably, the inert gas is high-purity argon, high-purity nitrogen or argon-hydrogen mixed gas.

For example, the mass ratio of the silicon monoxide powder to the wood-based aerogel is 1:0.2, 1; 0.25, 1:0.3, 1: 0.35 or 1: 0.4.

preferably, the freezing time of the freeze drying in the step (1) is 12-24 hours; the drying time of freeze drying is 24-48 hours; the drying pressure of freeze drying is 10-20 Pa.

Preferably, the step (3) is specifically: and (3) performing vacuum pumping and inert gas filling scrubbing treatment on the high-temperature box type furnace for at least 3 times to remove oxygen in the furnace. And then, heating the mixture to 1400-1600 ℃ in a high-temperature box furnace at a heating rate of 5-10 ℃/min, and then preserving heat for 2-4 hours. And then naturally cooling to room temperature to obtain the silicon carbide aerogel. The volume fraction of argon in the high-purity argon is 99.99%. The volume fraction of nitrogen in the high-purity nitrogen gas was 99.99%. The volume fraction of hydrogen in the argon-hydrogen mixture was 5%.

Compared with the traditional preparation method of the silicon carbide aerogel, the preparation method has the following gain effects.

1. The preparation method is simple and has good repeatability. In the preparation method, wood which is easy to obtain is used as a biomass carbon source, and compared with carbon sources such as carbon fiber and the like adopted in other methods, the method has the advantages of low cost, large-scale popularization and the like. Meanwhile, the method adopts silicon monoxide powder as a silicon source, and compared with other organic precursors such as polysilazane, polysiloxane and the like involved in the invention method, the invention method has the advantages of simple preparation method, safety, environmental friendliness and the like.

2. The anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material prepared by the invention has a unique layered structure and a micro-nano hierarchical structure. Since wood itself has a macroscopic layered structure and a cellular structure on a smaller scale, the wood-based aerogel obtained by freeze-drying in the present invention also has a unique layered structure and cellular structure. In the high-temperature sintering process, the laminated structure of the wood-based aerogel is further transformed into a laminated structure of silicon carbide aerogel with the thickness of 45-80 microns. Meanwhile, the wood-based aerogel is used as a carbon source to participate in the reaction, and the honeycomb structure of the wood-based aerogel on a smaller scale is changed into a silicon carbide nanowire structure which is 15-35 nm in diameter and is staggered with each other. The layered structure and the micro-nano hierarchical structure enable the silicon carbide aerogel obtained by the method to have the characteristic of obvious anisotropy. Compared with isotropic silicon carbide aerogel structures in other inventions, the layered structure and the hierarchical structure can more effectively reduce solid heat conduction and gas convection heat transfer in the direction perpendicular to the layered structure, so that the heat insulation effect of the silicon carbide aerogel obtained by the invention is greatly improved.

3. The anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material prepared by the invention has excellent heat-insulating property, and the radial heat conductivity coefficient can be as low as 0.019Wm at room temperature^-1K^-1. Even at 1000 ℃, the radial thermal conductivity is still lower than 0.1Wm^-1K^-1. This excellent thermal insulation benefits from the layered structure of the silicon carbide aerogel. In particular, the layered structure can effectively divide the space, limiting gas convective heat transfer and solid heat transfer. Meanwhile, the laminated structure enables the inner layers of the silicon carbide aerogel to be compressed and restored, so that the silicon carbide aerogel obtained by the method has excellent elasticity. Compared with the brittle silicon carbide aerogel obtained by other inventions, the elastic silicon carbide aerogel is more beneficial to transportation, installation and long-term use of the silicon carbide aerogel.

Drawings

FIG. 1 is a schematic diagram illustrating a process for preparing an anisotropic high temperature resistant silicon carbide aerogel thermal insulation material according to the present invention;

FIG. 2 is a pictorial representation of a silicon carbide aerogel prepared in example 1;

FIG. 3 is a Scanning Electron Microscope (SEM) image of a silicon carbide aerogel prepared in example 1;

FIG. 4 is an X-ray diffraction (XRD) pattern of the silicon carbide aerogel prepared in example 1;

FIG. 5 is a Transmission Electron Microscope (TEM) image of the silicon carbide aerogel prepared in example 1;

FIG. 6 is an alcohol lamp flame burn resistant image of the silicon carbide aerogel prepared in example 2;

FIG. 7 is a butane torch flame ablation resistant image of the silicon carbide aerogel prepared in example 2;

FIG. 8 is a fatigue test chart for the silicon carbide aerogel prepared in example 3;

FIG. 9 is a graph showing the elastic recovery process at high temperature of the silicon carbide aerogel prepared in example 3;

FIG. 10 is an infrared thermographic view of the silicon carbide aerogel prepared in example 3 heated on a hot plate;

FIG. 11 is a graph of thermal conductivity versus temperature for the silicon carbide aerogel prepared in example 3.

Detailed Description

To further illustrate the present invention, the following method for preparing a refractory anisotropic silicon carbide aerogel is described in detail with reference to the following examples, which are provided for the purpose of illustration, and it is to be understood that the examples are only illustrative of the present invention and should not be construed as limiting the scope of the present invention.

In the following examples, the test methods and equipment used were as follows:

(1) scanning Electron Microscope (SEM) picture, and the used equipment is a cold field scanning electron microscope SU 8220;

(2) x-ray diffraction (XRD) patterns using a sample level high power diffractometer, (TTR-III);

(3) a Transmission Electron Microscope (TEM) image, and the used equipment is a high-resolution transmission electron microscope (JEM-2100F);

(4) the flame ablation pattern of the alcohol lamp is resisted, and the used equipment is a common alcohol lamp;

(5) fatigue test patterns for silicon carbide aerogels using a universal tester (Instron E3000K 8953); the experimental method comprises the following steps: the sample was compressed to 30% of its thickness at a loading and unloading rate of 60mm/min, and then the pressure was again unloaded and the sample rebounded. The compression and rebound are repeated for 400 circles;

(6) the experimental method is as follows: the silicon carbide is compressed and rebounded by tweezers in the flame of the butane spray gun;

(7) an infrared thermograph of the heated silicon carbide aerogel on a hot plate using a thermal infrared imager (FLIRA655 sc);

(8) thermal conductivity of the silicon carbide aerogel was plotted as a function of temperature using a laser thermal conductivity instrument (LFA467/HFM 446S).

Example 1

2g of sodium chlorite, 0.5ml of acetic acid and 100ml of deionized water are taken to be put into a beaker, and the mixture is uniformly mixed and stirred to obtain the oxidation bleaching agent solution with the pH value of 4. And soaking the balsawood blocks with the side length of 2cm in the oxidation bleaching agent at the temperature of 90 ℃, and replacing the oxidation bleaching agent once every 8 hours until the wood is completely white. Then, soaking white wood in a 5 wt% sodium hydroxide aqueous solution at 95 ℃ for 8 hours to further remove residual lignin in the white wood, and then cooking the white wood with deionized water at 95 ℃ for 4 hours to remove residual reagents to obtain lignin-removed wood; freezing the delignified wood at-60 ℃ for 24 hours, and then carrying out vacuum drying for 36 hours at the vacuum drying pressure of 20Pa and the vacuum drying temperature of 25 ℃ to obtain anisotropic wood-based aerogel; 1g of SiO powder was spread on the bottom of the boat, and 0.4g of wood based aerogel was placed over the SiO powder and the boat lid was closed. The boat was then placed in a high temperature box furnace. And (3) performing vacuum pumping and inert gas filling scrubbing treatment on the high-temperature box type furnace for at least 3 times to remove oxygen in the furnace. And then heating to 1550 ℃ at the heating rate of 5 ℃/min in the argon atmosphere, then preserving the heat for 4 hours, and then naturally cooling to room temperature to obtain the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material. The schematic diagram of the whole preparation process is shown in figure 1.

As shown in FIG. 2, the anisotropic silicon carbide aerogel obtained in example 1 had a density of only 0.03g/cm³Can stand on the dandelion. The anisotropic silicon carbide aerogel obtained in example 1 had a radial thermal conductivity of only 0.027Wm^{- 1}K^-1And exhibits excellent heat insulating properties. SEM results (figure 3) show that the silicon carbide aerogel prepared by the method has an obvious layered structure, and the thickness of each layer is 45-80 μm. The layered structure effectively partitions the space, reduces solid heat conduction and gas convection, and greatly improves the heat insulation performance of the silicon carbide aerogel. At the same time, the silicon carbide nanowire structure can be observed under a larger magnification of 2 ten thousand times. The diameter of the silicon carbide nanowires is 15-35 nm, the nanowires are mutually staggered to form a nano-scale micropore and mesoporous structure, so that the thermal motion of molecules can be effectively limited, and the heat conduction is reduced. XRD (FIG. 4) was used to further analyze carbonizationThe phase structure of the silicon aerogel confirmed that the main component of the silicon carbide aerogel is 3C — SiC, and 3C — SiC mainly consists of the 111 crystal plane. TEM (fig. 5) shows single silicon carbide nanowires with a diameter of 33nm, further demonstrating the successful synthesis of silicon carbide nanowire structures.

Example 2

2g of sodium chlorite, 0.5ml of acetic acid and 100ml of deionized water are taken to be put into a beaker, and the mixture is uniformly mixed and stirred to obtain the oxidation bleaching agent solution with the pH value of 4. And soaking the balsawood blocks with the side length of 2cm in the oxidation bleaching agent at the temperature of 90 ℃, and replacing the oxidation bleaching agent once every 8 hours until the wood is completely white. Then, soaking white wood for 8 hours in 5 wt% sodium hydroxide aqueous solution at 95 ℃, further removing residual lignin in the white wood, and then, cooking the white wood for 4 hours by using deionized water at 95 ℃ to remove residual reagents, thereby obtaining lignin-removed wood; freezing the delignified wood at-60 ℃ for 24 hours, and then carrying out vacuum drying for 36 hours at the vacuum drying pressure of 20Pa and the vacuum drying temperature of 25 ℃ to obtain anisotropic wood-based aerogel; 1g of SiO powder was spread on the bottom of the boat, and 0.3g of wood based aerogel was placed over the SiO powder and covered with the boat lid. The boat was then placed in a high temperature box furnace. And (3) performing vacuum pumping and inert gas filling scrubbing treatment on the high-temperature box type furnace for at least 3 times to remove oxygen in the furnace. And then heating to 1550 ℃ at the heating rate of 5 ℃/min in the argon atmosphere, then preserving the heat for 4 hours, and then naturally cooling to room temperature to obtain the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material.

The thermal conductivity of the silicon carbide aerogel obtained in example 2 was 0.021Wm^-1K^-1It is reduced compared to example 1, mainly because the mass ratio of the SiO powder to the wood-based aerogel is improved in the preparation process of example 2. The carbon source is sufficiently reacted, so that the residual amount of carbon is reduced, and the thermal conductivity is further reduced. In order to confirm that the silicon carbide aerogel prepared by the method has excellent high temperature resistance and ablation resistance, the silicon carbide aerogel obtained in example 2 was respectively placed in an alcohol burner flame and a butane torch flame for burning (fig. 6 and 7). From FIG. 7 can be seenIt is seen that the silicon carbide aerogel obtained in example 2 is non-combustible in a butane torch flame at 1300 c, and its appearance and overall structure remain substantially unchanged. The silicon carbide aerogel prepared by the method has excellent high-temperature resistance and ablation resistance, and can be used as a high-temperature-resistant and refractory material.

Example 3:

2g of sodium chlorite, 0.5ml of acetic acid and 100ml of deionized water are taken to be put into a beaker, and the mixture is uniformly mixed and stirred to obtain the oxidation bleaching agent solution with the pH value of 4. And soaking the balsawood blocks with the side length of 2cm in the oxidation bleaching agent at the temperature of 90 ℃, and replacing the oxidation bleaching agent once every 8 hours until the wood is completely white. Then, soaking white wood for 8 hours in 5 wt% sodium hydroxide aqueous solution at 95 ℃, further removing residual lignin in the white wood, and then, cooking the white wood for 4 hours by using deionized water at 95 ℃ to remove residual reagents, thereby obtaining lignin-removed wood; freezing the delignified wood at-60 ℃ for 24 hours, and then carrying out vacuum drying for 36 hours at the vacuum drying pressure of 20Pa and the vacuum drying temperature of 25 ℃ to obtain anisotropic wood-based aerogel; 1g of SiO powder was spread on the bottom of the boat, and 0.2g of wood based aerogel was placed over the SiO powder and the boat lid was closed. The boat was then placed in a high temperature box furnace. And (3) performing vacuum pumping and inert gas filling scrubbing treatment on the high-temperature box type furnace for at least 3 times to remove oxygen in the furnace. And then heating to 1550 ℃ at the heating rate of 5 ℃/min in the argon atmosphere, then preserving the heat for 4 hours, and then naturally cooling to room temperature to obtain the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material.

The resulting anisotropic silicon carbide aerogel of example 3 had a thermal conductivity of only 0.019Wm^-1K^-1Compared with examples 1 and 2, the thermal conductivity is significantly reduced. This is mainly because the mass ratio of the silicon monoxide powder to the wood-based aerogel is the highest in the preparation process of example 3, and the silicon source is the most sufficient, so that the carbon source is fully reacted, and the thermal conductivity is further reduced. As can be seen from fig. 8, the silicon carbide aerogel obtained in example 3 can perform compression and rebound actions in a butane torch flame, and has excellent elasticity. The fatigue resistance test shows that the methodThe prepared silicon carbide aerogel can complete 400 loading and unloading cycle tests (figure 9) under the deformation of 30%. The mechanical test results show that the silicon carbide aerogel prepared by the method has excellent elasticity and fatigue resistance. In addition, the silicon carbide aerogel obtained in example 3 was placed on a 1200 ℃ iron plate in the axial direction (parallel to the layered structure of the aerogel) and the radial direction (perpendicular to the layered structure of the aerogel), respectively, and the temperature distribution of the silicon carbide aerogel was observed and recorded by a thermal infrared imager. The results of the infrared images show that after the temperature of the silicon carbide sample had stabilized, the upper surface temperature of the radially positioned silicon carbide sample was only 133 deg.c, while the upper surface temperature of the axially positioned sample was 229.9 deg.c (fig. 10). This indicates that the thermal insulation effect in the radial direction is significantly better than that in the axial direction, and therefore the silicon carbide aerogel prepared by the method has significant anisotropic thermal insulation properties. To further analyze the anisotropic thermal insulation properties of the silicon carbide aerogel, the thermal conductivity of the silicon carbide aerogel was measured in both the axial and radial directions and plotted in fig. 11. As shown in FIG. 11, at room temperature, the silicon carbide aerogel prepared by the method has an axial thermal conductivity of 0.063Wm^-1K^-1And is 3.3 times the radial thermal conductivity. Meanwhile, as can be seen from fig. 11, as the temperature increases, the axial and radial thermal conductivity coefficients both show an upward trend, but at a high temperature of 1000 ℃, the thermal conductivity coefficient of the radial silicon carbide aerogel is only 0.086Wm^-1K^-1Much lower than the thermal conductivity (490 Wm) of intrinsic crystals of silicon carbide^-1K^-1). The results show that the silicon carbide aerogel prepared by the method has anisotropy and excellent heat insulation performance. The anisotropic heat insulation performance can avoid the problem that the material has heat insulation failure at local high temperature. Therefore, the anisotropic high-temperature-resistant silicon carbide aerogel heat-insulating material prepared by the method can be used as an advanced heat-insulating material.

The invention has not been described in detail and is part of the common general knowledge of a person skilled in the art. The above-described embodiments are merely illustrative of the preferred embodiments of the present invention, and the preferred embodiments are not exhaustive and do not limit the invention to the precise embodiments described. Various modifications and improvements of the technical solution of the present invention may be made by those skilled in the art without departing from the spirit of the present invention, and the technical solution of the present invention is to be covered by the protection scope defined by the claims.