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CN114806514A - Method for preparing discontinuous scattering reinforced hole-sphere composite polymer-based radiation refrigeration material by adopting template method - Google Patents

Method for preparing discontinuous scattering reinforced hole-sphere composite polymer-based radiation refrigeration material by adopting template method Download PDF

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CN114806514A
CN114806514A CN202210489324.0A CN202210489324A CN114806514A CN 114806514 A CN114806514 A CN 114806514A CN 202210489324 A CN202210489324 A CN 202210489324A CN 114806514 A CN114806514 A CN 114806514A
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radiation refrigeration
refrigeration material
composite polymer
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田雪峰
索鹏飞
张亦岚
艾鑫
刘钰龙
高继慧
王怀远
陆袁威
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Harbin Institute of Technology Shenzhen
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Abstract

采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法,它涉及材料科学技术领域,具体涉及一种辐射制冷材料的制备方法。本发明的目的是要解决现有技术制备的辐射制冷材料存在制备方法不环保,或大气窗口区域发射性能较差的问题。方法要点:制备聚合物混合液;成型,得到辐射制冷材料粗品;去除致孔剂,得到非连续散射强化的孔球复合聚合物基辐射制冷材料。优点:太阳光谱(0.3μm~1μm)反射率R可以达到68%,与单一多孔材料相比,在大气窗口波段(8μm~13μm)发射率显著提高;且夜间降温效果最低可达5.8℃。本发明主要用于制备非连续散射强化的孔球复合聚合物基辐射制冷材料。

Figure 202210489324

A method for preparing a non-continuous scattering-strengthened hole-ball composite polymer-based radiation refrigeration material by a template method relates to the field of material science and technology, in particular to a preparation method of a radiation refrigeration material. The purpose of the present invention is to solve the problem that the radiation refrigeration material prepared in the prior art has an unenvironmental preparation method or poor emission performance in the atmospheric window area. Key points of the method: preparing polymer mixture; molding to obtain crude radiation refrigeration material; removing porogen to obtain discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material. Advantages: The reflectivity R of the solar spectrum (0.3μm~1μm) can reach 68%. Compared with a single porous material, the emissivity in the atmospheric window band (8μm~13μm) is significantly improved; and the cooling effect at night can be as low as 5.8℃. The invention is mainly used for preparing discontinuous scattering reinforced porous ball composite polymer-based radiation refrigeration material.

Figure 202210489324

Description

采用模板法制备非连续散射强化的孔球复合聚合物基辐射制 冷材料的方法Method for preparing discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material by template method

技术领域technical field

本发明涉及材料科学技术领域,具体涉及一种辐射制冷材料的制备方法。The invention relates to the technical field of material science, in particular to a preparation method of a radiation refrigeration material.

背景技术Background technique

我国建筑能耗约占整个社会总能耗比重较大,其中空调能耗占建筑总能耗的30%~60%。并且预计2050年全球用于冷却能耗将为目前的2倍,因此,为降低空调主动制备设备的使用,研发新型零碳被动制冷技术对于建筑节能至关重要。my country's building energy consumption accounts for a large proportion of the total energy consumption of the whole society, of which air-conditioning energy consumption accounts for 30% to 60% of the total energy consumption of buildings. And it is expected that the global energy consumption for cooling will be doubled in 2050. Therefore, in order to reduce the use of active air conditioning equipment, the development of new zero-carbon passive cooling technology is crucial for building energy conservation.

辐射制冷作为一种新型无能耗被动制冷技术受到了广泛关注。理想日间辐射制冷新材料通过大气窗口(8~13μm)将自身热量辐射到外太空巨大冷源中,无需消耗任何电能或者热能,对于降低制冷能耗、实现零碳环保具有重要意义。目前常见的辐射制冷材料主要有多层结构,具有表面周期性结构的超材料,随机分布的粒子结构,多孔结构。其中,多孔结构材料以其制冷效果好、制备方法简单、成本低廉、可大规模制备的优势脱颖而出,成为了最具应用与未来商业化前景的辐射制冷材料。但是对于目前的多孔材料而言,还存在有制备方法不环保、大气窗口发射率不高等问题限制其实际应用。Radiant cooling has received extensive attention as a new type of passive cooling technology without energy consumption. The ideal new material for daytime radiation refrigeration radiates its own heat into the huge cold source in outer space through the atmospheric window (8-13 μm) without consuming any electricity or heat energy, which is of great significance for reducing refrigeration energy consumption and achieving zero-carbon environmental protection. At present, the common radiation refrigeration materials mainly include multi-layer structures, metamaterials with periodic surface structures, randomly distributed particle structures, and porous structures. Among them, porous structure materials stand out for their advantages of good refrigeration effect, simple preparation method, low cost, and large-scale preparation, and become the radiation refrigeration material with the most application and future commercialization prospects. However, for the current porous materials, there are still problems such as unfriendly preparation methods and low atmospheric window emissivity, which limit their practical application.

中国已公开专利《一种超疏水自清洁辐射降温薄膜及其制备方法》(申请公布号:CN110483924A),该方法使用相转化法制备具有微纳双重多孔结构的薄膜。该种方式所使用的丙酮、四氢呋喃等有机溶剂均有毒并易挥发,不具有环境友好性。China has published a patent "A superhydrophobic self-cleaning radiation cooling film and its preparation method" (application publication number: CN110483924A), which uses a phase inversion method to prepare a film with a micro-nano dual porous structure. The organic solvents such as acetone and tetrahydrofuran used in this way are toxic and volatile, and are not environmentally friendly.

中国已公开专利《一种多孔聚二甲基硅氧烷辐射制冷材料及其制备方法》(申请公布号:CN113072737A),该方法首先合成微米级NaCl致孔剂,通过控制微米级NaCl致孔剂的大小和用量来控制合成多孔PDMS内孔隙的分布和尺寸,虽然该材料具有的孔隙可以散射太阳光谱波段的光,并隔绝散热体与周围环境的热交换,但是该材料在大气窗口区域发射性能较差。China has published a patent "a porous polydimethylsiloxane radiation refrigeration material and its preparation method" (application publication number: CN113072737A), this method first synthesizes micron-scale NaCl porogen, by controlling the micron-scale NaCl porogen The size and dosage of the synthetic porous PDMS are used to control the distribution and size of the pores in the synthetic porous PDMS. Although the pores of the material can scatter the light in the solar spectral band and isolate the heat exchange between the heat sink and the surrounding environment, the material emits properties in the atmospheric window region. poor.

发明内容SUMMARY OF THE INVENTION

本发明的目的是要解决现有技术制备的辐射制冷材料存在制备方法不环保,或大气窗口区域发射性能较差的问题,而提供采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法。The purpose of the present invention is to solve the problem that the radiation refrigeration material prepared by the prior art has an unenvironmental preparation method or poor emission performance in the atmospheric window region, and provides a template method to prepare a non-continuous scattering enhanced hole-ball composite polymer-based radiation Methods of refrigeration materials.

采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法,具体是按以下步骤完成的:The method for preparing a discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material by a template method is specifically completed according to the following steps:

一、制备聚合物混合液:将聚合物预聚体与固化剂充分混匀后,在真空机中抽真空消除气泡,制得聚合物混合液;所述聚合物预聚体与固化剂的体积比为10:(1~6);1. Preparation of polymer mixed liquid: after fully mixing the polymer prepolymer and the curing agent, vacuumize in a vacuum machine to eliminate air bubbles to prepare a polymer mixed liquid; the volume of the polymer prepolymer and the curing agent The ratio is 10:(1~6);

二、成型;先将致孔剂与无机微球材料混匀后平铺于容器内,再将步骤一得到的聚合物混合液均匀浇筑于容器内,然后置于真空机中抽真空消除气泡,最后进行固化成型,得到辐射制冷材料粗品;所述辐射制冷材料粗品中致孔剂的体积分数为30%~60%;所述辐射制冷材料粗品中无机微球材料的体积分数为6%~20%;2. Forming: first, mix the porogen and the inorganic microsphere material uniformly and then spread them in the container, then pour the polymer mixture obtained in step 1 into the container evenly, and then place it in a vacuum machine to vacuumize to eliminate air bubbles, Finally, solidify and form to obtain a crude radiation refrigeration material; the volume fraction of the porogen in the crude radiation refrigeration material is 30% to 60%; the volume fraction of the inorganic microsphere material in the crude radiation refrigeration material is 6% to 20% %;

三、去除致孔剂:将辐射制冷材料粗品浸于去离子水中加热脱除致孔剂,再放入烘箱中烘干,得到非连续散射强化的孔球复合聚合物基辐射制冷材料,所述非连续散射强化的孔球复合聚合物基辐射制冷材料的厚度为400μm~5mm。3. Removal of the porogen: the crude radiation refrigeration material is immersed in deionized water and heated to remove the porogen, and then placed in an oven for drying to obtain a non-continuous scattering-enhanced pore-ball composite polymer-based radiation refrigeration material. The thickness of the discontinuous scattering-enhanced hole-ball composite polymer-based radiation refrigeration material is 400 μm to 5 mm.

本发明优点:Advantages of the present invention:

一、本发明制备的非连续散射强化的孔球复合聚合物基辐射制冷材料具有孔隙散射体和微球散射体,孔隙散射体有较强的Mie散射效应,可以强烈散射太阳光谱波段的光,并且其中的孔隙可以隔绝散射体与周围环境的热交换。而微球散射体既可以通过Mie散射效应强烈散射太阳光谱波段的光,又可以通过表面声子极化共振效应强烈发射大气窗口波段的光,实现日间辐射制冷效果。1. The discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material prepared by the present invention has a porous scatterer and a microsphere scatterer, and the porous scatterer has a strong Mie scattering effect, which can strongly scatter the light in the solar spectrum band, And the pores in it can isolate the heat exchange between the scatterer and the surrounding environment. The microsphere scatterers can not only strongly scatter the light in the solar spectral band through the Mie scattering effect, but also can strongly emit the light in the atmospheric window band through the surface phonon polarization resonance effect, so as to achieve the effect of daytime radiation cooling.

二、本发明制备的非连续散射强化的孔球复合聚合物基辐射制冷材料其太阳光谱(0.3μm~1μm)反射率R可以达到68%,与单一多孔材料(如实施例3)相比,本发明制备的非连续散射强化的孔球复合聚合物基辐射制冷材料在大气窗口波段(8μm~13μm)发射率显著提高;且夜间降温效果最低可达5.8℃。2. The discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material prepared by the present invention has a solar spectrum (0.3 μm-1 μm) reflectance R of 68%. Compared with a single porous material (such as Example 3), The non-continuous scattering-strengthened hole-ball composite polymer-based radiation refrigeration material prepared by the invention significantly increases the emissivity in the atmospheric window band (8 μm-13 μm); and the cooling effect at night can be as low as 5.8°C.

三、本发明制备的非连续散射强化的孔球复合聚合物基辐射制冷材料具有单层膜结构,结构简单,稳定性好。3. The discontinuous scattering-strengthened porous-ball composite polymer-based radiation refrigeration material prepared by the invention has a single-layer membrane structure, which is simple in structure and good in stability.

四、本发明制备方法操作简单,成本较低,环境友好,可大规模制备与应用。Fourth, the preparation method of the present invention is simple in operation, low in cost, environmentally friendly, and can be prepared and applied on a large scale.

附图说明Description of drawings

图1是实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料实物照片;Fig. 1 is a real photo of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material obtained in Example 1;

图2是大气窗口区域发射率光谱图,图中A表示实施例1制备的非连续散射强化的孔球复合聚合物基辐射制冷材料的大气窗口区域发射率光谱图,B表示实施例2制备的非连续散射强化的孔球复合聚合物基辐射制冷材料的大气窗口区域发射率光谱图,C表示对比例1制备的纯多孔材料的大气窗口区域发射率光谱图;Fig. 2 is an emissivity spectrogram in the atmospheric window region, in which A represents the atmospheric window region emissivity spectrogram of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material prepared in Example 1, and B represents the emissivity spectrogram in the atmospheric window region prepared in Example 2 The atmospheric window region emissivity spectrum of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material, C represents the atmospheric window region emissivity spectrum of the pure porous material prepared in Comparative Example 1;

图3是实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料太阳光谱区域反射率光谱图。FIG. 3 is a reflectance spectrum in the solar spectral region of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material obtained in Example 1. FIG.

具体实施方式Detailed ways

具体实施方式一:本实施方式是采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法,具体是按以下步骤完成的:Embodiment 1: This embodiment is a method for preparing a discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material by a template method, which is specifically completed according to the following steps:

一、制备聚合物混合液:将聚合物预聚体与固化剂充分混匀后,在真空机中抽真空消除气泡,制得聚合物混合液;所述聚合物预聚体与固化剂的体积比为10:(1~6);1. Preparation of polymer mixed liquid: after fully mixing the polymer prepolymer and the curing agent, vacuumize in a vacuum machine to eliminate air bubbles to prepare a polymer mixed liquid; the volume of the polymer prepolymer and the curing agent The ratio is 10:(1~6);

二、成型;先将致孔剂与无机微球材料混匀后平铺于容器内,再将步骤一得到的聚合物混合液均匀浇筑于容器内,然后置于真空机中抽真空消除气泡,最后进行固化成型,得到辐射制冷材料粗品;所述辐射制冷材料粗品中致孔剂的体积分数为30%~60%;所述辐射制冷材料粗品中无机微球材料的体积分数为6%~20%;2. Forming: first, mix the porogen and the inorganic microsphere material uniformly and then spread them in the container, then pour the polymer mixture obtained in step 1 into the container evenly, and then place it in a vacuum machine to vacuumize to eliminate air bubbles, Finally, solidify and form to obtain a crude radiation refrigeration material; the volume fraction of the porogen in the crude radiation refrigeration material is 30% to 60%; the volume fraction of the inorganic microsphere material in the crude radiation refrigeration material is 6% to 20% %;

三、去除致孔剂:将辐射制冷材料粗品浸于去离子水中加热脱除致孔剂,再放入烘箱中烘干,得到非连续散射强化的孔球复合聚合物基辐射制冷材料,所述非连续散射强化的孔球复合聚合物基辐射制冷材料的厚度为400μm~5mm。3. Removal of the porogen: the crude radiation refrigeration material is immersed in deionized water and heated to remove the porogen, and then placed in an oven for drying to obtain a non-continuous scattering-enhanced pore-ball composite polymer-based radiation refrigeration material. The thickness of the discontinuous scattering-enhanced hole-ball composite polymer-based radiation refrigeration material is 400 μm to 5 mm.

具体实施方式二:本实施方式与具体实施方式一的不同点是:步骤一中所述聚合物预聚体为环氧树脂预聚体、聚酯树脂预聚体、聚丙烯酸酯树脂预聚体、聚酰胺树脂预聚体、聚氨酯树脂预聚体、聚烯烃树脂预聚体、氟树脂预聚体或硅树脂预聚体中的一种。其他与具体实施方式一相同。Embodiment 2: The difference between this embodiment and Embodiment 1 is that the polymer prepolymer in step 1 is an epoxy resin prepolymer, a polyester resin prepolymer, and a polyacrylate resin prepolymer , a polyamide resin prepolymer, a polyurethane resin prepolymer, a polyolefin resin prepolymer, a fluororesin prepolymer or a silicone resin prepolymer. Others are the same as the first embodiment.

具体实施方式三:本实施方式与具体实施方式一或二之一不同点是:步骤一中所述固化剂为过氧化苯甲酰、偶氮二异丁腈、过氧化甲乙酮和三乙烯二胺中的一种或几种。其他与具体实施方式一或二相同。Embodiment 3: The difference between this embodiment and Embodiment 1 or 2 is that the curing agent in step 1 is benzoyl peroxide, azobisisobutyronitrile, methyl ethyl ketone peroxide and triethylenediamine one or more of them. Others are the same as in the first or second embodiment.

具体实施方式四:本实施方式与具体实施方式一至三之一不同点是:步骤一中在真空机中抽真空,至真空度为0.02MPa~0.04MPa,在真空度为0.02MPa~0.04MPa下消除气泡0.8h~1.5h。其他与具体实施方式一至三相同。Embodiment 4: One of the differences between this embodiment and Embodiments 1 to 3 is that in step 1, the vacuum is evacuated in a vacuum machine to a degree of vacuum of 0.02 MPa to 0.04 MPa, and when the degree of vacuum is 0.02 MPa to 0.04 MPa Eliminate air bubbles for 0.8h to 1.5h. Others are the same as those in Embodiments 1 to 3.

具体实施方式五:本实施方式与具体实施方式一至四之一不同点是:步骤二中所述致孔剂为NaCl和糖中的一种或两种。其他与具体实施方式一至四相同。Embodiment 5: The difference between this embodiment and Embodiments 1 to 4 is that the porogen in step 2 is one or both of NaCl and sugar. Others are the same as the specific embodiments 1 to 4.

具体实施方式六:本实施方式与具体实施方式一至五之一不同点是:步骤二中所述无机微球材料为SiO2粉、BaSO4粉、CaCO3粉、MgO粉、Al2O3粉、Si3N4粉、钛白粉、滑石粉、硅酸铝粉和陶瓷粉中的一种或几种,且所述无机微球材料的粒径为0.4μm~2μm。其他与具体实施方式一至五相同。Embodiment 6: The difference between this embodiment and Embodiments 1 to 5 is that the inorganic microsphere materials described in step 2 are SiO 2 powder, BaSO 4 powder, CaCO 3 powder, MgO powder, Al 2 O 3 powder , one or more of Si 3 N 4 powder, titanium dioxide powder, talc powder, aluminum silicate powder and ceramic powder, and the particle size of the inorganic microsphere material is 0.4 μm to 2 μm. Others are the same as the specific embodiments 1 to 5.

具体实施方式七:本实施方式与具体实施方式一至六之一不同点是:步骤二中置于真空机中抽真空,至真空度为0.02MPa~0.04MPa,在真空度为0.02MPa~0.04MPa下消除气泡0.8h~1.5h。其他与具体实施方式一至六相同。Embodiment 7: One of the differences between this embodiment and Embodiments 1 to 6 is that: in step 2, the vacuum is placed in a vacuum machine, and the vacuum degree is 0.02MPa to 0.04MPa, and the vacuum degree is 0.02MPa to 0.04MPa. Remove air bubbles for 0.8h to 1.5h. Others are the same as the specific embodiments 1 to 6.

具体实施方式八:本实施方式与具体实施方式一至七之一不同点是:步骤二中在温度为80~120℃进行固化。其他与具体实施方式一至七相同。Embodiment 8: This embodiment differs from Embodiments 1 to 7 in that: in step 2, curing is performed at a temperature of 80-120°C. Others are the same as the specific embodiments 1 to 7.

具体实施方式九:本实施方式与具体实施方式一至八之一不同点是:步骤三中将辐射制冷材料粗品浸于去离子水中,在温度为40~80℃下加热2h~8h。其他与具体实施方式一至八相同。Embodiment 9: This embodiment differs from Embodiments 1 to 8 in that: in step 3, the crude radiative refrigeration material is immersed in deionized water, and heated at a temperature of 40-80°C for 2h-8h. Others are the same as the specific embodiments 1 to 8.

具体实施方式十:本实施方式与具体实施方式一至九之一不同点是:步骤三中在温度为50~100℃烘干0.5h~2h。其他与具体实施方式一至九相同。Embodiment 10: This embodiment differs from Embodiments 1 to 9 in that: in step 3, drying is performed at a temperature of 50 to 100° C. for 0.5 h to 2 h. Others are the same as the specific embodiments 1 to 9.

本发明内容不仅限于上述各实施方式的内容,其中一个或几个具体实施方式的组合同样也可以实现发明的目的。The content of the present invention is not limited to the content of the above-mentioned embodiments, and a combination of one or more specific embodiments can also achieve the purpose of the invention.

采用下述实验验证本发明效果:Adopt following experiment to verify the effect of the present invention:

实施例1:采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法,具体是按以下步骤完成的:Embodiment 1: The method for preparing discontinuous scattering-enhanced porous spherical composite polymer-based radiation refrigeration material by template method, which is specifically completed according to the following steps:

一、制备聚合物混合液:将聚合物预聚体与固化剂充分混匀后,在真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,制得聚合物混合液;所述聚合物预聚体与固化剂的体积比为10:1;1. Preparation of polymer mixture: After fully mixing the polymer prepolymer and curing agent, vacuumize in a vacuum machine until the vacuum degree is 0.02MPa, and eliminate bubbles at a vacuum degree of 0.02MPa for 1 hour to obtain a polymer The volume ratio of the polymer prepolymer to the curing agent is 10:1;

二、成型;先将致孔剂与无机微球材料混匀后平铺于容器内,再将步骤一得到的聚合物混合液均匀浇筑于容器内,然后置于真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,最后在温度为100℃进行固化成型,得到辐射制冷材料粗品;所述辐射制冷材料粗品中致孔剂的体积分数为50%;所述辐射制冷材料粗品中无机微球材料的体积分数为13%;2. Forming: first mix the porogen and the inorganic microsphere material uniformly and then spread them in the container, then pour the polymer mixture obtained in step 1 into the container uniformly, and then place it in a vacuum machine to vacuumize until the vacuum is reached. The temperature is 0.02MPa, the bubbles are eliminated at a vacuum degree of 0.02MPa for 1 hour, and finally the temperature is 100 °C for curing and molding to obtain a crude radiation refrigeration material; the volume fraction of the porogen in the crude radiation refrigeration material is 50%; The volume fraction of inorganic microsphere material in the crude radiation refrigeration material is 13%;

三、去除致孔剂:将辐射制冷材料粗品浸于去离子水中,在温度为80℃下加热8h脱除致孔剂,再放入烘箱中,在温度为80℃烘干1h,得到非连续散射强化的孔球复合聚合物基辐射制冷材料,所述非连续散射强化的孔球复合聚合物基辐射制冷材料的厚度为2.5mm。3. Removal of porogen: Immerse the crude radiation refrigeration material in deionized water, heat it at 80°C for 8 hours to remove the porogen, then put it in an oven, and dry it at 80°C for 1 hour to obtain discontinuous A scattering-enhanced hole-ball composite polymer-based radiation refrigeration material, the thickness of the discontinuous scattering-enhanced hole-ball composite polymer-based radiation refrigeration material is 2.5 mm.

本实施例步骤一中所述聚合物预聚体为PDMS预聚体。The polymer prepolymer described in step 1 of this example is a PDMS prepolymer.

本实施例步骤一中所述固化剂为过氧化苯甲酰。The curing agent described in step 1 of this embodiment is benzoyl peroxide.

本实施例步骤二中所述致孔剂为糖。The porogen in the second step of this example is sugar.

本实施例步骤二中所述无机微球材料为SiO2粉,且所述无机微球材料的平均粒径为4μm。In the second step of this embodiment, the inorganic microsphere material is SiO 2 powder, and the average particle size of the inorganic microsphere material is 4 μm.

图1是实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料实物照片,通过对照片进行孔隙放大分析,实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料的平均孔径约为280μm。Figure 1 is a real photo of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material obtained in Example 1. By performing pore amplification analysis on the photo, the discontinuous-scattering-enhanced porous-spherical composite polymer-based radiation obtained in Example 1 The average pore size of the refrigeration material is about 280 μm.

通过光纤光谱仪(CHS-5000/200μm)对实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料进行反射率的检测,结果如附图3所示,图3是实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料太阳光谱区域反射率光谱图,通过图3可知在太阳光谱(0.3μm~1μm)范围内反射率R可以达到68%。Optical fiber spectrometer (CHS-5000/200μm) was used to detect the reflectivity of the discontinuous scattering-enhanced hole-ball composite polymer-based radiation refrigeration material obtained in Example 1. The results are shown in Figure 3, which is Example 1. Figure 3 shows that the reflectance R in the solar spectrum (0.3μm-1μm) range can reach 68%.

采用热电偶(VC6801)对实施例1得到的非连续散射强化的孔球复合聚合物基辐射制冷材料的降温效果进行测试,其夜间降温效果最低可达5.8℃。A thermocouple (VC6801) was used to test the cooling effect of the discontinuous scattering-enhanced porous-ball composite polymer-based radiation refrigeration material obtained in Example 1, and its nighttime cooling effect was as low as 5.8°C.

实施例2:采用模板法制备非连续散射强化的孔球复合聚合物基辐射制冷材料的方法,具体是按以下步骤完成的:Embodiment 2: The method for preparing discontinuous scattering-enhanced porous spherical composite polymer-based radiation refrigeration material by template method, which is specifically completed according to the following steps:

一、制备聚合物混合液:将聚合物预聚体与固化剂充分混匀后,在真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,制得聚合物混合液;所述聚合物预聚体与固化剂的体积比为10:1;1. Preparation of polymer mixture: After fully mixing the polymer prepolymer and curing agent, vacuumize in a vacuum machine until the vacuum degree is 0.02MPa, and eliminate bubbles at a vacuum degree of 0.02MPa for 1 hour to obtain a polymer The volume ratio of the polymer prepolymer to the curing agent is 10:1;

二、成型;先将致孔剂与无机微球材料混匀后平铺于容器内,再将步骤一得到的聚合物混合液均匀浇筑于容器内,然后置于真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,最后在温度为100℃进行固化成型,得到辐射制冷材料粗品;所述辐射制冷材料粗品中致孔剂的体积分数为50%;所述辐射制冷材料粗品中无机微球材料的体积分数为10%;2. Forming: first mix the porogen and the inorganic microsphere material uniformly and then spread them in the container, then pour the polymer mixture obtained in step 1 into the container uniformly, and then place it in a vacuum machine to vacuumize until the vacuum is reached. The temperature is 0.02MPa, the bubbles are eliminated at a vacuum degree of 0.02MPa for 1 hour, and finally the temperature is 100 °C for curing and molding to obtain a crude radiation refrigeration material; the volume fraction of the porogen in the crude radiation refrigeration material is 50%; The volume fraction of the inorganic microsphere material in the crude radiation refrigeration material is 10%;

三、去除致孔剂:将辐射制冷材料粗品浸于去离子水中,在温度为80℃下加热8h脱除致孔剂,再放入烘箱中,在温度为80℃烘干1h,得到非连续散射强化的孔球复合聚合物基辐射制冷材料,所述非连续散射强化的孔球复合聚合物基辐射制冷材料的厚度为2.5mm。3. Removal of porogen: Immerse the crude radiation refrigeration material in deionized water, heat it at 80°C for 8 hours to remove the porogen, then put it in an oven, and dry it at 80°C for 1 hour to obtain discontinuous A scattering-enhanced hole-ball composite polymer-based radiation refrigeration material, the thickness of the discontinuous scattering-enhanced hole-ball composite polymer-based radiation refrigeration material is 2.5 mm.

本实施例步骤一中所述聚合物预聚体为PDMS预聚体。The polymer prepolymer described in step 1 of this example is a PDMS prepolymer.

本实施例步骤一中所述固化剂为过氧化苯甲酰。The curing agent described in step 1 of this embodiment is benzoyl peroxide.

本实施例步骤二中所述致孔剂为糖。The porogen in the second step of this example is sugar.

本实施例步骤二中所述无机微球材料为SiO2粉,且所述无机微球材料的平均粒径为4μm。In the second step of this embodiment, the inorganic microsphere material is SiO 2 powder, and the average particle size of the inorganic microsphere material is 4 μm.

对比例1:不添加无机微球材料对比:Comparative Example 1: Comparison of materials without inorganic microspheres added:

一、制备聚合物混合液:将聚合物预聚体与固化剂充分混匀后,在真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,制得聚合物混合液;所述聚合物预聚体与固化剂的体积比为10:1;1. Preparation of polymer mixture: After fully mixing the polymer prepolymer and curing agent, vacuumize in a vacuum machine until the vacuum degree is 0.02MPa, and eliminate bubbles at a vacuum degree of 0.02MPa for 1 hour to obtain a polymer The volume ratio of the polymer prepolymer to the curing agent is 10:1;

二、成型;先将致孔剂平铺于容器内,再将步骤一得到的聚合物混合液均匀浇筑于容器内,然后置于真空机中抽真空,至真空度为0.02MPa,在真空度为0.02MPa下消除气泡1h,最后在温度为100℃进行固化成型,得到辐射制冷材料粗品;所述辐射制冷材料粗品中致孔剂的体积分数为50%;2. Forming: firstly spread the porogen in the container, then pour the polymer mixture obtained in step 1 into the container evenly, and then place it in a vacuum machine to vacuum until the degree of vacuum is 0.02MPa, and the degree of vacuum is 0.02MPa. The bubbles were eliminated at 0.02 MPa for 1 h, and finally the temperature was 100 °C for curing and molding to obtain a crude radiation refrigeration material; the volume fraction of the porogen in the crude radiation refrigeration material was 50%;

三、去除致孔剂:将辐射制冷材料粗品浸于去离子水中,在温度为80℃下加热8h脱除致孔剂,再放入烘箱中,在温度为80℃烘干1h,得到纯多孔材料,所述纯多孔材料的厚度为2.5mm。3. Removal of porogen: Immerse the crude radiation refrigeration material in deionized water, heat it at 80°C for 8 hours to remove the porogen, then put it in an oven, and dry it at 80°C for 1 hour to obtain pure porous material, the thickness of the pure porous material is 2.5mm.

本实施例步骤一中所述聚合物预聚体为PDMS预聚体。The polymer prepolymer described in step 1 of this example is a PDMS prepolymer.

本实施例步骤一中所述固化剂为过氧化苯甲酰。The curing agent described in step 1 of this embodiment is benzoyl peroxide.

本实施例步骤二中所述致孔剂为糖。The porogen in the second step of this example is sugar.

通过傅里叶光谱仪对实施例1和2制备的非连续散射强化的孔球复合聚合物基辐射制冷材料及对比例1制备的纯多孔材料进行太阳光谱区域的发射率进行测量,结果如附图2所示;图2是大气窗口区域发射率光谱图,图中A表示实施例1制备的非连续散射强化的孔球复合聚合物基辐射制冷材料的大气窗口区域发射率光谱图,B表示实施例2制备的非连续散射强化的孔球复合聚合物基辐射制冷材料的大气窗口区域发射率光谱图,C表示对比例1制备的纯多孔材料的大气窗口区域发射率光谱图,通过实施例1与对比例1相比,本发明制备的非连续散射强化的孔球复合聚合物基辐射制冷材料在大气窗口波段(8μm~13μm)发射率显著提高。The emissivity in the solar spectral region was measured by Fourier spectrometer on the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration materials prepared in Examples 1 and 2 and the pure porous material prepared in Comparative Example 1. The results are shown in the accompanying drawings. 2; Figure 2 is the atmospheric window region emissivity spectrum, in the figure A represents the atmospheric window region emissivity spectrum of the discontinuous scattering enhanced porous-sphere composite polymer-based radiation refrigeration material prepared in Example 1, and B represents the implementation The atmospheric window region emissivity spectrum of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material prepared in Example 2, C represents the atmospheric window region emissivity spectrum of the pure porous material prepared in Comparative Example 1, through Example 1 Compared with Comparative Example 1, the emissivity of the discontinuous scattering-enhanced porous-sphere composite polymer-based radiation refrigeration material prepared by the present invention is significantly improved in the atmospheric window band (8 μm-13 μm).

Claims (10)

1. The method for preparing the discontinuous scattering reinforced hole-sphere composite polymer-based radiation refrigeration material by adopting the template method is characterized by comprising the following steps of:
firstly, preparing a polymer mixed solution: fully and uniformly mixing the polymer prepolymer and the curing agent, and vacuumizing in a vacuum machine to eliminate bubbles to prepare a polymer mixed solution; the volume ratio of the polymer prepolymer to the curing agent is 10 (1-6);
secondly, forming; uniformly mixing a pore-foaming agent and an inorganic microsphere material, then flatly paving the mixture in a container, uniformly pouring the polymer mixture obtained in the step one into the container, then placing the container in a vacuum machine for vacuumizing to eliminate bubbles, and finally performing curing molding to obtain a crude product of the radiation refrigeration material; the volume fraction of the pore-foaming agent in the crude product of the radiation refrigeration material is 30-60%; the volume fraction of the inorganic microsphere material in the crude product of the radiation refrigeration material is 6-20%;
thirdly, removing the pore-foaming agent: and soaking the crude product of the radiation refrigeration material in deionized water, heating to remove a pore-forming agent, and then putting the crude product of the radiation refrigeration material into an oven for drying to obtain the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material, wherein the thickness of the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material is 400 mu m-5 mm.
2. The method for preparing a discontinuous scattering-reinforced hole-sphere composite polymer-based radiation refrigeration material according to claim 1, wherein in the step one, the polymer prepolymer is one of epoxy resin prepolymer, polyester resin prepolymer, polyacrylate resin prepolymer, polyamide resin prepolymer, polyurethane resin prepolymer, polyolefin resin prepolymer, fluororesin prepolymer or silicone resin prepolymer.
3. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method as claimed in claim 2, wherein the curing agent in the step one is one or more of benzoyl peroxide, azobisisobutyronitrile, methyl ethyl ketone peroxide and triethylene diamine.
4. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method as claimed in claim 3, wherein in the step one, the vacuum machine is vacuumized until the vacuum degree is 0.02MPa to 0.04MPa, and bubbles are eliminated for 0.8h to 1.5h under the vacuum degree of 0.02MPa to 0.04 MPa.
5. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method according to claim 1 or 4, wherein the pore-forming agent in the second step is one or both of NaCl and sugar.
6. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method as claimed in claim 5, wherein the inorganic microsphere material in the second step is SiO 2 Powder, BaSO 4 Powder, CaCO 3 Powder, MgO powder, Al 2 O 3 Powder, Si 3 N 4 One or more of powder, titanium dioxide, talcum powder, aluminum silicate powder and ceramic powder, and the particle size of the inorganic microsphere material is 0.4-2 mu mm。
7. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method according to claim 6, wherein in the second step, the material is placed in a vacuum machine for vacuum pumping until the vacuum degree is 0.02MPa to 0.04MPa, and bubbles are eliminated for 0.8h to 1.5h under the vacuum degree of 0.02MPa to 0.04 MPa.
8. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method as claimed in claim 7, wherein the curing is carried out at a temperature of 80-120 ℃ in the second step.
9. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method according to claim 1 or 8, characterized in that in the third step, the crude product of the radiation refrigeration material is immersed in deionized water and heated at the temperature of 40-80 ℃ for 2-8 h.
10. The method for preparing the discontinuous scattering-reinforced pore-sphere composite polymer-based radiation refrigeration material by adopting the template method according to claim 9, wherein the drying is carried out at the temperature of 50-100 ℃ for 0.5-2 h in the third step.
CN202210489324.0A 2022-05-06 2022-05-06 Method for preparing discontinuous scattering reinforced hole-sphere composite polymer-based radiation refrigeration material by adopting template method Pending CN114806514A (en)

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Application publication date: 20220729