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A light-weight, high-strength, heat-insulating and wave-permeable composite material and its preparation method

A composite material and high-strength technology, applied in chemical instruments and methods, lamination auxiliary operations, lamination and other directions, can solve the problems of improving the thermal insulation performance of resin-based composite materials, poor mechanical properties, and inability to radome main structural materials, etc. To achieve the effect of improving heat resistance and mechanical properties, meeting thermal insulation requirements, and improving thermal insulation performance

Active Publication Date: 2022-01-28
SHANDONG NON METALLIC MATERIAL RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, its mechanical properties are extremely poor, and the tensile strength at room temperature is only 0.88MPa. It can only be used as a heat-insulating and wave-transmitting functional material, and cannot be used as the main structural material of the radome.
[0009] At present, there are no domestic reports on the use of hollow quartz fibers as reinforcements to prepare silicone resin-based wave-transparent composite materials to reduce material density, improve strength, heat insulation performance and dielectric properties, and there is no use of airgel powder as filler to improve Report on Thermal Insulation Properties of Resin Matrix Composites

Method used

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  • A light-weight, high-strength, heat-insulating and wave-permeable composite material and its preparation method
  • A light-weight, high-strength, heat-insulating and wave-permeable composite material and its preparation method

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Experimental program
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Effect test

Embodiment 1

[0051] Add 8.2g octaglycidyl ether-based POSS, 0.08g 2-ethyl-4-methylimidazole, 8.2g SiO 2 Airgel powder (specific surface area 650m 2 / g), after ultrasonic dispersion, heat and react at 50°C for 8 hours to prepare a modified methylphenyl silicone resin solution. Brush the resin solution evenly on the surface of 164g hollow quartz fiber cloth (hollowness 32%), let it air in the air for 12 hours, then treat it in a blast drying oven at 50°C for 40 minutes, and cut it into 180mm×180mm prepreg cloth after drying , laying up neatly to get the prepreg layer. Place the prepreg layer on a vacuum hot press machine for hot press molding. The final molding temperature is 230°C and the pressure is 9MPa. After the molding is completed, it is cooled to obtain a composite material. The composite material is heat-treated in a high-temperature oven under the condition of 300° C. for 3 minutes to obtain a resin-based wave-transparent composite material.

Embodiment 2

[0053] In 820g methylphenyl silicone resin solution (DC808, resin mass concentration is 30%), add 36.9g octaglycidyl ether base POSS, 0.4g triethylamine, 19.6gAl 2 o 3 Airgel powder (specific surface area 350m 2 / g), after ultrasonic dispersion, heat and react at 120°C for 2 hours to prepare a modified methylphenyl silicone resin solution. Brush the resin solution evenly on the surface of 300g hollow quartz fiber cloth (hollowness 42%), let it air in the air for 4 hours, then treat it in a blast drying oven at 100°C for 20 minutes, cut it into 250mm×250mm prepreg after drying Cloth, laid neatly to obtain prepreg cloth layer. Place the prepreg layer on a vacuum hot press for hot pressing molding. The final molding temperature is 210°C and the pressure is 16MPa. After molding, it is cooled to obtain a composite material. The composite material is heat-treated in a high-temperature oven under the condition of 400° C. for 3 minutes to obtain a resin-based wave-transparent compo...

Embodiment 3

[0055] Add 3.24g octaepoxycyclohexyl POSS, 0.03g diaminodiphenyl sulfone, 16.2g ZrO successively in 180g methyl silicone resin solution (SH-9502, resin mass concentration is 60%) 2 Airgel powder (specific surface area 400m 2 / g), after ultrasonic dispersion, heat and react at 80°C for 5h, and prepare a modified methyl silicone resin solution. Brush the resin solution evenly on the surface of 162g hollow quartz fiber cloth (hollowness 32%), let it air in the air for 8 hours, then treat it in a blast drying oven at 80°C for 40 minutes, and cut it into 150mm×150mm prepreg cloth after drying , laying up neatly to get the prepreg layer. Place the prepreg layer on a vacuum hot press for hot pressing molding. The final molding temperature is 200°C and the pressure is 6MPa. After molding, it is cooled to obtain a composite material. The composite material is heat-treated in a high-temperature oven under the condition of 400° C. for 1 minute to obtain a resin-based wave-transparent c...

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Abstract

The invention belongs to the field of composite materials, and in particular relates to a light-weight, high-strength, heat-insulating and wave-permeable composite material and a preparation method thereof. The hollow quartz fiber is used as a reinforcement, the organic silicon resin is used as a matrix, and airgel powder is added as an additive. The resin-based wave-transparent composite material is prepared by compression molding. The material has the characteristics of low density, high strength, excellent dielectric performance and heat insulation performance, and is especially suitable for the structure / transmission Technical requirements for wave composite materials.

Description

technical field [0001] The invention belongs to the field of composite materials, and in particular relates to a light-weight, high-strength, heat-insulating and wave-permeable composite material and a preparation method thereof. Background technique [0002] As a key component of missile weapons, the radome is an important part of the antenna system and is called the "electromagnetic window" of the antenna system. The radome is located on the head or the side of the projectile weapon equipment. During the high Mach number flight of the projectile weapon, it is subjected to severe aerodynamic heating and the endurance time is getting longer and longer. The temperature at the stagnation point is high. , heat protection, heat insulation, wave transmission, bearing and other functions in one structure / function integrated component. The characteristics of the radome are high acceleration load, fast aerodynamic temperature rise of the wall, low power, high precision, complex use...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C08L83/04C08L83/06C08K7/26C08K7/24C08K7/10C08J5/24B32B5/02B32B33/00B32B5/26B32B37/06B32B37/10B32B38/00
CPCC08J5/24B32B5/02B32B33/00B32B5/26B32B37/06B32B37/10B32B38/0036C08J2383/04C08J2483/06C08K7/26C08K7/10C08K7/24
Inventor 孔国强李莹魏化震于秋兵尹磊安振河李居影王康孙晓冬毕卫东
Owner SHANDONG NON METALLIC MATERIAL RES INST