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A high-temperature-resistant radiation-resistant heat insulation component and its preparation method

A radiation-resistant and high-temperature-resistant technology, applied in ceramic products, other household appliances, household appliances, etc., can solve the problems of not including a radiation-resistant layer, cannot withstand high temperature, and cannot be used, and achieves good radiation resistance. The effect of high temperature thermal insulation performance

Active Publication Date: 2021-04-30
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, this composite material prevents powder falling by chemical methods, cannot withstand high temperatures above 1200°C, cannot be used in an oxygen-deficient environment such as a carbon dioxide environment and / or nitrogen environment, and does not include a suitable anti-radiation layer, and cannot achieve excellent performance. Insulation effect, can not guarantee no excess under high vibration conditions

Method used

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  • A high-temperature-resistant radiation-resistant heat insulation component and its preparation method

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preparation example Construction

[0041] (1) Preparation of core layer:

[0042] A fiber-reinforced matrix formed of at least one fiber selected from the group consisting of quartz fibers, mullite fibers, and alumina fibers is selected. The density of the fiber reinforced matrix can be 0.1g / cm 3 to 0.14g / cm 3 . After preparing the Si-Al sol precursor, add a catalyst such as ammonia (the concentration can be 0.10% to 0.15% by mass, such as 0.12% by mass) and stir evenly, and use the RTM method to impregnate. After the impregnation is completed, after 24h to 48h After aging at room temperature, after 48h-72h of high-temperature aging, the mold was removed for solvent replacement twice, and then supercritical carbon dioxide drying was carried out for 96h. Finally, moisture-proof treatment is carried out in the atmosphere of hydrophobic agent, the treatment temperature is 100-150°C, and the treatment time is 24-48h. Then, the silicon dioxide airgel core layer material is obtained through machining and finishin...

Embodiment 1

[0051] Choose a density of 0.1g / cm 3 The mullite fiber-reinforced matrix is ​​paved into the mold and clamped in place. After the Si-Al sol precursor with a concentration of 15% is prepared, it is mixed with 0.1mol / L NH 3 ·H 2 O Stir evenly according to the mass ratio of 100:3, use the RTM method for impregnation, after the impregnation is completed, after 48 hours of room temperature aging, and then after 48 hours of high temperature aging at 100 ° C, use ethanol for solvent replacement twice after demoulding, and then carry out Dry with supercritical carbon dioxide for 96 hours. Finally, moisture-proof treatment at 100° C. for 48 hours was carried out in an atmosphere of methyltrimethoxysilane. After finishing machining the inner and outer profiles, the airgel is evenly distributed with holes with a diameter of 1mm and a hole spacing of 30mm to obtain the airgel core layer material. After that, the graphite paper with a thickness of 0.2mm is laid flat and cut into a singl...

Embodiment 2

[0054] Choose a density of 0.1g / cm 3 The mullite fiber and quartz fiber are made into a uniform fiber-reinforced matrix in a ratio of 9:1. Lay it into the mold and close the mold in place. After preparing the Si-Al sol precursor with a concentration of 20%, mix it with 0.1mol / L NH 3 ·H 2 O was stirred evenly according to the mass ratio of 100:3, impregnated by the RTM method, aged at room temperature for 48 hours after impregnation, and then aged at 100°C for 48 hours at high temperature. Critical carbon dioxide drying for 96h. Finally, moisture-proof treatment at 150° C. for 24 hours was carried out in an atmosphere of methyltrimethoxysilane. After finishing machining the inner and outer profiles, the airgel is evenly distributed with holes with a diameter of 1mm and a hole spacing of 30mm to obtain the airgel core layer material. Afterwards, the graphite paper with a thickness of 0.5 mm is laid flat and cut into a single-sided size according to the inner and outer surfac...

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Abstract

The invention provides a high-temperature-resistant and radiation-resistant heat-insulation component, a preparation method and application thereof. The heat insulation component includes: a core layer formed by a fiber-reinforced matrix and an airgel material; (2) anti-radiation layers located on both sides of the core layer; and fiber cloth covering the anti-radiation layer. The method includes: impregnating the fiber reinforced matrix with a sol precursor and drying to obtain a core layer; laying anti-radiation layers on both sides of the core layer to form a sandwich structure; covering the sandwich structure with fiber cloth; wrapping the coated sandwich structure Integral sewing to obtain a heat insulating member. The present invention also provides the application of the thermal insulation member in an oxygen-deficient environment, for example, in a carbon dioxide environment and / or a nitrogen environment. The heat insulating member of the present invention can be used in a low-oxygen or oxygen-free environment, such as a carbon dioxide atmosphere and / or a nitrogen atmosphere, which can not only ensure heat insulation performance, but also have excellent high-temperature radiation resistance performance and prevent the generation of redundant substances, etc. performance.

Description

technical field [0001] The invention relates to a high-temperature radiation heat-insulating component and a preparation method thereof, belonging to the technical field of heat protection. Background technique [0002] The field of deep space exploration involves the exploration of the moon, Mars probes, and asteroids, among which the Martian environment is mainly CO 2 atmosphere, and during the landing process of the Mars rover, in order to ensure the normal operation of other electronic components, a high-temperature heat insulation device needs to be added when the engine is ignited. It is a comprehensive performance heat insulation component without excess. [0003] Airgel material is a new type of low-density nanoporous material. It is the solid material with the best thermal insulation performance. Airgel is formed by the accumulation of nanoparticles and has a three-dimensional network nanoporous structure, which can significantly reduce the solid thermal conductivi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B30/02C04B38/00
CPCC04B30/02C04B2111/40C04B2111/763C04B2201/20C04B2201/32C04B14/4643C04B14/302C04B14/064C04B14/024C04B38/0067
Inventor 张丽娟李文静李健孙阔赵英民简文政
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH